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REAL-TIME RECONCILIATION OF COAL COMBUSTOR DATA

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Authors Montgomery, Roger Lee

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MONTGOMERY, ROGER LEE REAL-TIME RECONCILIATION OF COAL COMBUSTQR DATA.

THE UNIVERSITY OF ARIZONA, M#S,, 1982


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International

REAL-TIME RECONCILIATION OF COAL COMBUSTOR DATA

by

Roger Lee Montgomery

A Thesis Submitted to the Faculty of the

DEPARTMENT OF CHEMICAL ENGINEERING

In Partial Fulfillment of the Requirements For the Degree of

MASTER OF SCIENCE

In the Graduate College

THE UNIVERSITY OF ARIZONA

1 9 8 2

STATEMENT BY AUTHOR

This thesis has been submitted in partial fulfillment of requirements for an advanced degree at the University of Arizona and is deposited in the University Library to be made available to borrowers under rules of the Library.

Brief quotations from this thesis are allowable without special permission, provided that accurate acknowledgement of source is made. Requests for permission for extended quotations from or reproduction of this manuscript in whole or in part may be granted by the head of the major department or the Dean of the Graduate College when in his judgment the proposed use of the material is in the interests of scholarship. In all other instances, however, permission must be obtained from the author.

SIGNED:

APPROVAL BY THESIS DIRECTOR

This thesis has been approved on the date shown below:

JOST 0. L. WE Date Profeseor of Chemical Engineering

ACKNOWLEDGMENT

The author wishes to express his gratitude to Dr.

James Wm. White for his guidance, encouragement and shelter,

to Mr. Jonathan P. Olson for his technical help, to Dr.

Jost 0. L. Wendt and Dr. Thomas W. Peterson for their

technical advice, to Mr. James W. Glass for his guidance

during the planning stages of the project and finally to Mr.

Sal Gonzales for his electronics support. The author also

acknowledges financial support provided under D. 0. E.

Contract DE-AC01-79ET-15184.

iii

TABLE OF CONTENTS

Page

LIST OF TABLES vi

LIST OF ILLUSTRATIONS vii

ABSTRACT viii

1 . INTRODUCTION 1

2. DATA ACQUISITION 5

The Combustor Configuration 5 The Data Acquisition .Configuration 10

3. DATA ANALYSIS 17

The Mass Balance Problem 17 The Data Adjustment Problem 22

4. INVESTIGATION 32

Adjustment Verification 32 Consistency Results 37

5. SUMMARY 57

6. CONCLUSIONS 59

7. RECOMMENDATIONS FOR FURTHER STUDY 60

APPENDIX A: FLUE GAS MOISTURE CORRECTION ... 61

APPENDIX B: DETERMINATION OF THE COMBUSTOR SOLUTION SET 62

APPENDIX C: D.O.E. FURNACE MONITOR USER'S GUIDE 69

System Start-up, Shut-down and Crashes ... 70 System Start-up 70 System Shut-down 72 System Crash 73

iv

Option Selection Structure 73 Data Entry i . . . 74 Search 78 Delete 78 Examine . 79 Acquire . 79 Analyze 81 Calibrate ..... 83 Reload 85

APPENDIX D: THE CROMEMCO MICROCOMPUTER PROGRAM 86

System Configuration 86 Interrupt Service Hierarchy 87

System Initialization 88 System Interrupt Service 89 Data Acquisition 94

Concluding Remarks 96

APPENDIX E: D.O.E. COMMAND FILES AND SOURCE LISTINGS 97

v

LIST OF TABLES

Table Page

1. Analyzers Purchased by ERDA Under Contract E(49-18) -1817 9

2. Laminar Flow Element Specifications 11

3. Typical Furnace Data Summary ........ 23

4. Furnace "Calculated" and "Search" Variables 26

5. Consistent Fuel Rich Data Set and Analysis 34

6. Adjustment Classification of "Calculated" and "Search" Variables 38

7. Data Adjustment of Coal Nitrogen Mass Fraction 39

8. Adjustment Classification of Sensitive "Calculated" and "Search" Variables 43

9. Data Adjustment of Coal Hydrogen Mass Fraction 44

10. Data Adjustment of Flue Gas Hydrogen Mole Fraction 47

11. Data Adjustment of Flue Gas Carbon Dioxide Mole Fraction 51

12. Data Adjustment of Flue Gas Nitrogen Mole Fraction 54

vi

LIST OF ILLUSTRATIONS

Figure Page

1. Furnace General Flow Scheme 6

2. Locations of Sampling and Thermocouple Ports . 7

3. Data and Communications Flow Diagram .... 13

4. Cromemco Analog Input Front End 15

5. Material / Composition Flows 18

6. Coggin Data Adjustment in One Space ..... 27

7. Coggin Data Adjustment in Two Space 29

8. Cromemco Macro Flow Chart 91

vii

ABSTRACT

The low cost and versatility of microcomputers as

data acquisition devices has resulted in their widespread

application in chemical and metallurgical processes.

Usually these processes are sufficiently instrumented to

overly define the system. This results in mass balances

which rarely close due to error within the reported data. A

technique for computing consistent mass balances in the

presence of erroneous data is presented. A sum of squares

functional formed from squared data residuals is minimized

by adjusting search variables to reduce error within a

calculated variable set. The technique is applied to coal

combustion data to correct and identify sources of error

within the data.

viii

CHAPTER 1

INTRODUCTION

Within the last ten years, the application of

microcomputers as data acquisition devices has become

widespread throughout chemical and mineral industries. The

result has been increased data reliability and,

consequently, control of process operations. Usually,

process variables that are needed for control purposes are

instrumented whenever possible or calculated from variables

which are measured. The philosophy of "increased control

with more instrumentation" has resulted in processes which

are overly-instrumented from a calculation point of view.

Redundant data enable the calculation of unknown variables

via several paths leading to discrepancies within the

results.

The inconsistencies between data and equations could

be due to three sources. Some of the equations may not

apply to the system, or the method of computation may be

incorrect for the application. Also, it is virtually

impossible to obtain error free data since sensors have

1

2

finite accuracy limits and lifetimes. The first two sources

of inconsistencies can be eliminated by applying suitable

engineering principles and numerical techniques. The third

source can be minimized by correcting instruments which are

out of calibration or improving data acquisition methods.

The extent of this work is concerned with detection

and correction of inconsistent combustion data obtained in a

real-time data acquisition environment. The work is divided

into two stages: data acquisition and data analysis. Data

acquisition is concerned with obtaining data from the

coal-fired research furnace of Wendt and Glass (1979) using

real-time techniques. Data analysis is concerned with

calculating unmeasured furnace operating variables,

providing summary reports of furnace operating conditions,

and performing data adjustment to obtain data consistency in

a least squares sense.

The few publications concerning in data adjustment

in over-defined systems have been restricted to extractive

metallurgical concentrator applications. Smith and Ichiyen

(1973) applied sum of squares functional minimization to

flotation circuit data. The minimization algorithm requires

estimates of data variances and uses a direct search

technique to adjust the data. In some cases negative flow

rates were obtained since loose constraints were not

enforced during optimization. Wiegel (1972) and Hockings

(1977) minimize a sum of squares objective function using

3

Lagrange multipliers; variance estimates are needed in the

sum of squares minimization however. Winslow (1980) points

out that independent variance estimates are difficult to

obtain since multiple simultaneous sets of field data would

need to be collected presenting an unattractive task to

operation personnel.

Whiten (1971) proposed a least squares approach to

removing data inconsistencies through data adjustment in

classifying operations. No methodology on the adjustment

search algorithm was given however. Whiten's results showed

occasional negative screen fractions in the resultant

adjustment set.

White and Winslow (1979, 1977) divide data into

"calculated" and "search" sets such that "search" data is

adjusted to remove "calculated" discrepancies. Both

"calculated" and "search" variables contribute to a sum of

squares functional which is minimized univariably using the

method of Coggin (see Kuester and Mize, 1973). After two

global iterations, convergence is accelerated by minimizing

the functional along a hypervector formed from the previous

two locations in search space. Loose constraints are

enforced by supplying penalty terms when unrealizable

adjustments occur. The method does not require knowledge of

variances and exhibits desirable convergence

characteristics.

N

A characteristic common to the systems investigated

by the aforementioned authors is that data adjustment was

applied to strongly over-defined systems, i.e. fewer

unknown variables than the number of additional equations.

In the furnace application, four unknown variables must be

calculated leaving, at most, two degrees of over-definition

when the six applicable equations are solved. Another

distinction from previously analyzed systems is that

chemical reactions among the constituents occur within the

furnace; unlike the metallurgical examples, component

balances interact prohibiting a staged approach to data

adjustment. Finally, the equilibrium relation of the

water-gas-shift reaction is applied in addition to mass

conservation relationships.

CHAPTER 2

DATA ACQUISITION

The Combustor Configuration

The data acquisition and analysis system described

herein was tailored to the coal-fired research furnace used

by Wendt and Glass (1979, 1978, 1977). Funded by the

Department of Energy, the predominent direction of the

furnace research is in the study of nitrogenous specie

formation and particulate emissions under various operating

conditions.

The combustor proper consists of a refractory lined

cylinder standing vertically to allow a down-fired burn.

Material flows, shown in Figure 1, consists of three air

inputs from an air main, coal input from a screwfeeder, and

flue gas and solids exiting to a convective section.

Transport air carries the coal from the screwfeeder to a

mixing chamber where preheated secondary air is added. The

fuel/air mixture is injected into the furnace throat located

at the top of the furnace. Staged air is added through

ports located along the furnace length, see Figure 2. The

5

6

X Coal

Transport Air

Main Air

Preheater

Primary Air

L

J Supply

Staged Air l5 Furnace

Convective Section

Figure 1: Furnace General Flow Scheme

7

—24'

27' Sampling

Port

Locations

— 30" Thermocouple | Port 3g" Locations

39'

48'

—60'

63" • •

72'

Figure 2: Locations of Sanipling and Thermocouple Ports

8

ports also allow sampling of the furnace atmospheres with a

water quenched probe.

The furnace is normally operated in either a fuel

lean mode, a fuel rich mode or a staged mode (fuel rich

followed by fuel lean conditions). Under fuel lean

conditions, excess air is supplied with either preheated

secondary air or staged air. Fuel rich conditions are

obtained by reducing the secondary air flow rate until the

desired stoichiometric fuel/air mixture is reached. To

ensure a constant coal input flow rate, transport air flow

rate and screw speed are not adjusted following system

start-up.

Combustion products are sampled with a water

quenched probe. The sample is refrigerated and filtered to

remove both moisture and particulates prior to gas analysis.

Gas analysis is provided by a Perkin-Elmer gas chromatograph

and five gas analyzers. The analyzers, listed in Table 1,

measure C02, CO, 02, NO and S02 in a continuous manner. The

chromatograph reports gas fractions of C02, CO, 02, N2, H2

and CH4, as well as trace specie concentrations of NH3, HCN

and H2S. Analyzer outputs are displayed with meters and

recorded with strip chart recorders. Gas chromatograph data

analyses are performed by the microcomputer controlled

chromatograph console and are printed on the console

printer-plotter.

Table 1: Analyzers Purchased by ERDA Under Contract E(49-18) - 1817

1. Beckman Model F3 Paramagnetic 02 Analyzer

2. Beckman Model 864 Infared CO Analyzer

3. Beckman Model 864 Infared C02 Analyzer

4. Beckman Model 75 Polarographic 02 Analyzer

5. Thermo Electron Model 10AR Cherailuminescent NO - NOx Analyzer

10

Air input rates are determined indirectly by

measuring differential pressure across Meriam laminar flow

elements in each air line. Table 2 shows the laminar flow

element specifications and the formula used to determine air

input flow rates at standard conditions.

Temperatures along the length of the furnace are

measured using thermocouples inserted in the furnace wall as

shown in Figure 2. The temperature of the nample is

measured with a thermocouple placed at the tip of the probe

inserted in one of the sampling ports. Axis temperatures

are measured using type R, platinum/platinum-30% rhodium,

thermocouples. Type K, chromel/alumel, thermocouples are

used where temperatures do not exceed 1250 degrees Celsius.

Detailed information concerning the configuration

and operation of the furnace may be found in D.O.E.

quarterly report FE-1518M-1.

The Data Acquisition Configuration

Data acquisition objectives include monitoring

furnace instrumentation, as well as providing a tool for

accessing and analyzing the collected data. Data analysis

and bulk storage functions are performed by the ES/M RTCL

General Automation SPC-16/65 minicomputer. On-line data

acquisition is performed by a Cromemco microcomputer located

near the furnace instrumentation.

1 1

Table 2: Laminar Flow Element•Specifications

8" H20 = 3.2 cfm 6 70°F, 760 mm Hg

8" H20 = 20. cfm @ 70°F, 760 mm Hg

8" H20 = 17. cfm @ 70°F, 760 mm Hg

Given h inches H2O differential pressure, the

following formula is used to obtain SCFM air flow rates:

Transport Air

Secondary Air

Staged Air

Q . = A . * ( 6 9 2 + 1 4 . 7 * 7 6 0 ) m m H q * 5 3 0 ° R * h . 1 1 7 6 0 m m H g ( 4 6 0 ° R + T ) •

Where:

Ai

Pi

T

h.

= Air Flow Stream

= Air Flow Rate

= LFE Specification

= Gauge Pressure

[=] SCFM

[ = ] cfm / inch H2O

[=] psig

= Air Stream Temperature [=] °F

= Manometer Reading [=] inches H20

12

As shown in Figure 3, the Cromemco coordinates all

data transfer. Data originates from three sources: the Gas

Chromatograph Console (GCC), the laboratory operator via the

teletype, and the analog instrumentation via an analog to

digital interface. Communication with the GCC is similar to

communication with the teletype because data is transferred

asynchronously and serially in an ASCII character format.

Data is collected from the analog instrumentation interface

periodically and buffered for subsequent transmission to the

SPC-16. The Cromemco also acts as an extension of the

SPC-16 input/output subsystem when coordinating

communication between the operator and the SPC-16.

The analog instrumentation interface was designed to

allow sampling of the various furnace instrument outputs

under software control. Robinson-Halpern differential

pressure transducers applied to the laminar flow elements

output 0 to +5 VDC over the input range of 0 to 10 inches

H20. The analyzers output signals from -5 to +5 VDC over

their respective concentration ranges. Type R and type K

thermocouples output signals within 0 to 75 mVDC for furnace

operating temperatures.

Each analog signal is sampled by selecting the input

line, amplifying the signal, converting the conditioned

signal to a digital format and reading the digital result.

1 3

Cromemco yU Computer

PerKin-Elmer

Gas Chromatograph

Thermocouples

P/E Transducers

Analyzers

General Automation

SPC-16 Minicomputer

Figure 3: Data and Communications Flow Diagram

14

As shown in Figure 4, the input line is selected by

outputting the channel number of the input line to the

multiplexers. The selected input signal is amplified to

meet the input range requirements of the analog to digital

converter. For an input range of -5 to +5 VDC, the analog

to digital converter generates an integer from 0 to 4096.

The scaled integer is read from the interface and saved in

memory.

The sampling sequence is executed for each input

line every 3.75 seconds. At the end of a minute, the mean

of each input is computed and stored as a vector of means to

represent the instrumentation activity for the previous

minute. A total of sixteen vectors are retained by the

Cromemco so that a sixteen minute history of the

instrumentation activity is maintained. Since the gas

chromatography generates its analysis report fifteen minutes

after injection of the gas sample, the Cromemco can

synchronize the GCC analyses with data from the other

instruments.

Upon request by the user, data being held by the

Cromemco is transferred to the SPC-16 and stored on disk by

record number. An immediate report of air flow rates and

flue gas analysis is output when the data is received by the

SPC-16. The time, date, and data record number are also

1 5

Decoder

X

r

K

Cromemco

Single Card

Computer

LZ_' 12 Bit ADC

4

8 Channel Multiplexer

A

8 Channel 8 Channel

W

JFT ii f n ••• I II ••• I




Figure' 4: Cromemco Analog Input Front End

16

output to facilitate data identification. Referenced by

record number, data may be modified, examined, deleted or

analyzed. Appendix C details the available options.

CHAPTER 3

DATA ANALYSIS

The Mass Balance Problem

Not all variables which describe the operating

condition of the furnace are measured; these system

unknowns must be calculated from the available data. The

equations available are the five component balances of

carbon, hydrogen, oxygen, nitrogen, and sulfur and the

equilibrium of the water-gas-shift reaction. Not all six

equations are necessary because there are, at most, four

unknowns during either fuel rich or fuel lean conditions.

The information provided by the additional equations enables

an optimum data and solution set to be obtained from an

error minimization standpoint.

The variables associated with the furnace material

flows are shown in Figure 5. Coal and air comprise the

material inputs and flue gas and unburned flue solids

comprise the material outputs. Compositions of the streams

are shown to fully define the combustion system from a

steady state material balance perspective. The symbol •

17

1 8

C08 CO 0.79 N:

NO HCN 0.79 N

0.21 0: HzS SOe 0.79 N

0.21 0 NH

HgQ

Qi Mmoles/time

yi C=] mole fraction

Wi C=] mass /time

Xi.nru W mass fraction

© denotes on-line measurement

• denotes off-line measurement

Figure 5: Material / Composition Flows

19

beside a variable denotes that the variable is determined

off-line and must be entered using the teletype. The symbol

(.) denotes that a variable is measured on-line and is

obtained from an instrument monitored by the Cromemco

microcomputer. The remaining variables which are not

measured are declared unknowns; these variables are

calculated from the remaining data.

Coal and flue solids analyses are performed off-line

and must be entered by the operator prior to mass balance

calculations. Coal analyses are available prior to

operating the furnace and need to be entered only when the

composition of the coal feed changes. Flue solids analyses

are not available for use in on-line calculations and must

be assumed. On an ash-free basis, the flue solids are

normally greater than 95? carbon by weight. The assumption

of 100% carbon on the same basis is made for on-line mass

balance calculations; a better estimate may be entered and

will be assumed constant until a new composition is entered.

On-line measurements yield data for air input rates

and flue gas fractions. Flue gas fractions, available from

the analyzers, are C02, CO, 02, and NO. Flue gas fractions

available from the gas chromatograph are C02, CO, 02, H2,

CH4, N2 and trace specie concentrations of HCN, NH3, and

H2S. When the gas chromatograph is not used, gas fractions

of C02, CO, and 02 are supplied by the analyzers. Gas

fraction N2 is assumed in this case to be:

20

N2 = 1.0 - C02 - CO - 02

Also, gas compositions of H2, CH4, HCN, NH3, and H2S are

assumed to be zero when they are not available.

The system unknowns are gas fractions S02 and H20,

the flue gas output flow rate, the coal input flow rate, and

the flue solids output flow rate. Gas fraction S02 is

unknown because the GCC does not report it and the S02

analyzer is not used. Gas fraction H20 is unknown because

the flue sample is quenched with water and then refrigerated

to remove the majority of moisture within the sample. The

flue gas and solids output rates are unknown since no device

is installed to measure them; likewise, the coal input flow

rate is not measured.

The calculation path for determining the unknowns

depends on the stoichiometric operating conditions of the

furnace. Gas fractions S02 and H20 and the flue gas output

flow rate are calculated unconditionally. Either the coal

input flow rate or the flue solids output flow rate are

calculated, depending on whether conditions are fuel lean or

fuel rich. During fuel lean conditions, the coal input flow

rate is computed and the flue solids output rate, on an

ash-free basis, is assumed zero. During fuel rich

conditions, the coal input flow rate, obtained during fuel

lean calculations, is used to compute the flue solids output

flow rate.

21

Fuel lean or fuel rich operating conditions are

determined by examining the ratio of 02/C0 in the flue gas

(Wendt, 1981). When the ratio exceeds 0.5, conditions are

defined to be fuel lean; likewise, conditions are defined

to be fuel rich when the ratio is less than 0.5. Although

other methods could be used to determine stoichiometric

conditions, the 02/C0 ratio is one of the most sensitive

inicators (Takacs, 1977).

A multivariable Newton-Raphson algorithm (see

Carnahan, Luther, Wilks, 1979) is used to solve for the

unknowns because the system of equations is non-linear. The

non-linearity arises because the flue gas output rate and

flue gas fractions S02 and H20 are unknown. Furthermore,

because the flue sample is both quenched with H20 and

refrigerated to remove much of the moisture, the measured

flue gas fractions do not represent the actual flue gas

fractions. A correction factor is applied to measured flue

gas fractions to transform them to a moisture included

presampled basis. The correction factor adds another degree

of non-linearity since the gas fraction H20 is involved

within the factor (see Appendix A).

The equations used to solve for the system unknowns

are derived from mass balances of carbon, hydrogen,

nitrogen, and sulfur and include flue gas moisture

correction. The system of equations and the accompanying

coefficient matrix are listed in Appendix B. The

22

Newton-Raphson algorithm normally requires three to six

iterations to achieve a global relative convergence of one

part per million.

The results reported to the teletype include a

summary of the furnace operating conditions. As shown in

Table 3, the summary includes coal analysis, flue solids

analysis and flue gas analysis broken down into major and

minor constituents. Flow rates of coal, air, flue gas and

solids are reported on the same basis as their respective

stream analyses. Stoichiometric air and the stoichiometric

ratio are also reported. A stoichiometric ratio greater

than unity indicates fuel lean conditions while a ratio less

than one indicates fuel rich conditions. The ratio is

defined (Wendt, 1981) as the amount of oxygen supplied to

the minimum amount of oxygen required for complete

theoretical combustion of the fuel.

The Data Adjustment Problem

In most systems which are over-defined, i.e. the

number of independent equations exceeds the number of

unknowns, the solution set depends on which equations are

used to define the calculation path (White and Winslow,

1979, 1977). Assuming that the applied equations correctly

describe the system behavior, the dependence of the solution

set on the calculation path is due to error within the data.

Since the system is over-defined, an optimal solution may be

2.3

Table 3: Typical Analysis Summary of Furnace Data

*** RECORD 1 PROBE 4 3/11/81 4:17s 9 C0NSI8. FUEL RICH

***

***

***

***

***

[=] LB/HR

COAL INPUT RATE = 6.025E+00

FLUE SOLIDS OUTPUT - 1.217E+00

[=] SCFH

FLUE GAS OUTPUT = 9.305E+00 AIR INPUT RATE = 8.286E+00

TRANSPORT AIR - 1.558E+00 SECONDARY AIR » 6.728E+00

STAGED AIR » Q.000E-01

STOICHIOMETRIC AIR » 1.142E+01

STOICHIOMETRIC RATIO = 0.73

KG/S

7.598E-04 I.535E-04

N**3/S

4.392E-03 3.911E-03

7.354E-04 3.176E-03 0.000E-01

5.390E-03

COAL FLUE SOLIDS FLUE 6AS FLUE GAS PERCENTAGES PERCENTAGES PERCENTAGES TRACE PPNV

68.73 C 55.60 C 12.64 C02 480.00 NO 5.36 H 0.01 H 5.56 CO 14.00 HCH 10.03 0 0.54 N 0.00 02 0.00 H2S 0.97 S 0.00 S 0.00 CH4 1150.91 S02 1.56 N 43.86 ASH 1.50 H2 98.00 NH3 4.49 H20 9.62 H20 8.86 ASH 70.52 N2

24

obtained by adjusting the data to minimize the discrepancies

due to the calculation path. Resultant adjustments are

assumed to represent error within the data so that data with

large relative adjustments may help identify error sources.

A sum of squares optimization functional is defined,

which includes both discrepancy contributions and adjustment

contributions (White, 1977). Discrepancy contributions are

defined from "calculated" variables; "calculated" variables

are those variables for which data are available and are

calculated from the independent equations or from the tight

system constraints. Adjustment contributions are defined

from "search" variables; "search" variables are those

variables for which data are available and which are not

calculated but adjusted such that the sum of squares

functional is minimized. The sum of squares functional

takes the following form:

i ~ni a j n A

SSQ = £ 1 (C. - C.)2 + Z 1 (S. - S.) 1=1 w. 1 ;=i w. >sf >

\ \ J J

W. = Weighting factor for variable i A

C. = Calculated value for "Calculated" variable i A

S. = Adjusted value--for "Search" variable J ) '

C. = Data for "Calculated" variable i

S. = Data for "Search" variable J J '

m = Number of "Calculated" variables

n = Number of "Search" variables

25

In the furnace application, there are four unknowns,

six independent equations, and three tight constraints. The

four unknowns are flue gas fractions S02 and H20, the flue

gas output flow rate, and either the coal input flow rate or

the flue solids output flow rate. The six equations are

component balances for carbon, hydrogen, nitrogen, sulfur

and oxygen and the equilibrium of the water-gas-shift

reaction. The three constraints are that the sum of

fractions equal one within the coal, flue gas, and flue

solids flow streams.

"Calculated" variables are flue gas fractions CO,

H2, and N2 and coal mass fraction C and flue solids fraction

C. Flue gas fractions CO and H2 are calculated by including

the balance of oxygen and from the water-gas-shift

equilibrium during calculation of the unknowns. "Search"

variables and "calculated" variables are listed in Table 4.

"Search" and "calculated" variables do not contribute to the

sum of squares functional if no data is available for them.

The form of the sum of squares functional suggests

quasi-quadratic behavior of the response surface (White,

1977). Coggin's method (see Kuester and Mize, 1977) for

finding an optimum in one-space fits a quadratic to three

points straddling the optimum and estimates the location of

the optimum from the quadratic optimum. The algorithm

proceeds, see Figure 6, as follows. A step is taken from

point 1 to point 2; if an increase is observed then the

2 6

Table 4: Furnace "Search" and "Calculated" Variable Sets

"Search" Variables

Flue Gas Mole Fractions:

C02, 02, HCN, NH3, NO, H2S

Flue Solids Mass Fractions:

H, S, N

Coal Mass Fractions:

H, N, S, 0, H2O

Temperature at the Probe:

T

Air Input Flow Rate:

Qi + Q2 + Q3

Coal Input Flow Rate:

Wi

"Calculated" Variables


CO, Hz, N2

Flue Solids Mass Fraction:

C

Coal Mass Fraction:

C

27

1 Starting Point 2 First Step Rejected

. 3 Direction Reversed 4 Move Accelerated

+2 A -A a c o o c if

CO a> h. O 3 cr CO

H— o

E 3 CO

Quadratic Minimum True Minimum

Search Variable : i

Fi gure 6 : Coggin Data Adjustment in One Space

28

step direction is reversed to obtain point 3. If the

functional decreases, then the step size is doubled until

the sum of squares functional increases, point 4. A

parabola is fit to the three points with the least

functional values. The minimum of the parabola becomes the

next point for a successive parabola. Parabolas are

consecutively fit until relative convergence is attained at

the functional minimum.

Following two global applications of the Coggin

algorithm, a vector is formed between the current and the

previous locations in search space. The Coggin algorithm is

then applied to an acceleration factor to allow minimization

along the hypervector (White, 1977). Figure 7 illustrates

the procedure in two-space. The starting point, i-2, is

obtained from the initialized search data. After two global

applications of the Coggin algorithm points i-1 and i are

obtained. A vector, P, is formed from the two points which

points toward the optimum. The Coggin algorithm applied

along the vector yields point i+1. The algorithm is

continued by stepping off the vector using another global

Coggin application and forming a new vector from the

previous and current locations. This sequence is continued

until global convergence is achieved.

Search Variable:

Figure 7: Coggin Data Adjustment in Two Space

30

Because all "search" variables are initialized to

their data values prior to data adjustment, the sum of

squares functional initially, contains only discrepancies

within the "calculated" variables. By adjusting "search"

variables from their data values, the sum of squares is only

decreased when the magnitude of the discrepancy decrease is

greater than the magnitude of the adjustment of the "search"

variable.

Whenever data adjustment is practiced to minimize

discrepancies among data it is usually assumed that

variables with large resultant adjustments are most suspect

for being erroneous. Furthermore, it is assumed that error

within reported data is distributed normally to adjustments

in all variables (White, 1979, 1977, Winslow, 1980, Smith,

1973, Davidson, 1977). Given these premises, an analysis of

adjustments should yield some information about error

sources within the combustion data.

By treating adjustments as samples from an error

population, t-values can be computed for each variable

contributing to the sum of squares functional (Himmelblau,

1969). The hypothesis that an adjustment is not a member of

the sample population is tested by performaing an outlier

test. The outlier criterion proposed by Anscombe (1960)

examines t-values obtained from the sample and compares them

against a rejection constant. If a t-value is greater than

31

the rejection constant, the variable is flagged . as an

outlier and becomes suspect for being an error source. The

possible error from accepting the hypothesis is a type 1

error, i.e. erroneously rejecting a member of the sample.

The rejection constant is a function of the degree

of confidence to be applied to the test, the degrees of

freedom of the sample, the sample mean and standard

deviation. Anscombe gives two formulas for the rejection

constant. The first, which is poorly conditioned from a

computational standpoint, is:

Where:

1-a = Confidence of the test 1 v = Degrees of freedom of the sample

t = Student-t variable ("Student", 1927)

n = Sample size

C = Anscombe rejection constant

The second formula which is better conditioned is given by:

a = I..(( v - 1 )> JL ) x 2 2

I = Incomplete Beta Function (Pearson, 1954) X X = ( v2 - n C2 )

v 2

In determining the rejection constant, the second formula is

used.

CHAPTER 4

INVESTIGATION

Adjustment Verification

The ability of the data adjustment algorithm to

identify and correct error within a furnace data set was

tested using data sets with known error sources. A

consistent set of representative data was generated and used

as a standard for error introduction. Error was introduced

by perturbing "search" and "calculated" variables prior to

applying data adjustment. The resulting adjustments were

compared with the introduced error to evaluate the merit of

the adjustment algorithm.

The data set used as the standard for subsequent

data perturbations not only needed to be consistent but also

needed to be representative of experimental operating

conditions. A data set obtained by J. W. Glass (1981)

while operating the furnace under fuel rich stoichiometric

conditions was used as an initial guess of obtaining a

consistent set. The consistent set was obtained from the

experimental set by applying the adjustment algorithm to the

32

33

experimental set. The resultant adjusted set became the

consistent standard and is shown in Table 5.

Members of the search set were perturbed from their

consistent values by fractions of the consistent values. To

avoid unreasonable data sets, no variable was perturbed more

than 20 percent. In the event that a variable to be

perturbed was a mole/mass fraction, the tight constraint

that the sum of fractions equal 1.0 was enforced. Also the

loose constraints that mole/mass fractions be nonnegative

and less than or equal to 1.0 were enforced.

The following formula was used to perturb members of

the search set:

X. = ( 1.0 + e ) X. J J

Where: /s X. = Perturbed "Search" Variable j

X. = Consistent Value of "Search" Variable ; J

e = Fractional Perturbation

In the event that X. is a mole/mass fraction, the tight J

constraint:

E X . = 1 . 0 )

is enforced by distributing the perturbation over the

remaining fractions of the stream. Defining a perturbation

distribution factor, 6 , given by:

34

Table 5: Consistent Fuel Rich Data Set and Analysis

*** RECORD 1 PROBE 4 3/11/81

M* ITERATION • 0 [=] LB/HR

*** COAL INPUT RATE » 6.025E+00

*** FLUE SOLIDS OUTPUT * 1 -217E+00

[=•] SCFN

*** FLUE GAS OUTPUT = 9.305E+00

#«• AIR INPUT RATE * 8.286E+00

TRANSPORT AIR = 1.558E+00

SECONDARY AIR • 6.728E+00 STAGED AIR = O.OOOE-OI

*** STOICHIOMETRIC AIR = 1.142E+01

STOICHIOHETRIC RATIO » 0.73

COAL FLUE SOLIDS FLUE GAS FLUE GAS PERCENTAGES PERCENTAGES PERCENTAGES TRACE PPMV

68.73 C 55.60 C 12.64 C02 480.00 NO 5.36 H 0.01 H 5.56 CO 14.00 HCN 10.03 0 0.54 N 0.00 02 0.00 H2S 0.97 S 0.00 S 0.00 CH4 1150.91 S02 1.56 N 43.86 ASH 1.50 H2 98.00 NH3 4.49 H20 9.62 H20 8.86 ASH 70.52 N2

4:17: 9 CONSIS. FUEL RICH

K6/S

7.598E-04 1.535E-04

H**3/S

4.392E-03

3.91IE-03

7.354E-04 3.176E-03 O.OOOE-OI

5.390E-03

35

Table 5--Continued

D.O.F. 19 HEANs 1.356E-07 SDEVi ! 2.933E-07 CONFIDi

HASS FRACTIONS OF COAL:

RAU DATA ADJUSTED DATA Z ADJUSTHENT T VALUE 7.54120E-01 C 7.S4120E-01 0.0 0.348 S.88441E—02 H S.88441E-02 0.0 1.072 1.09998E-01 0 1.09998E-01 0.0 0.462 1.06399E-02 S 1.06399E-02 0.0 0.376 1.71074E-02 N 1.71074E-02 0.0 0.421 4.92901E-02 H20 4.92901E-02 0.0 0.462

HOLE FRACTIONS OF FLUE GASi

RAU DATA ADJUSTED DATA X ADJUSTHENT T VALUE 1.26361E-01 C02 1.26361E-01 0.0 0.462 5.56019E-02 CO 5.56019E-0 2 0.0 2.606 4.79999E-04 NO 4.79999E-04 0.0 0.462 t.40000E-05 HCN 1.40000E-05 0.0 0.462 9.79998E-05 NH3 9.79998E-05 0.0 0.374 1.49339E-02 H2 1.49539E-02 0.0 2.840 7.05163E-01 N2 7.05163E-01 0.0 0.458

MASS FRACTIONS OF FLUE SOLIDSi

RAU DATA ADJUSTED DATA I ADJUSTHENT T VALUE 9.90300E-0t C 9.90300E-01 0.0 0.300 1.60000E-04 H 1.60000E-04 0.0 0.348 9.S4000E-03 N 9.S4000E-03 0.0 0.461

TEMPERATURE AT PROBE: [»] KELVIN

RAU DATA ADJUSTED DATA 1 ADJUSTHENT T VALUE t.56620E+03 1.56620E+03 0.0 0.266

SOLIDS FLOU RATESi I =] LB/HR

RAU DATA ADJUSTED DATA Z ADJUSTMENT T VALUE 5.49137E+00 COAL 5.49137E+00 0.0 0.462

GAS FLOU RATESi i [=] SCFH

RAU DATA ADJUSTED DATA Z ADJUSTMENT T VALUE 1.55800E+00 TRNS 1.55800E+00 0.0 0.462

OUTLIER?

OUTLIER?

OUTLIER?

OUTLIER?

OUTLIER?

OUTLIER?

6.72782E+00 SECD 6.72782E+00 0.0 0.462

36

6 = ( 1.0 - X. ) / ( 1.0 - X. ) , J J

the sum of fractions within a perturbed stream takes the

form:

6 E X . + ( 1 . 0 + e ) X . = 1 . 0 , i j * ; .

The loose constraints are enforced by assuring the following

inequalities are maintained.

1.0 > X. > 0.0 J

1.0 > X. > 0.0 J

Furthermore, e and 6 are constrained by the following

arbitrary limits:

1 . 2 > 6 > 0 . 8

-0.2 > E > 0.2

Perturbed data sets were analyzed for consistency

using one and two degrees of over-definition. One degree of

over-definition was obtained by including the oxygen balance

but not water-gas-shift equilibrium. Two degrees of

over-definition is obtained using both relations. The

sensitivity of the adjustment algorithm to error within the

data decreased when only one degree of over-definition was

used. The number of interactions required for convergence

also decreased when one instead of two degrees of

over-definition was used.

37

The Consistency Results

The results of the consistency analysis classified

the search set into two catagories according to adjustment

sensitivity. Table 6 groups the variables into their

respective catagories. Sensitive variables are those

'wariables which caused significant, greater than 1%,

adjustments when perturbed by 20% of their consistent

values. Similarly, insensitive variables caused

insignificant adjustments when perturbed to their maximun

extents.

As expected, perturbations within flue gas trace

species HCN, NH3 and NO did not affect the adjustment

algorithm since their contributions to the mass balance are

insignificant. Likewise, mass fractions N and S within the

coal and mass fractions H and N within the flue solids were

insensitive to data perturbations. Mass fraction C of the

flue solids could not be perturbed significantly since its

consistent value is close to one. The resultant adjustments

when mass fraction N within the coal is perturbed from its

consistent value by +20% are shown in Table 7. This table

typifies resultant adjustments when the class of insensitive

variables is perturbed.

Fractions H2S and S within the flue gas and flue

solids, respectively, were not tested since no data were

available for them. The consistency response to their

38

Table 6: Adjustment Classification of "Search" and "Calculated" Variables

Sensitive Variables


C02, CO, Hz, N2


T


C, H, 0, H20


QI + Q2 + Q3


Wi

Insensitive Variables


HCN, NHs, NO

Flue Solids Mass Fractions:

C, H, N


N, S

3 9

Table 7: Data Adjustment of Coal Nitrogen Mass Fraction

RECORD 55 PROBE 4 3/16/81 0:54:25

C = ] LB/HR KG/S

*** COAL INPUT RATE s 6.025E+00 7.598E-04 *** FLUE SOLIDS OUTPUT s 1.200E+00 1.514E-04

C = ] SCFH N**3/S

*** FLUE GAS OUTPUT =

9.308E+00 4.393E-03 *** AIR INPUT RATE

= 8.28AE+00 3.911E-03

TRANSPORT AIR - 1.558E+00 7.354E-04 SECONDARY AIR = 6.728E+00 3.176E-03

STAGED AIR = O.OOOE-OI 0.000E-01

*** STOICHIOMETRIC AIR = 1.138E+01 5.373E-03

STOICHIOHETRIC RATIO s 0.73

COAL FLUE SOLIDS FLUE GAS FLUE GAS PERCENTAGES PERCENTAGES PERCENTAGES TRACE PPNV

68.49 C 54.99 C 12.64 C02 480.13 NO 5.35 H 0.01 H 5.56 CO 14.00 HCN 9.98 0 0.53 N 0.00 02 0.00 H2S 0.97 S 0.00 S 0.00 CH4 1150.71 S02 1.86 N 44.47 ASH 1.50 H2 98.03 NH3

4.48 H20 9.59 H20 8.86 ASH 70.54 N2

Table 7--Continued

D.O.F. 19 MEAN: 1.356E-04 SDEV : 2.059E-04 CONFIDENCE : 0.950


RAU DATA ADJUSTED DATA X ADJUSTHENT T VALUE OUTLIER? 7.51474E-01 C 7.51455E-01 0.0 0.534 5.87366E-02 H 5.87524E-02 0.0 0.646 1.09544E-01 0 1.09546E-01 0.0 0.566 1.06414E-02 S 1.06414E-02 0.0 0.639 2.04483E-02 N 2.04482E-02 0.0 0.636 4.91551E—02 H20 4.91567E-02 0.0 0.504

HOLE FRACTIONS OF FLUE GAS:

RAU DATA ADJUSTED DATA 1 ADJUSTHENT T VALUE OUTLIER? 1.26396E-01 C02 1.26301E-01 0.1 2.967 YES 5.56173E-02 CO 5.56356E-02 0.0 0.937 4.80132E-04 NO 4.80132E-04 0.0 0.653 1.40039E-05 HCN 1.40039E-05 0.0 0.658 9.80270E-05 NH3 9.80270E-05 0.0 0.656 1.49580E-02 H2 1.49507E-02 0.0 1.707 7.05358E-01 N2 7.05347E-01 0.0 0.578

HASS FRACTIONS OF FLUE SOLIDS:

RAU DATA ADJUSTED DATA X ADJUSTHENT T VALUE OUTLIER? 9.90300E-01 C 9.90300E-01 0.0 0.658 1.60000E-04 H 1.60000E-04 0.0 0.658 9.54000E-03 N 9.54000E-03 0.0 0.658

TEHPERATURE AT PROBE: [=] KELVIN

RAU DATA ADJUSTED DATA X ADJUSTHENT T VALUE OUTLIER? 1.56620E+03 1.56601E+03 0.0 0.078

SOLIDS FLOU RATES: C =] LB/HR

RAU DATA ADJUSTED DATA X ADJUSTHENT T VALUE OUTLIER? 5.49137E+00 COAL 5.49311E+00 0.0 0.877

GAS FLOU RATES: CO SCFH

RAU DATA ADJUSTED DATA X ADJUSTHENT T VALUE OUTLIER? 1.55800E+00 TRNS 1.55790E+00 0.0 0.356 6.72782E+00 SECD 6.72594E+00 0.0 0.699

4 1

T a b l e 7 - - C o n t i n u e d

RECORD 55 PROBE 4 3/16/81 0:54:25

*** ITERATION = 14 C=3 LB/HR K6/S

*** COAL INPUT RATE S 6.027E+00 7.601E-04 *** FLUE SOLIDS OUTPUT = 1.204E+00 1.519E-04

C=] SCFM H**3/S

FLUE GAS OUTPUT - 9.306E+00 4.392E-03 *** AIR INPUT RATE = 8.284E+00 3.910E-03

TRANSPORT AIR = 1.558E+00 7.353E-04 SECONDARY AIR = 6.726E+00 3.175E-03

STAGED AIR = O.OOOE-OI O.OOOE-OI

*** STOICHIOMETRIC AIR = 1.139E+01 5.374E-03

STOICHIOMETRIC RATIO s 0.73

COAL FLUE SOLIDS FLUE GAS FLUE GAS PERCENTAGES PERCENTAGES PERCENTAGES TRACE PPHV

68.49 C 55.11 C 12.63 C02 480.13 NO 5.35 H 0.01 H 5.56 CO 14.00 HCN 9.98 0 0.53 N 0.00 02 0.00 H2S 0.97 S 0.00 S 0.00 CH4 1151.33 302 1.86 N 44.35 ASH 1.50 H2 98.03 NH3 4.48 H20 9.60 H20 8.86 ASH 70.53 N2

perturbations would be expected to be similar to the

response to insensitive variable perturbations. Flue gas

fraction 02 was not tested since its data value was zero;

whenever data for a variable is zero it is not included in

the search.

The consistency analysis further divided (see Table

8) the sensitive variables into two classes depending on the

ability of the adjustment algorithm to correct error

introduced within the variables. Flue gas fractions C02 and

N2 were the only two variables for which the majority of

error introduced from their perturbations was corrected.

The remaining variables would, in general, be adjusted in

the correct sense to remove perturbation error but not to

the degree that was introduced.

An example of two variables which showed incomplete

adjustment but were still flagged as erroneous are mass

fraction H within the coal and flue gas fraction H2. Both

variables when perturbed upwards +20% from their consistent

values were adjusted such that 25% of the introduced error

was removed (see Tables 9 and 10). The remaining error was

distributed among the other sensitive variables.

Table 8: Adjustment Classification of Sensitive "Search" and "Calculated" Variables

Majority Removal of Introduced Error


C02f N2

Partial Removal of Introduced Error


CO, H2


C, H, 0, H20


T


QI + Q2 + Q3


WI

Table 9: Data Adjustment of Coal Hydrogen Mass Fraction

RECORD 37 PROBE 4 3/16/81 0:37:12 H+20Z

[=] LB/HR KG/S

*** COAL INPUT RATE = 6.025E+00 7.598E-04 FLUE SOLIDS OUTPUT = 1.165E+00 1 .469E-04

C=] SCFH N**3/S

*** FLUE GAS OUTPUT = 9.494E+00 4.481E-03

*** AIR INPUT RATE = 8.286E+00 3.911E-03


STAGED AIR = 0.000E-01 O.OOOE-OI

•«» STOICHIOHETRIC AIR = 1.176E+01 5.S50E-03

STOICHIOHETRIC RATIO = 0.70

COAL PERCENTAGES

FLUE SOLIDS PERCENTAGES

FLUE GAS PERCENTAGES

FLUE GAS TRACE PPNV

67.87 C 6.44 H 9.89 0 0.96 S 1.54 N 4.44 H20 8.86 ASH

53.66 C 0 . 01 K 0.52 N 0.00 S 45.81 ASH

12.38 C02 5.45 CO 0.00 02 0.00 CH4 1.47 H2 11.42 H20 69.11 N2

470.43 NO 13.72 HCN 0.00 H2S

1117.61 S02 96.05 NH3

4 5


D.O.F. 19 HEAN: 1.154E-02 SDEV l 1.580E-02 CONFIDENCE : 0.950

HASS FRACTIONS OF COAL • •

RAU DATA ADJUSTED DATA X ADJUSTHENT T VALUE OUTLIER? 7.44723E-01 C 7.47390E-01 0.4 0.504 7.06626E-02 H 6.76151E-02 4.3 1.999 YES 1.08551E-01 0 1.08922E-01 0.3 0.514 1.05420E-02 S 1.05398E-02 0.0 0.717 1.69089E-02 N 1.69099E-02 0.0 0.727 4.87163E-02 H20 4.86235E-02 0.2 0.610


RAU DATA ADJUSTED DATA X ADJUSTHENT T VALUE

1.23842E-01 C02 1.23425E-01 0.3 0.518 5.44936E-02 CO 5.26326E-02 3.4 1.431 4.70431E—04 NO 4.70407E-04 0.0 0.727

1.37209E-05 HCN 1.37209E-05 0.0 0.730 9.60464E-05 NH3 9.60518E-05 0.0 0.727

1.46558E-02 H2 1.51233E-02 3.2 1.288 6.91107E-01 N2 7.04744E-01 2.0 0.518

OUTLIER?


RAU DATA ADJUSTED DATA X ADJUSTMENT T VALUE OUTLIER? 9.90300E-01 C 9.90300E-01 0.0 0.730 1.60000E-04 H 1.60001E-04 0.0 0.730 9.54000E-03 N 9.54001E-03 0.0 0.730

TEHPERATURE AT PROBE: C=3 KELVIN

RAU DATA ADJUSTED DATA X ADJUSTMENT T VALUE OUTLIER? 1.56620E+03 1.57776E+03 0.7 0.263

SOLIDS FLOU RATES: C=] LB/HR

RAU DATA ADJUSTED DATA X ADJUSTHENT T VALUE OUTLIER? 5.49137E+00 COAL 5.25860E+00 4.2 1.952 YES

GAS FLOU RATES: [-] SCFH

RAU DATA ADJUSTED DATA X ADJUSTHENT T VALUE OUTLIER?

1.55800E+00 TRNS 1.56958E+00 0.7 0.260 A.777A7F+00 RFm A.94374F+00 3.2 1.301


*** RECORD 37 PROBE 4 3/16/81 0:37:12 H+20%

•*» ITERATION = 27 [=3 LB/HR KG/S

••• COAL INPUT RATE = 5.770E+00 7.276E-04 *** FLUE SOLIDS OUTPUT = 1.001E+00 1.262E-04

[=3 SCFM ii*;»3/S

**# FLUE GAS OUTPUT = 9.564E+00 4.514E-03

*** AIR INPUT RATE = 8.513E+00 4-018E-03


STAGED AIR = 0.000E-01 0.000E-01

*** STOICHIOMETRIC AIR - 1.118E+01 5.276E-03


COAL FLUE SOLIDS FLUE GAS FLUE GAS

PERCENTAGES PERCENTAGES PERCENTAGES TRACE PPHM

68.12 C 48.44 C 12.34 C02 470.41 NO 6.16 H 0.01 H 5.26 CO 13.72 HCN 9.93 0 0.47 N 0.00 02 0.00 H2S 0.96 S 0.00 S 0.00 CH4 1062.12 S02

1.54 N 51.08 ASH 1.51 H2 96.05 NH3 4.43 H20 10.24 H20 8.86 ASH 70.47 N2

4 7

T a b l e 1 0 : D a t a A d j u s t m e n t o f F l u e G a s H y d r o g e n M o l e F r a c t i o n

*** RECORD 1? PROBE 4 3/11/81 4:23:27

[ = ] LB/HR KG/S

*** COAL INPUT RATE s 6.025E+00 7.598E-04 *** FLUE SOLIDS OUTPUT = 1.218E+00 1.536E-04

[ = 3 SCFM H*=»3/S

*** FLUE GAS OUTPUT s 9.304E+00 4.392E-03 *** AIR INPUT RATE = 8.286E+00 3.911E-03

TRANSPORT AIR s 1.558E+00 7.354E-04 SECONDARY AIR = 6.728E+00 3.176E-03

STAGED AIR = 0.000E-01 0.000E-01

«** STOICHIOMETRIC AIR = 1.142E+01 5.390E-03

STOICHIOMETRIC RATIO s 0.73



4 8

T a b l e 1 0 - - C o n t i n u e d

D.O.F. 19 MEAN: 1.091E—02 SDEV: 1.435E-02 CONFIDENCE: 0.950

HASS FRACTIONS OF COAL • •

RAU DATA ADJUSTED DATA I ADJUSTMENT T VALUE OUTLIER? 7.54120E-01 C 7.52389E-01 0.2 0.600

5.88441E-02 H 6.05216E-02 2.9 1.226 1.09998E-01 0 1.09935E-01 0.1 0.720 1.06399E-02 S 1.06392E-02 0.0 0.755 1.71074E—02 N 1.71046E-02 0.0 0.749

4.92901E-02 H20 4.94113E-02 0.2 0.589


RAU DATA ADJUSTED DATA X ADJUSTMENT T VALUE OUTLIER? 1.26373E-01 C02 1.21917E-01 3.5 1.697 5.55642E-02 CO 5.71697E-02 2.9 1.253 4.81422E-04 NO 4.81417E—04 0.0 0.760 1.40415E-05 HCN 1.40415E-05 0.0 0.760 9.82904E-05 NH3 9.82847E-05 0.0 0.756 1.80533E-02 H2 1.73440E-02 3.9 1.978 YES 7.05183E-01 N2 6.99730E-01 0.8 0.221


RAU DATA ADJUSTED DATA % ADJUSTMENT T VALUE OUTLIER? 9.90300E-01 C 9.90300E-01 0.0 0.760 1.60000E-04 H 1.59998E-04 0.0 0.759 9.54000E-03 N 9.54008E-03 0.0 0.760

TEMPERATURE AT PROBE: [=] KELVIN

RAU DATA ADJUSTED DATA I ADJUSTMENT T VALUE OUTLIER? 1.56620E+03 1.55197E+03 0.9 0.127

SOLIDS FLOU RATES: C=] LB/HR

COAL •RAU DATA 5.49137E+00

ADJUSTED DATA 5.66140E+00

X ADJUSTMENT 3.1

T VALUE 1.398

OUTLIER?

GAS FLOU RATES: [=3 SCFH

RAU DATA ADJUSTED DATA % ADJUSTMENT T VALUE OUTLIER? 1.55800E+00 TRNS 1.54830E+00 0.6 0.327 6.72782E+00 SECD 6.54907E+00 2.7 1.091

T a b l e I P — C o n t i n u e d

*•* RECORD 19 PROBE 4 3/11/81 4:23:27 H2+20*

*** ITERATION = 22 [=3 LB/HR KG/S

*** COAL INPUT RATE = 6.212E+00 7.834E-04 **• FLUE SOLIDS OUTPUT = 1.461E+00 1.842E-04

C=] SCFH M**3/S

*** FLUE GAS OUTPUT = 9.164E+00 4.326E-03 *** AIR INPUT RATE = 8.097E+00 3.822E-03

TRANSPORT AIR * 1.548E+00 7.308E-04 SECONDARY AIR » 6.549E+00 3.091E-03


•** STOICHIOHETRIC AIR = 1.182E+01 5.577E-03


COAL PERCENTAGES

FLUE SOLIDS PERCENTAGES

FLUE GAS PERCENTAGES

FLUE GAS TRACE PPHV

68.57 C 5.52 H

10 .02 0 0.97 S 1.56 N 4.50 H20 8.86 ASH

61.71 C 0.01 H 0.59 N 0.00 S 37.68 ASH

12.19 C02 5.72 CO 0.00 02 0.00 CH4 1.73 H2 10.20 H20 69.97 N2

481.42 NO 14.04 HCN 0.00 H2S

1204.62 S02 98.28 NH3

j

I 50

Perturbations within flue gas fractions C02 and N2

were mostly corrected as shown in Tables 11 and 12. In the

case of N2 when perturbed from its consistent value by +1%,

93% of the introduced error was removed by the adjustment

algorithm. N2 was not flagged as an outlier, however, since

the C02 adjustment was greater than the N2 adjustment; this

result is due primarily to the perturbation distribution

factor which altered C02 from its consistent value by -3%.

When flue gas fraction C02 was perturbed from its

consistent value by +10% and the remaining flue gas

fractions were perturbed downwards from their consistent

values by -1.5%, the algorithm corrected 90% of the

perturbation error. The error introduced from the

perturbation distribution factor was corrected almost

entirely for fractions H2 and N2 and partially for fraction

CO.

5 1

T a b l e 1 1 : D a t a A d j u s t m e n t o f F l u e G a s C a r b o n D i o x i d e M o l e F r a c t i o n

*** RECORD 6 PROBE 4 3/ 7/81 18:13:22 C02+10Z

***

***

***

***

[=] LB/HR

COAL INPUT RATE = 6.025E+00 FLUE SOLIDS OUTPUT = 9.354E-01

[=] SCFH

FLUE GAS OUTPUT =

AIR INPUT RATE = 9.442E+00

8.286E+00

TRANSPORT AIR = 1.558E+00 SECONDARY AIR = 6.728E+00

STAGED AIR = 0.000E-01

*** STOICHIOHETRIC AIR = 1.142E+01


KG/S

7.598E-04 1.180E-04

N**3/S

4.457E-03 3.911E-03

7.354E-04 3.176E-03 0.000E-01

5.390E-03



52

T a b l e 1 l - - C o n t i n u e d

D.O.F. 19 MEAN: 7.288E-03 SDEU: : 1.809E-02 CONFIDENCE) ! 0.950


RAU DATA ADJUSTED DATA Z ADJUSTMENT T VALUE OUTLIER? 7.54120E-01 C 7.54172E-01 0.0 0.399 5.88441E-02 H 5.82501E-02 1.0 0.1S5 1.09998E-01 0 1.10506E-01 0.5 0.148 1.06399E-02 S 1.06343E-02 0.1 0.374 1.71074E-02 N 1.71036E-02 0.0 0.391 4.92901E-02 H20 4.93341E-02 0.1 0.354


RAU DATA ADJUSTED DATA X ADJUSTMENT T VALUE OUTLIER? 1.38977E-01 C02 1.27713E-01 8.1 4.078 YES 5.47910E-02 CO 5.48559E-02 0.1 0.337 4.69923E-04 NO 4.69874E-04 0.0 0.397 1.39977E-05 HCN 1.39977E-05 0.0 0.403 9.69840E-05 NH3 9.69852E-05 0.0 0.402 1.47976E-02 H2 1.45638E-02 1.6 0.470 6.94985E-01 N2 7.06372E-01 1.6 0.503

MASS FRACTIONS OF FLUE SOLIDS:

RAU DATA ADJUSTED DATA I ADJUSTMENT T VALUE OUTLIER? 9.90300E-01 C 9.90300E-01 0.0 0.403 1.60000E-04 H 1 .60001E-04 0.0 0.403 9.54000E-03 N 9.S4012E-03 0.0 0.402

TEHPERATURE AT PRODE: [=2 KELVIN

RAU DATA ADJUSTED DATA 1 ADJUSTMENT T VALUE OUTLIER? 1.56620E+03 1.55922E+03 0.4 0.156

SOLIDS FLOU RATESt C x] LD/HR


GAS FLOU RATES : C=] SCFH

RAU DATA ADJUSTED DATA X ADJUSTHENT T VALUE OUTLIER? 1.55800E+00 TRNS 1.55945E+00 0.1 0.351 6.72782E+00 SECD 6.75529E+00 0.4 0.177

5 3

T a b l e l l - - C o n t i n u e d

*** RECORD 6 PROBE 4 3/ 7/81 18:13:22

$** ITERATION = 30 C=3 LB/HR KG/S

$**

*** COAL INPUT RATE =

FLUE SOLIDS OUTPUT * 5.993E+00 1.175E+00

7.558E-04 1.481E—04

C=1 SCFH M**3/S

***

*** FLUE GAS OUTPUT = AIR INPUT RATE =

9.321E+00 8.315E+00

4.400E-03 3.925E-03

TRANSPORT AIR = SECONDARY AIR »

STAGED AIR =

1.559E+00 6.755E+00 O.OOOE-Ot

7.361E-04 3.189E-03 O.OOOE-OI

*** STOICHIOMETRIC AIR =

STOICHIOHETRIC RATIO -

1.133E+01

0.73

5.349E-03


68.74 C 54.26 C 12.77 C02 469.87 NO 5.31 H 0.01 H 5.49 CO 14.00 HCN 10.07 0 0.52 H 0.00 02 0.00 H2S 0.97 S 0.00 S 0.00 CH4 1142.17 S02 1.56 N 45.21 ASH 1.46 H2 96.99 NH3 4.50 H20 9.48 H20 8.86 ASH 70.64 N2

T a b l e 1 2 : D a t a A d j u s t m e n t o f F l u e G a s N i t r o g e n M o l e F r a c t i o n

*** RECORD 24 PROBE 4 3/11/81 4:30:27

C =3 LB/HR KG/S

*** COAL INPUT RATE s 6.025E+00 7.598E-04 *** FLUE SOLIDS OUTPUT = 1 .333E+00 1 .682E-04

C = ] SCFH N**3/S

*** FLUE GAS OUTPUT — 9.248E+Q0 4.365E-03 *** AIR INPUT RATE = 8.286E+00 3.911E-03

TRANSPORT AIR s 1.558E+00 7.354E-04

SECONDARY AIR =

6.72BE+00 3.176E-03


*** STOICHIOHETRIC AIR = 1.142E+01 5.390E-03

STOICHIOHETRIC RATIO s 0.73

COAL FLUE SOLIDS FLUE GAS FLUE GAS

PERCENTAGES PERCENTAGES PERCENTAGES TRACE PPNV

68.73 C 59.39 C 12.29 C02 468.13 NO

5.36 H 0.01 H 5.41 CO 13.94 HCN

10.03 0 0.57 N 0.00 02 0.00 H2S

0.97 S 0.00 S 0.00 CH4 1157.95 S02

1.56 H 40.03 ASH 1.45 H2 95.62 NH3

4.49 H20 9.73 H20

8.86 ASH 70.95 N2

Table 12--Continued

55

D.O.F. 19 HE AN: 2.831E-03 SDEV : 6.722E-03 CONFIDENCE : 0.950


RAU DATA ADJUSTED DATA I ADJUSTHENT T VALUE OUTLIER? 7.54120E-01 C 7.54081E-01 0.0 0.413 5.88441E-02 H 5.91155E-02 0.5 0.265 1 .09998E-01 0 1.09781E-01 0.2 0.127 1.06399E-02 S 1.06423E-02 0.0 0.388 1.71074E-02 N 1.71088E-02 0.0 0.409 4.92901E—02 H20 4.92719E-02 0.0 0.366


RAU DATA ADJUSTED DATA X ADJUSTHENT 7 VALUE OUTLIER?

1 .22908E-01 C02 1.26614E-01 3.0 4.064 YES 5.40837E-02 CO 5.40587E-02 0.0 0.353

4.68127E-04 NO 4.68148E-04 0.0 0.415 1.39442E-05 HCN 1.39442E-05 0.0 0.421 9.56175E-05 NH3 9.56171E-05 0.0 0.421 1.45418E-02 H2 1.46331E-02 0.6 0.512 7.09462E-01 N2 7.05478E-01 0.6 0.414


RAU DATA ADJUSTED DATA X ADJUSTHENT T VALUE OUTLIER? 9.90300E-01 C 9.90300E-01 0.0 0.421 1.60000E-04 H 1.60000E-04 0.0 0.421 9.54000E-03 N 9.53997E-03 0.0 0.421

TEHPERATURE AT PROBE: C=] KELVIN

RAU DATA ADJUSTED DATA X ADJUSTHENT T VALUE OUTLIER? 1.56620E+03 1.56903E+03 0.2 0.153

SOLIDS FLOU RATES: C =] LB/HR


GAS FLOU RATES: : [=0 SCFH

RAU DATA ADJUSTED DATA 1 ADJUSTHENT T VALUE OUTLIER? 1.55800E+00 TRNS 1.55723E+00 0.0 0.348 6.72782E+00 SECD 6.71382E+00 0.2 0.112

T a b l e 1 2 - - C o n t i n u e d

••*** RECORD 24 PROBE 4 3/1 1/81 4:30:27 N2+12

*** ITERATION = 28 [=3 L6/HR KG/S

**4 COAL INPUT RATE s 6.040E+00 7.A17E-04 *** FLUE SOLIDS OUTPUT 3 1.261E+00 1.590E-04

[ = ] SCFH H**3/S

*** FLUE GAS OUTPUT — 9.284E+00 4.382E-03 *** AIR INPUT RATE

= 8.271E+00 3.904E-03

TRANSPORT AIR — 1.557E+00 7.350E-04 SECONDARY AIR = 6.714E+00 3.1A9E-03

STAGED AIR = 0.000E-01 O.OOOE-OI

*** STOICHIOHETRIC AIR =

1.146E+01 5.408E-03

STOICHIOHETRIC RATIO - 0.72


68.73 C 57.00 C 12.66 C02 468.15 NO 5.3? H 0.01 H 5.41 CO 13.94 HCN 10.01 0 0.55 N 0.00 02 0.00 H2S 0.97 S. 0.00 S 0.00 CH4 1156.48 S02 1.56 N 42.44 ASH 1.46 H2 95.62 NH3 4.49 H20 9.75 H20 8.86 ASH 70.55 N2

CHAPTER 5

SUMMARY

The real-time data acquistion and analysis system

applied to the coal-fired reseach furnace provides on-line

experimental data recording and analysis. Data analysis

includes the calculation of unmeasured furnace operating

parameters and data adjustment to obtain consistent data in

lieu of erroneous data. The data adjustment algorithm

imposes additional degrees of definition to a uniquely

defined system of equations so that discrepancies between

data and their calculated values are minimized. The

discrepancies are removed by adjusting the remaining members

of the data set. Following data adjustment, the adjustment

magnitudes are examined for outliers; data with

exceptionally large adjustments become suspect for being

erroneous.

The ability of the adjustment algorithm to identify

and correct error within the data was tested by perturbing a

perfectly consistent set of data. Results indicate that

without imposing additional relations among variables with

57

58

"small" magnitudes, error associated with them cannot be

detected. Variables with "large" magitudes were adjusted in

the correct sense to remove error although the adjustment

magnitude may not reflect the magnitude of the true error.

CHAPTER 6

CONCLUSIONS

The data adjustment algorithm does correct erroneous

data only if the data contributes to a significant degree to

the governing chemical and physical relations. The extent

of data adjustment may not be to the same degree of error

within the data; with additional degrees of system

definition the adjustments should more closely approximate

error within the data. Under these circumstances outlier

analysis of data adjustments would prove more effective in

labeling error sources.

59

CHAPTER 7

RECOMMENDATIONS FOR FURTHER STUDY

Data adustment was applied under conditions of weak

system over-definition since at least four unknowns needed

to be calculated with at most six equations. The error

correction ability of the adjustment algorthm appeared to

decrease significantly with only one degree of system

over-definition. The effect of varying the degree of system

over-definition on the data adjustment could be studied by

imposing additional constraints or treating values obtained

for unknowns as data.

Additional features to the data analysis and

management program should include data base transmission to

the U.C.C. DEC system-10, energy balances, temperature and

specie profiles and residence time analyses. Intrumentation

should be added to obtain on-line static pressures within

air supply lines.

60

APPENDIX A

FLUE GAS MOISTURE CORRECTION

Because flue gas samples are obtained with a water

quenched probe and then refrigerated to remove the majority

of moisture within the sample, measured flue gas fractions

need to be corrected to a presampled moisture included

basis. The correction factor is developed as follows.

N = M e a s u r e d n u m b e r o f m o l e s

n = P r e s a m p l e d n u m b e r o f m o l e s

y . = M e a s u r e d m o l e f r a c t i o n o f s p e c i e i

y n = P r e s a m p l e d m o l e f r a c t i o n o f H 2 0

y ^ N = M e a s u r e d m o l e s o f s p e c i e i

y ^ . N = P r e s a m p l e d m o l e f r a c t i o n o f s p e c i e i

J Y = M o i s t u r e c o r r e c t i o n f a c t o r £ n

A s s u m i n g n o r e a c t i o n w i t h i n t h e p r o b e :

n = N Z y . + n y n , t f H 2 0

S o l v i n g f o r t h e m o i s t u r e c o r r e c t i o n f a c t o r :

? = N = ( 1 . 0 - , y 1 ! ) , i f H 2 0 n E y .

6 1

APPENDIX B

DETERMINATION OF THE COMBUSTOR SOLUTION SET

There are six equations which describe the corabustor

system. They are material balances for carbon, hydrogen,

oxygen, nitrogen, sulfur and thermodynamic equilibrium of

the water-gas-shift reaction. A subset of the available

equations is used to calculate unmeasured variables of the

combustor system.

The combustor system consists of two phases in the

input stream and two phases in the output stream. The input

stream consists of air and coal and the output stream

consists of flue gas and solids. All variables which

describe the system from a material balance standpoint are

shown in Figure 5. Temperature and pressure are not shown

but are also variables considered in conjunction with the

water-gas-shift equilibrium.

The solution set is dependent on the stoichiometry

of the system. If the system is fuel-lean, the output flow

rate of flue solids is assumed to be zero, on an ash free

basis, and the input flow rate of coal is calculated. If

the system is fuel-rich, the output flow rate of flue solids

6 2

63

is calculated and the input flow rate of coal is known from

fuel-lean calculations.

The remaining variables which may be calculated are

the output flow rate of flue gas and flue gas fractions of

S02 and H20. Flue gas fractions of CO and H2 are calculated

during data adjustment. At most, a total of six varibles

must be calculated.

The order of precedence for retaining equations in

the presence of uncertainty or non-convergence is as

follows. Balances of nitrogen, hydrogen, carbon and sulfur

are always imposed. The oxygen balance and water-gas-shift

equilibrium are enforced only during data adjustment. If

variable overflow or nonconvergence occurs during data

adjustment then the water-gas-shift equilibrium is dropped

and the procedure is retried. If a second overflow occurs

during data adjustment then the adjustment algorithm is

aborted. Water-gas-shift equilibrium is not imposed and

flue gas mole fraction H2 is not calculated if no

measurements are available for mole fractions H2 or C02 in

the flue gas.

A multivariable Newton-Raphson algorithm (see

Carnahan, Luther, Wilkes, 1969) is used to solve for the

unknowns because the equations are nonlinear and the speed

of convergence is fast. Convergence is achieved when global

relative convergence of one part per million is attained.

The multivariable case is structured as follows.

6 4

The raultivariable Newton-Raphson algorithm:

It + - * 0 = o

i = I t e r a t i o n C o u n t

z . = S o l u t i o n S e t

f . = E q u a t i o n S e t

4 > . = C o e f f i c i e n t M a t r i x , d > . . = 8 f . ^ I Z )

J

f x = N i t r o g e n B a l a n c e , Z i = Q < *

f 2 = H y d r o g e n B a l a n c e , z 2 = y n

f 3 = C a r b o n B a l a n c e , z 3 = W i ( f u e l l e a n )

z 3 = W 2 ( f u e l r i c h )

f i » = S u l f u r B a l a n c e , Z i » = y 8

f s = O x y g e n B a l a n c e , z 5 = y 2

f 6 = G a s S h i f t E q u i l i b r i u m , z 6 = y i o

N i t r o g e n B a l a n c e :

f i = 0 = m 2 W ? . - x s W i - 1 . 5 8 ( Q i + Q 2 + Q 3 ) +

1 4 1 4

? Q i ( y ^ + y 5 + y s + 2 y 1 2 )

H y d r o g e n B a l a n c e ' :

f2 = 0 = m2W2 ~ (x2 + 2x6)Mi + 2ynQif + 18

£ ( K ( y s + 4 y 6 + 2 y 7 + 3 y 9 + 2 y 1 0 )

C a r b o n B a l a n c e :

f 3 = 0 = m i W ? - XtWt + C Q 4 ( y ! + y 2 + y 5 + y 6 ) 1 2 1 2

S u l f u r B a l a n c e :

f i , = 0 = n u w , - x uMt + £CK( y 7 + y 8 ) 3 2 3 2

O x y g e n B a l a n c e :

f 5 = 0 = - 0 . 4 2 - ( Q i + Q2 + Q 3 ) - ( x _ L + x _6.) + Qnyn + 1 6 1 8

5 Q i ( 2 y i + y 2 + 2 y 3 + y - + 2 y e )

W a t e r - G a s S h i f t E q u i l i b r i u m :

f 6 = 0 = Y n Y ; - e x p ( - A G ° ) yioyiS RT

N i t r o g e n B a l a n c e C o e f f i c i e n t s :

<|)ii = 5(y4 + y5 + yg + 2 yX2)

*12 = ziQ4.(y4 + y5 + ys + 2yX2) l-Yii

* 1 3 = - x _5. ( f u e l l e a n ) ; * x 3 = H i ( f u e l r i c h ) 1 4 1 4

*ii» = -ggQit (yi» + ys + y9 + 2 y 1 2 ) 1-yn

*15 = -55Q «* (y + Y S + Y $ + 2yi2) l-yn

<f>i6 = -g£Qi» (yi» + ys + y9 + 2y12) l-yn

H y d r o g e n B a l a n c e C o e f f i c i e n t s :

* 2 1 = 2 y l x + C ( y 5 + 4 y 6 + 2 y 7 + 3 y 9 + 2 y i 0 )

< J > 2 2 = 2 Q 4 - £ ( K ( y 5 + 4 y e + 2 y 7 + 3 y 9 + 2 y 1 0 ) 1-yn

* 2 3 = - ( x 2 + x _ s _ ) ( f u e l l e a n ) ; 4 > 2 3 = m 2 ( f u e l r i 9

* 2 | » = - € S Q t ( y s + 4 y 6 + 2 y 7 + 3 y 9 + 2 y i 0 ) l-yn

* 2 5 = - i i S - ! t ( y s + 4 y 6 + 2 y ? + 3 y 9 + 2 y 1 0 ) l-yn

* 2 6 = ~ S 5 Q ( v s + 4 y 6 + 2 y 7 + 3 y 9 + 2 y i 0 - 2 ( 1 - y i l-yn e

C a r b o n B a l a n c e C o e f f i c i e n t s :

$31 = ?(yi + YZ + ys + ye)-

$ 3 2 = - € Q o ( y i + y 2 + y 5 + y 6 ) l-yn

< ( > 3 3 = -X j l . ( f u e l l e a n ) ; $33 = nii ( f u e l r i c h ) 12 12

$31* = -g^Qf (yi + y2 + ys + Y E ) l - y n

<p3s = -Mi i (y i + y2 + y 5 + y 6 - ( i - y n ) ) i - y i i c

$36 = -CCQi»(yi + y2 + ys + ye) l-yn

S u l f u r B a l a n c e C o e f f i c i e n t s :

< K i = c ( y 7 + y 8 )

• 12 = -gQu( .y 7 + y 8 ) l-yn

$ 4 3 = - X u ( f u e l l e a n ) ; ( } > 4 . 3 = ( f u e l r i c h ) 3 2 3 2

'K't = (y7 + y8- (l-Vi i)) i-yn 5

5 = - ? ? Q u (.y 7 + ye) i-yn

^te = -£€Q i> (y 7 + ye) l-yn

O x y g e n B a l a n c e C o e f f i c i e n t s :

• s i = y n + 5 ( 2 y i + y 2 + 2 y 3 + + 2 y a )

< ( > 5 2 = Q - - S Q u ( 2 y ! + y 2 + 2 y 3 + y - + 2 y 8 ) 1 - y n

( J > 5 3 = - ( x j . + 2 L s . ) ( f u e l l e a n ) ; 4 > S 3 = 0 ( f u e l r i c h ) 16 18

$ 5 4 = - i £ Q j s . ( 2 y i + y 2 + 2 y 3 + y ^ + 2 y 8 - 2 ( 1 - V n ) ) l - y n 5

4 ) 5 5 = - i i ^ ! i . ( 2 y 1 + y 2 + 2 y 3 + y * + 2 y 8 - ( 1 - V n ) ) l - y n 5

4 * s 6 = - £ €Qk ( 2 y i + y 2 + 2 y 3 + y 4 + 2 y 8 ) l - y n

W a t e r - G a s S h i f t E q u i l i b r i u m C o e f f i c i e n t s

4 > 6 1 = 0

 6 3 = 0

 = y i i y 2

y i o y i ( i - y n )

< J > 6 5 = y i i V 2 + ? y i i y i o y i ( i - y n ) y i o y i

• e e = y i i y 2 r - ? y i i y 2 y i o y i ( i - y n ) y x o y i y i o

APPENDIX C

D.O.E. FURNACE MONITOR USER'S GUIDE

The D.O.E. furnace program was developed to aid

combustion researchers collect and analyze data from the

experimental coal furnace located in the University of

Arizona Chemical Engineering Department. Data collection

includes on-line real-time monitoring of furnace sensors,

bulk data storage, and manual data entry. Data analysis

includes computing unmeasured furnace operating variables

and performing data consistency analyses.

To effectively use the data acquisition and analysis

system, FURNACE, the user must be aware of the capabilities

and limitations of the system. FURNACE provides real-time

monitoring of many operating variables but not all variables

are measured. To obtain reliable mass balance results,

FURNACE expects the user to provide required data which are

not monitored. This guide includes a section on data

collection which details data required for data analysis.

Also included are sections covering system start-up and

shut-down, data retrieval, storage and analysis.

69

7°

The system is configured with a SPC-16 minicomputer,

a Cromemco microcomputer, a KSR 43 teletype, and the furnace

sensors. The furnace sensors monitored by the Cromemco

include thermocouples, differential pressure transducers,

gas analyzers and a Perkin-Elmer gas chromatograph. The

Cromemco microcomputer and the KSR 43 teletype are located

near the furnace and provide dedicated data acquisition and

on-line interaction with the user. Data analysis and bulk

data storage are performed by the SPC-16 minicomputer

located in the Earth Sciences/Mines Real Time Computing

Laboratory (ES/M RTCL, room 324). The SPC-16 also programs

the Cromemco during system start-up; this procedure is

known as down-loading the Cromemco.

System Start-up, Shut-down and Crashes

This section details the start-up, shut-down and

system crash recovery procedures.

System Start-up

I. KSR-43 Teletype.

A. Turn the teletype power on.

B. Set the BAUD rate to 30 cps.

C. Set the Line/Local mode to Line.

D. Connect the communications cable to the Cromemco

port labeled TTY.

71

Cromeraco Microcomputer.

Connect the SPC - 16 communications cable to the

Cromemco port labeled SPC-16.

A. If the Cromeraco power is on, do NOT turn the

power off; if the power is off, go to step II.B.

Type a control-C at the teletype and wait five

seconds for a response at the teletype.

1. If the response '... Enter option1 is printed

then the Cromeraco is operational and requires

no further initialization.

2. Otherwise, turn the Cromeraco power off and go

to step II.B.

B. If the power is off, turn the power on and wait

one minute for the following to be printed at the

teletype:

CROMEMCO SCCHQN

RTOS-16. Rev.7: D.O.E. Furnace

Ootions: 1 = Delta Entrv 5 = Acquire 2 = Search 6 = Analyze 3 = Delete 7 = Calibrate

4 - Exanine 8 = Reload

... Enter option

1. If the above message is printed, the Cromeraco

is operational and requires no further

initialization.

72

2. If the above message is not printed, the

program on the SPC-16 must be resynchonized.

a. Turn the Cromemco power off.

b. Inform the RTCL operator that the SPC-16

furnace task must be restarted.

3. Following confirmation that the SPC - 16

program has been restarted, go to step II.B.

III. Perkin-Elmer Chromatograph Console. (Optional)

Connect the communications cable from the Perkin-

Elmer console to the Cromemco.

System Shut-down

I. Type a control C at the KSR-43 teletype; the response

should be:

•** Options: t = Data Entry 5 = Acquire 2 = Search 6 = Analyse 3 = Delete 7 = Calibrate 4 = E>:anine 8 = Reload

... Enter option . 8

II. If the above response was not obtained within ten

seconds, the SPC-16 is down and it is safe to turn

the power off at the Cromemco and KSR-43 teletype.

73

III. If the above response was obtained,, select the

"Reload" option, wait five seconds and turn the power

off at the Croraemco and KSR-43 teletype.

IV. (Optional)

All communications cables and data cables may be

safely removed whenever the system is powered off.

The Perkin - Elmer console communications cable and

the data cables may be removed from the Cromemco at

any time without affecting system communications.

The teletype cable should not be removed without

performing the power off sequence.

System Crash

After a successful system startup, the user should

always obtain a message from the system whenever a control C

is typed at the KSR-43 teletype. If no response is obtained

then the SPC-16 has crashed. At this point the user should

turn the Cromemco power off and contact the RTCL operator in

Earth Sciences room 324 (X-3932, X-3947).

Option Selection Structure

For ease of implementation and user interaction an

option selection structure leads the user through chosen

catagories. Upon system start-up the SPC-16 downloads the

data acquisition and teletype communications program to the

Cromemco microcomputer. The SPC-16 then may communicate

with the user via the Cromemco. The options available allow

74

data entry, acquisition, analysis, deletion and searching.

Also an option is available to enter calibration constants

for conversion of raw scaled data to the proper units.

Another option is provided to resynchronize the SPC-16 with

the Cromeraco whenever the Croraeraco power is to be turned

off.

Data Entry

The "Data Entry" option provides manual entry of all

data collected from the furnace. Since some data is not

monitored by the Cromemco microcomputer, the user must enter

the data. Also the user may alter data collected by the

system. To modify any piece of information, the user

selects the record number and the type of data to be

modified. FURNACE prompts for data by name and expected

units. A null entry, carriage . return only, retains and

echoes the previous assignment. If the user enters a new

value, the old value is replaced and the new value is

echoed.

After the user has entered all data of a selected

type, a new data type may be selected. Return to the main

option level is made by entering a null entry for the data

type. At this point data alterations are saved on disk. If

the user exits by typing a control C while in the data entry

mode, previous changes are not saved and the new values must

reentered.

Enter option

*#* Options: 1 = Data Entry 5 = Acquire 2 = Search 6 = Analyze 3 = Delete 7 = Calibrate 4 = Exanine 8 = Reload

... Enter option

... Hodify which data record? 40

... Data Entry Options: 1 = Coal Feed Rate 7 = Air Input Rates

2 = Proxinate Analysis 8 = Fiue Gas Analysis 3 = Ultinate Analysis 9 = Flue Gas Tenperature

4 = Flue Solids Analysis 10 = Probe Position 5 = Air Tenperature and Pressures 6 = Coal Sanple Nane

... Enter the data option: 1 ... Coal Feed Rate = ? £=] los/hour

5.0 5.000

... Enter the data option:

2 * ProKinate Analysis: (As-Received Basis) ... Percent F.C. = ?

70 70.00 ... Percent V.H. = ?

20 20.00 ... Percent ASH = ?

5 5.000 ... Percent H20 = ?

5 5.000

... Enter the data option: 3

* Ultinate Analysis: (Dry, Ash-included Basi ... Percent C = ?

70 70.00 ... Percent H = ?

15 15.00 ... Percent 0 = ?

5 5.00V ... Percent S = ?

4 4.000 ... Percent N = ?

I 1 . 0 0 0


* Flue Solids Analysis: (Ash-Free Basis) ... Percent C = ?

100 100 .0

... Percent H = ?

0 0 . 0 0 0 0 ... Percent N = ?

0 0 . 0 0 0 0 ... Percent S = ?

0 0 . 0 0 0 0


... Air Temperature: [=] Fahrenheit 75 75.00 ... TRNS Pressure: C=] psiq

5 5.000 ... KKHI Pressure: [=] psiq 5 5.000 ... STGP Pressure: C=3 psiq

5 5.000

... Enter the data option: 6 ... Input Sanple Nane D.O.E. BITUMINOUS B.O.E. BITUMINOUS

7 7

Enter the data option 7

0

7

2 TRNS Air = ? [=] SCFH

2 .000 PRHT Air = ? C=] SCFH

7.000 STGD Air = ? [=] SCFH

0 . 0 0 0 0

... Enter the data option: . 8 * Flue Gas Analysis:

... Percent C02 = ?

.15 15.00 ... Percent CO = ?

.5 5.000 ... Percent 02 = ?

... Percent N2 = ?

.70 70.00 ... PPHV NO = ?

. 0 0 . 0 0 0 0 ... PPHM HCN = ?

. 0 0 . 0 0 0 0 ... PPHV H2S = ?

. 0 0 . 0 0 0 0 ... PPHM NH3 = ?

. 0 0 . 0 0 0 0

... Enter the data option: .9

... Flue Gas Temperature: [=3 Celsius . 6 0 0 8 0 0 . 0

... Enter the data option: . 1 0

... Prooe Position = ?

. 0

2 . 0 0 0 Percent CH4 = ?

0 . 0 0 0 0 Percent H2 = ?

1 . 0 0 0

1.000

Enter the data option

Enter option

78

Search

The "Search" option lists all data records that have

been obtained on a user specified date. Data records are

listed by record number, time when the record was created

and position of the sampling probe.

... Enter option

. 2

...Search on today's date? Y/N . i(

Input date record was obtained: HH,BB,YY . 1 2 . 1 0 . 8 1

*** Searching for records on: 12/10/81

**» End search

... Enter option

Delete

The "Delete" option allows the user to initialize

all or individual data records to an unused state. Upon

selection of this option the user is prompted to delete all

data. If all data records are to be deleted, the user must

verify two queries to initialize all data. Individual data

records may be deleted by answering NO to the prompt for

initializing all data and then entering the record number to

be deleted. To exit from this option the user should enter

a null entry.

79

*#* Options: 1 = Data Entry 5 = Acquire 2 = Search 6 = Analyze 3 = Delete 7 = Calibrate 4 = Examine 8 = Reload

... Enter option .3

... Delete all data? Y/N .Y

... Delete every record? Y/N .ii|

... Input record nunber to be Deleted .40

... Input record nunber to be Deleted .40

... Input record nunber to be Deleted

Examine

The "Examine" option reports disk data to the

teletype by record. This information is used for debugging

purposes.

Acquire

The "Acquire" option is used to ship data monitored

by the Cromemco to the SPC-16 for bulk storage and

subsequent data analysis. Data collected from the furnace

may be subdivided into two catagories. Those collected

automatically and those which must be entered by the user.

The Cromemco monitors the following outputs:

1. Flue Gas Fraction C02.

2. Flue Gas Fraction CO.

3. Flue Gas Fraction 02.

4. Flue Gas Fraction NOx.

80

5. Transport Air Differential Pressure.

6. Secondary Air Differential Pressure.

7. Staged Air Differential Pressure.

8. Furnace Thermocouples.

9. Chromatograph Console Reports.

The following data are not measured and must be

entered via the Data Entry option.

1. Coal Analysis (Proximate and Ultimate)

2. Flue Solids Analysis

3. Coal Feed Rate (Fuel Rich Conditions only)

4. Any furnace sensor data which are not monitored

but are assumed to be monitored.

Analyzer, differential pressure transducer and

thermocouple outputs are sampled every 3.75 seconds by the

Cromemco. The Cromemco averages the values collected over

the period of a minute. When the user requests that data be

shipped from the Cromemco to the SPC-16, only the averaged

data records are sent. Three data records representing 1,

11 and 15 minute old furnace sensor activity are received by

the SPC-16. The one minute old data set is used to report

the current state of furnace operation. Data from the 11

and 15 minute old data sets are used with chromatograph

reports; the chromatograph requires 11 and 15 minutes to

generate results. If no data is available from the

chromatograph console, the 11 and 15 minute old data are

disreguarded.

81

To ship data from the Cromemco to the SPC-16, the

user must select the "Acquire" option. FURNACE then prompts

the user for the static pressure in each of the three air

supply lines and the air supply temperature. These are used

with differential pressures to compute air input rates.

FURNACE then ships the data to the SPC-16 and reports air

flow rates and flue gas analyses. The time, date and record

number are also output so that data may be referenced for

deletion, analysis or edition.

The coal analysis, flue solids analysis and coal

feed rate (fuel rich conditions only) are assumed constant

and need to be entered by the user only when they change.

The values entered are used for all subsequent data analysis

and reports. When conditions are fuel lean, reported values

for the coal flow rate are computed and are not influenced

by the manually entered coal feed rate.

Analyze

The "Analyze" option is used to compute unmeasured

furnace operating variables. Four equations are solved

simultaneously to determine four unknowns. The four

equations are mass balances for nitrogen, hydrogen, carbon

and sulfur. Three unknowns that are unconditionally

computed are flue gas fractions of H20 and S02 and the flue

gas output flow rate. The fourth unknown is either the coal

input flow rate or the flue solids output flow rate. If

conditions are fuel lean then the coal input flow rate is

calculated and the output flow rate of flue solids is

assumed zero (ash free basis). If conditions are fuel rich

then the flue solids output flow rate is calculated and the

manually entered coal input flow rate is used. Fuel rich

versus fuel lean conditions are indicated by the measured

ratio of flue gas 02 content to flue gas CO content.

Conditions are considered fuel lean if the ratio is greater

than 0.5; otherwise, conditions are considered fuel rich.

A multivariable Newton-Raphson technique is used to

solve for the unknowns and the results are reported to the

teletype. Coal analysis and coal input flow rate are

reported on a moisture and ash included basis. Flue solids

analysis is reported on an ash included basis. Flue gas

fractions are reported on a moisture included and corrected

basis. The flue gas output flow rate and the air input flow

rates are reported at standard conditions.

Data consistency analysis is concerned with

minimizing discrepancies between data and values calculated

by imposing additional mass balance or thermodynamic

constraints. Furnace variables which are not calculated are

adjusted to minimize inconsistency between data and

constraints. The minimization algorithm is an iterative

process and normally requires about thirty iterations to

achieve global relative convergence. Each global iteration

requires approximately one minute; therefore, data

83

consistency should not be performed during data acquisition

periods. The results of the data consistency analysis are

reported in the same format as normal data analysis results.

Calibrate

The "Calibrate" option allows the user to enter

calibration model parameters to convert raw scaled data to

the proper units. Data conversion occurs after data is

acquired from the Cromemco to the SPC-16. Twentyfour raw

data channels are reserved for thermocouple data and eight

channels are reserved for three differential pressure

transducer and five gas analyzer data. Data from each

thermocouple is converted using two parameter models while

four parameter models may be used for each analyzer or

pressure transducer data.

*** Options: 1 = Data Entry 5 = Acquire 2 = Search 6 = Analyze 3 = Delete 7 = Caliorate 4 = Exanine 8 = Reload

... Enter option

.7 ... List the calibration assignments? Y/N

. H

**» Calibration options: 1 = P/E Transducers 2 = Analyzers

3 = Pt/PT-Rhodiun Thermocouples 4 = Chronel/Aluttel Thermocouples CH<8-15) 5 = CHROHEL/ALUHEL THERMOCOUPLES CH(16-23)

... Enter the calibration option:

... Enter option

7 ... List the calibration assignments? Y/N Y

CHANNEL SLOPE INTERCEPT 0 TC.R

= -1.043E+00 * TC.R 2.058E+03

1 TC.R = -I.043E+00 •* TC.R 2.058E+03

2 TC.R = -1.043E+00 * TC.R 2.058E+03

3 TC.R = -1.043E+00 * TC.R 2.058E+03

4 TC.R = -1.043E+00 • TC.R 2.058E+03

5 TC,R = -1.043E+00 • TC.R 2.058E+03

6 TC,R = -1.043E+00 • TC.R 2.058E+03

7 TC.R = -1.043E+00 * TC.R 2.058E+03

8 TC.K = -8.984E-01 * TC.K 1.777E+03

9 TC.K = -8.984E-01 * TC.K 1.777E+03 10 TC.K

= -8.984E-01 TC.K 1.777E+03

11 TC.K = -8.984E-01 * IU.K 1.777E+03

12 TC.K = -8.984E-01 * TC.K 1.777E+03 13 TC.K

= -8.984E-01 * TC.K 1.777E+03

14 TC.K = -8.984E-01 * TC.K 1.777E+03

15 TC.K = -8.984E-01 * TC.K 1.777E+03

16 TC.K =

9.150E-01 * TC.K 1.914E+03 17 TC.K

= -9.150E-01 * TC.K 1.914E+03

18 TC.K = -9.150E-01 * TC.K 1.914E+03

19 TC.K = -9.150E-01 * TC.K 1.914E+03

20 TC.K = -9.150E-01 * TC.K 1.914E+03

21 TC.K = -9.150E-01 * TC.K 1.9l4t+03

22 TC.K = -9.150E-01 * TC.K 1.914E+03

23 TC.K = -9.150E-01 •* TC.K 1.914E+03

CHANNEL = AO + AI*ADC + A2*ADC**2 + A3*ABC**3

AO A1 A2 A3 TRNS 9 .135E+00 -4 .780E-03 0. OOOE -01 0 .OOOE-•01 PRHT 8 .205E+00 -4 .080E-03 0. OOOE -01 0 .OOOE-•01 STGD 1 .009E+0I -5 .180E-03 0. OOOE -01 0 .OOOE-•01 C02 -4 .001E+01 4 .311E-02 -1. 589E -05 2 .249E-•09 CO -3 .387E+0I 4 .036E-02 -1. 654E -05 2 .437E-•09 02 3 .319E+01 -1 .693E-02 0. OOOE -01 0 .OOOE-•01 NO -4 .566E+03 2 .350E+00 0. OOOE -01 0 . OOOE-01 S02 0 .000E-01 0 . 000E-01 0. OOOE -01 0 .OOOE-01

*** Calibration options: 1 = P/E Transducers 2 = Analyzers

3 = Pt/PT-Rhodiun Thernocouples 4 = Chronel/Alunel Thernocouples CH<8-15) 5 = CHROHEL/ALUHEL THERMOCOUPLES CH(16-23)

... Enter the calibration option:

85

Reload

The "Reload" option should be selected prior to

turning the Croraeraco power off. This option synchronizes

the SPC-16 with the Cromemco when power is turned on at a

later time. Whenever the Cromeco is turned on, the SPC-16

must program the Cromemco. By selecting the "Reload" option

the user is informing the SPC-16 that the Croraeco power is

to be turned off. The SPC-16 then waits until the Cromemco

is turned on and then reloads the Cromemco with the data

acuisition and teletype monitor program.

APPENDIX D

THE CROMEMCO MICROCOMPUTER PROGRAM

The purpose for programming the Cromemco

microcomputer was to provide dedicated data acquisistion and

monitoring of the coal fired research furnace in the

Chemical Engineering deparment. Furthermore, communications

were to be established with the Earth Scieces/Mines

Real-Time Computing Laboratory to provide on-line data

analysis using a General Automation SPC-16/65 minicomputer.

System Configuration

Data acquisition includes sampling the analog

outputs from furnace sensors via an analog to digital

interface and monitoring for reports generated from a

Perkin-Elmer microcomputer controlled gas chromatograph.

Communications involved coordinating character Input and

Output (I/O) between the SPC-16, the laboratory teletype,

and the chromatograph (see Figure 3). An interrupt driven

approach was taken so that simultaneous events could be

serviced.

86 .

87

The Cromemco is configured with a Single Card

Computer (SCC) monitor, eight kilobytes of RAM, three

programmable UARTs, five parallel I/O ports, fifteen

interval timers, and an analog to digital interface. Acting

as an extension of the I/O subsystem of the SPC-16, the

Cromemco provides fully buffered full duplex communication

to a laboratory operator at a KSR-43 teletype. Periodic

data acquisition from the furnace sensors is implemented

using interval timers and chromatograph monitoring is

provided with one of the UARTs.

Interrupt Service Hierarchy

Following initialization, all functions performed by

the Cromemco are caused by interrupts. Whenever characters

arrive or leave any of the three UARTs, interrupt service is

requested. Likewise, whenever the data acquisition interval

timers time-out, interrupt service is requested. The

similarity of service required by interrupting devices

enables general purpose drivers and handlers to be common

among the service routines. Particular service needs can be

satisfied by examining parameters within Device Control

Blocks (DCBs) and executing the appropriate options with

special purpose handlers.

88

System Initialization

Prior to any interrupt service some initialization

must take place. Initialization occurs in the following

sequence. First the Cromemco is down-loaded from the SPC-16

upon Cromemco power-on since no bulk storage bootstrap is

supplied with the SCC monitor. After down-loading, the SCC

monitor exits to the down-loaded program where a checksum of

the program is computed to ensure the integrity of the

program. If the checksum computed by the Cromemco does not

match the checksum computed by the SPC-16, a control C is

issued to the SPC-16 and the down-loading sequence is

retried. Following a successful program load, interrupt

service initialization is executed.

Interrupt service initialization encompasses Z-80

CPU system initiazation and SCC external device

initialization. Z-80 initialization redefines the system

stack pointer from the location defined by the SCC monitor

to a more convenient location. Also the mode of Z-80 CPU

interrupt service is selected so that the page of the

interrupt service routine table is software selectable. The

I-register is loaded with the page of the table and the

interrupt service routine table is subsequently filled using

a block transfer from its down-loaded address to the proper

absolute address.

89

SCC external device initialization is concerned with

initializating the UARTs and the interval timers. The UARTs

are initialized by setting their BAUD rates, resetting their

interrupt status and defining their interrupt masks. The

interrupt status and masks for the timers are defined in the

same manner as with the UARTs. Initialization is complete

when interrupts are enabled; the Cromemco spends the

majority of its time thereafter in a null loop waiting for

interrupts to occur.

System Interrupt Service

When an external device requests service, the Z-80

CPU disables interrupts, pushes the return address onto the

stack, picks up the page of the interrupt service routine

table from the I-register and the pointer into the table

from the interrupting device and performs an indirect jump

using the effective address to the Interrupt Service Routine

Handler (H$ISR).

All interrupt service routines begin at H$ISR entry

points; there is one entry point for each interrupting

device. The advantage of this structure is that interrupts

may be simulated simply by executing a subroutine call to

one of the H$ISR entry points. Functions performed by H$ISR

include saving all registers, picking up the DCB address and

calling the appropriate service driver. Upon return from

90

the driver, H$ISR restores all registers, enables interrupts

and returns to the uninterrupted state.

Three service drivers were written to handle

character input, character output, and timer service (see

figure 8). Character input may occur from physical ports

01, A1 and B1. Character output may occur to ports 01 or

A1. Port 01 is the SCC monitor port and connects the

Cromemco to the SPC-16 minicomputer. Ports A1 and B1 are

serial ports supplied by the Cromemco TUART I/O expansion

board. Port A1 connects the Cromemco with the KSR-43

teletype and port B1 connects the Cromemco with the

Perkin-Elmer chromatograph console. Of the fifteen

available interval timers, the three that are used are

loaded via ports A5, A6 and A7.

Whenever a character is assembled by one of the

three UARTs, an interrupt is requested indicating Receiver

Data is Available (RDA). H$ISR saves all registers, picks

up the DCB address and calls the Driver for Receiver Data

Available (D$RDA). D$RDA is responsible for inputting the

character form the UART and buffering the character.

Character examination handlers are called so that special

control characters may be detected. Upon matching a control

character, other handlers may be called to implement

additional functions. Just prior to returning to H$ISR, an

output interrupt request is simulated if the character

9 1

( Start )

Wait for

Interrupt

1

^ v w n i c n m t e i r u p t ^ ^ 1

Clock 1 Time-out f

D$RDA || || D$TIMR || || D$TBE

1 r 1 >

|| H$RDA || || H$TIMR H$1 "BE

i £ i ( Return ) ( Return ^ ( Return )

F i g u r e 8 : C r o m e m c o M a c r o F l o w C h a r t

92

destination port is not busy. Output interrupts must be

simulated if "long" periods of inactivity have occurred

since the previous character output. The integrity of data

at the port is upheld by checking the status of the UART and

ensuring the UART Transmitter Buffer is Empty (TBE).

Whenever a UART finishes serial output and its

transmitter buffer becomes empty, an interrupt is generated.

Entry is made into H$ISR, registers are saved, the

corresponding DCB address is retrieved, and a call is made

to the Driver for Transmitter Buffer Empty (D$TBE). The

driver examines the character buffer pointers and decides if

any more characters need to be output. If the character

buffer is not empty then a call is made to the handler for

outputting characters.

Characters may either be output to the SPC-16 or to

the teletype. If characters are to be output to the

teletype then no special consideration is required prior to

their output. If characters are to be output to the SPC-16,

however, special care must be taken to ensure that the

SPC-16 is in a solicited input state. This is done by

handshaking using the SPC-16 input prompt to initiate record

transmission and ending record transmission with a carriage

return from the Cromemco. If the prompt has not been the

last character received by the Cromemco from the SPC-16, no

characters are output and return is transferred to H$ISR

without updating buffer pointers. If the prompt has been

received by the Croraemco, characters may be output to the

SPC-16 and simultaneously echoed to the teletype until a

carriage return is sent.

Circular buffers are used to hold characters

obtained from the serial input ports. Pointers are kept on

the lower and upper memory limits of the buffers as well as

pointers to the next available location for input characters

and to the next character for output. When characters

arrive, the character input pointer gets ahead of the

character output pointer. When the output pointer catches

up to the input pointer, character output stops. The

pointers are contained in the DCB correspoinding to the

interrupting I/O device.

Since the SPC-16 transmits characters at 2400 BAUD

and the Cromemco removes them at 300 BAUD to the teletype,

transmit-on and transmit-off protocol is practiced to

prevent buffer "overflow." When a character arrives from the

SPC-16, a buffer counter is incremented and the counter is

decremented when a character is removed to the teletype. If

the buffer count exceeds an upper limit, a control-S is sent

to the SPC-16. When the buffer count drops below a lower

limit, a control-Q is sent to the SPC-16. The buffer sizes

allocated for characters from the SPC-16 and the teletype

are 256 bytes each. A buffer size of 1536 bytes is

allocated for the chromatograph data. The buffer size for

9 4

the chromatograph needs to be large since an entire gas

analysis report may be held prior to its transmission to the

SPC-16 or the teletype.

Data Acquisition

The primary objective for using the Cromemco was to

monitor the instrumentation of the coal fired research

furnace. Analog signals from the thermocouples, analyzers,

and differential pressure transducers needed to be sampled

periodically, recorded and transferred to the SPC-16 for

subsequent data analysis. The problem of monitoring the

chromatograph was resolved by printing the report to both

the Perkin-Elmer GCC and to the Cromemco via RS-232 serial

transmission.

An analog to digital interface was designed to

multiplex, amplify, and convert conditioned analog signals

to 12 BIT parallel numbers. The interface, shown in Figure

4, requires a six BIT parallel signal to address the input

channel from a two-tiered multiplexor configuration.

Following channel selection, the Analog to Digital Converter

(ADC) is pulsed to start conversion. After conversion is

complete, the output is read by the Cromemco and stored in a

circular buffer. A total of 32 channels are sampled in an

ordinal fashion to provide a vector representing the

activity of the analog sensors.

95

It was decided to sample each channel sixteen times

per minute, average the data at the end of a minute and save

the resultant vector in another circular buffer designed to

hold sixteen vectors. Pointers into the sixteen minute

history buffer indicate fifteen, eleven and one minute old

data sets. This was done to synchronize data from the

chromatograph with data from the analog instruments since

the chromatograph requires fifteen minutes to generate gas

analysis reports.

The function of the interval timers are to provide

periodic interrupts for sampling the analog interface.

Three timers are used because three fundamental periods are

involved. Time is required for the interface to settle when

each new channel is multiplexed. Another time period is

required for analog to digital conversion to be completed.

Finally, the sampling frequency of sixteen data sets per

minute is enforced. Admittedly the above timing

requirements could be met using one timer with additional

logic; fifteen timers were available, however, and timing

tasks were distributed among the three. The time required

for analog to digital conversion and analog interface

stabilization is on the order of 50 microseconds. An

arbitrarily long waiting period of 8.2 milliseconds is used

for both stabilization and conversion and a waiting period

of 3.75 seconds is used to obtain a sampling rate of sixteen

sets per minute.

9 6

The interval timers decrement their load count once

every 64 microseconds. When a timer count reaches zero an

interrupt is generated. As in UART interrupt service,

interrupts become disabled and indirect subroutine call is

made to an entry point of the Interrupt Service Routine

Handler (H$ISR). The handler saves all registers, picks up

the corresponding DCB address and calls the Driver for TIMeR

interrupt service (D$TIMR).

D$TIMR reloads the timer and checks the status of

the data service handler. If the handler status is disabled

then a return to H$ISR is made. If the data service is

enabled, a call to the Handler for TIMeR (H$TIMR) service is

made. H$TIMR is responsible for calling the appropriate

data management and interface control handlers. Upon

completion of the specific task, return is made to H$ISR

where registers are restored, interrupts enabled and return

to the uninterrupted state is made.

Concluding Remarks

The entire Cromemco program was assembled by hand

and linked via the Z80LNK utility developed on the SPC-16

minicomputer. After tedious debugging the end product is

operational and located near the furnace instumentation. An

interrupt driven approach has enabled simultaneous character

I/O with data acquisition while protecting the integrity of

all information tranfer.

APPENDIX E

D.O.E. COMMAND FILES AND SOURCE LISTINGS

Following are the command files and source listings

neccessary to completely generate the D.O.E. program set.

The command files include compilation, linking and loading

files for SPC-16 tasks and compilation and linking files for

the Zilog Z80A assembly to Cromemco Control BASIC utility.

Source files include compilation listings of all SPC-16

FORTRAN-IV modules and all Z80A assembly modules.

97

t JOB $C *C COMPILE FILE FOR THE D.O.E.COAL FURNACE $C *C LUN/PUN ASSIGNMENTS! 20=02 tC 53=UJ(D0EDAT> $C «SI=DS(DOEBLK> «FI4F*RO:AOOO *SI=DS(DOEMAN) TF16F*R0!AOOO *SI=DS(Z80L0D) *FHF#RO!AOOO *SI=DS(Z80SHK) »F16F*ROSAOOO •8SI=nS(Z80FUN> «F16F»ROSAOOO TSI=DS(DOEBEL) SFI6F*RO:AOOO *SI=DS(DOESEA) SFI6F*RO:AOOO $SI=HB(HOESTK) IFI6F*RO:AOOO tsi=ns<noECAL) »F16F*R0SA000 4SI=DS(D0EDIS) $FI&F*RO:AOOO $SI=HS(DOEGET) »FI6F*RO:AOOO

ISI=DS(DOEINP) IF16F*R0!A000 1SI=DS(D0ECH0) *FI6F*RO:AOOO *EOD $C $C BOUND COMMON AT C*AL02 + X'OOOF' *C •LO=TY TCLOB *MAF'L *80UNB>CEIC£E *CONMQNrP»S *BUILDfUL »REPLACE»DC(DOERUN)»UC •PACKfDC $c t JOB IE — COMPILE FILE FOR THE D.O.E.COAL FURNACE $C *C LUN/PUN ASSIGNMENTS! 20=02 tC 53=UJ(D0EDAT> *C SSI=DS(DOEBLK> *F16F*R0!A000 $si=ns(noEio> $F16F*R0!A000 *SI=DS(DOERPT> »F16F#R0!AOOO «SI=DS(DOEGMA) $FliF*R0!A000 1.SI=HS(D0EBFN) »FI6F#RO:AOOO «SI=DS(DOEGAU> $F16F#R0:AOOO $SI=DS(DOESTK) *F16F*RO!AOOO TSI=DSCDOEOUT>

— LUN/PUN ASSIGNMENTS! 20=02 53=UJ(D0EDAT)

SFI6F*RO:AOOO tSI=DS(D0EBTA) SFI6F*RO:AOOO lEon *c tc — BOUND GLOBAL AT X'630' FOR SPOOLER «C tLO=TY tCLOB *MAPL ABOUNDiG6630 tCOMMONrPrS *BUILD>UL tREPLACErDC(DOERPT)>UC tPACK» DC tc t JOB $C tC COMPILE FILE FOR THE D.O.E.COAL FURNACE tC tC tC

tSI=DS(DOEBLK> tF16F*R0!A000 tSI=DS(DOECPU) tF16F*R0!A000 tSI=DS(DOESET) »FI6F*RO:AOOO tSI=IiS CDOESTK) tF16F*ROiAOOO JSI=DS(DOECOG) tF16F*RO{AOOO tSI=DS(DOENEU) tFl&FtRO!AOOO $SI=DS(DOECNV> tF16F*ROiAOOO tSI=DS(DOEFVC) tF16F*R0tA000 $S1=DS(D0EJAC) tF16F*R0!AOOO tSI=»S(DOEPIV) tF16F#RO!AOOO tSI=DS(DOEMAT> tF16FIR0!AOOO tSI=BS(DOESSO) tF16F*R0!A000 tSI=DS(DOEZVL) tF16F*R0SA000 tSI=DS(DOEFVL) tF16F*RO:AOOO ISI=DS(DOESRT) tF16F*R0!A000 $SI=HS(DOESQR> tF16F#R0JAOOO tEOD tLO=TY tCLOB *MAPL *COMMON»PrS IBUILDFUL tREPLACEiDC(DOECPU)FUC tPACK.DC tCC=TY

END t JOB tC tc DOE FURNACE PROG COMMAND FILE tC tFX !OFFrF

!DELETE»FP(J3)»RP(J3) !DELETEiFP<J6)iRP(J6) !DELETEiFP(J27)>RP(J27) !•PROG»3>PU8(104)rAPUrZB3» OFF»PS=36FOfPI=DC(DOECPt)iFP(J3)rRP(J3) ! •PROGr6fP08<104)fAPU»Z05»OFFtPS=36F0>PI=DC<D0ERPt)»FP<J6)»RP(J6) !•PROG»27?P08(104)»APUiZ06»OFFrPS=36FO>PI=DC(DOERUt)»FP(J27)tRP(J27) !BX $ JOB tCC=TY

END (JOB tC tC THIS COHHAND FILE BUILDS THE FURNACE CROHEHCO LINKER $C »SI=DS(Z80LNK> »FI6F#RO:AOOO $SI=DS(Z80HTC) *FI6F*RO:AOOO $SI=DS(Z80CTH) $FI6F*RO:AOOO »SI=DS(Z800UT) $FI6F»RO:AOOO $E0H tc ICLQB CHAPL *BUILD *F:EPLACErDC(ZBOLNK)rUC tPACKfDC tc tC TO BUILD THE CROHEHCO PROGRAH. ISSUE! »CC=CHCZ80BLD) tCC=TY

END $ JOB tc tC CROHEHCO / ZBO BUILD FILE tc tC — OBTAIN A LISTING VIA LUN! LO tC ERROR HESSAGES APPEAR ATS OH tc tso=us tIS=DP tSI=UJ(Z80BAS) t63=DS(Z80DIR) TZBOLNK t JOB tC tC — THE EDITOR REH0VES UNNECCESSARY REFERENCES. tC tSI=DP tEDITOR 03/4&iD 0C=Y tC SC THE LINKED BINARY IMAGE IS IN USt tC REPLACE UJ(Z80PGH> WITH THE NEU IHAGE tC UHEN THE FURNACE LAB IS NOT EXECUTING. tC tCC=TY

END

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FIND OUT UHICH RECORD TO ANALYZE

URITE(TTY»106) READ(TTY»104) IOPT IF(IOPT.LE.O.OR.IOPT.GT.HAXREC) GO TO 10 IREC=IOPT

CHECK FOR A CONSISTENCY ANALYSIS

URITE(TTY»108) READ(TTY»112) IOPT SSQMIN=IOPT.EQ.'Y' IF(.NOT.SSQMIN) GO TO 20

CHECK FOR THE INCLUSION OF THE GAS-SHIFT REACTION

URITE(TTY»110) READ(TTY»112) IOPT SHIFT=IOPT.NE.'N' CONTINUE

SAVE LABELED COHHON ON DISK

CALL DOESTK(PUSH) CALL TPNf1(J0B6.N0U.M0DE) CALL RSFOF CALL DOESTK(PULL)

GO TO 10

D.O.E. Furnace')

1

FORMAT(//'RTOS-16. Rev.75 FORHAT<//'*** Options?'/ 4X»'l = Data Entry'.2X.'5 = Acauire'/ 4X»'2 = Search '.5X.'6 = Analyze'/ 4Xi'3 = Delete '»5X.'7 = Calibrate'/ 4Xi'4 = Examine'rSXf'8 = Reload') FORMAT*/'... Enter option') FORMAT(V) FORMAT</'.. FORMAT('... FORMAT <'. • 1 FORMAT(A1) END

0000. PSECT SIZE! 0453. DSECT SIZES 0001i REV. 5

• Analyze which data record?') Include a consistency analysis? Include the Sas-shift reaction?

Y/N') Y/N')

LABELS VARIABLES ARRAYS PROCEDURES

)1 001B TTY 0000 C RDATA 0000 C FREMAT OOCB 1100 0116 DISK 0001 C NOU 0000 P FtMDl OOCC >5 002A RANGET 0002 P Z80L0D OOCD ) 101 0129 RANPUT 0003 P DELtl OOCE ) 10 0030 PUSH 0004 P F»URF OOCF ) 102 0178 PULL 0005 P F$TEF OODO ) 104 0183 DEBUG 0000 c F$REF 00D1 >15 0081 RESET 0001 c FIARF 00D2 1106 0185 SHIFT 0002 c DOENTR 00D3 ) 108 0197 SSQMIN 0003 c DOESEA 00D4 ) 112 01C3 RELOAD 0006 p DOEDEL 00D5 )20 0106 HAXREC 0002 c DQEDIS OOD6 >110 01 AD 1REC 0003 c DOEGET 00D7

J0B3 0007 p DOECAL 00D8 J0B6 0008 p FIOPN 00D9 IOPT 0009 p F$IOS OODA HODE OOOA p F*CLS OODB MASSBL OOOB p DOESTK 0113 • ALA 0000 TPN*1 0114

09/16/80 BLOCKNANES

DATA 0066 LUN 0004 DEBUG 0004

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0146! NREC=NREC*32 01475 0148!

WRITE(LINE»520) ISTART. NREC.CHKSUM.ISTART 01475 0148! URITE(LINE»522> 0149S14 CONTINUE 0150! H=M$FBF<DOEDAT> 0151! H=M»CFA«DISK»DATFIL) 0152! RETURN 0153 * C 01541500 FORHAT('NEU') 0155:502 FORHATCLOCK X40'> 0156i512 FORMAT(40A2) 0157:516 FORHAT('QUIT') 0158:518 FORMAT('R'.Z4.4H S20)

FORMAT('1 A=' .15.'»N='» 0159:520 FORMAT('R'.Z4.4H S20) FORMAT('1 A=' .15.'»N='» I5i'!S='. 13.'>CALL%'.Z4.'(S.N.A>'>

01601522 FORHAT('RUN') 0161!524 FORMAT(32Z4) 0162:c 0163: END »ERR0R COUNT.* OOOO. PSECT SIZE! 0517» DSECT SIZE! 0013; REV. 5

LABELS VARIABLES ARRAYS " PROCEDURES

)10 006B LINE OOOO C BINARY OOOO P Z80FUN 0133 ) 500 01CB DISK 0001 C UAIT 0012 P Z80SHK 0134 ) 502 01CF MAXREC 0002 C Z80PGH 0014 P DEL$1 0135 >16 008C IREC 0003 C ASCII 001C P FtURF 0136 >512 01H5 Z80FIL 0014 P DOEDAT 0018 P F*TEF 0137 >20 00B2 DATFIL 0018 P BASIC 0045 P M»FBF 0138 >22 OOBA ADDR 0044 P BUFF 004A P MtCFA 0139 >30 OOEB CHKSUH 004F P ADDRS 0048 P FtREU 013A )40 01A5 HR 0054 P TIME 0050 P F*REF 013B >516 01D8 HN 0055 P F»MD1 013C >34 0103 SC 0056 P FtARF 013D >42 019D IOSGET 0057- P FiENC 0142 >518 01DC IOSPUT 0058 P F*IOS 01C8 >36 0183 NCHAR 0059 P F$M00 01C9 >520 01E4 H 005A P FIRET 01CA >522 01FE I 005B P >14 01BE J 005C P >524 0202 NREC 005D P

NODE 005E P LTEMP 005F P ISTART 0060 P tAlA OOOA • ALA OOOB •AIB OOOC

09/16/80 BLOCKNAHES

LUN 0004

OOOliC 0002!C=== 0003JC 0004! OOOS'C 00061C 0007!C 0008!C= 0009JC ooio: OOlliC 0012: 0013: c ooi4:c oois:c ooi6: 0017! ooi8: ooi?:c oo2o:c 0021: c 0022: 0023: 0024:c 0025:c

SUBROUTINE Z80SHKCLINE.M0DE)

***ROUTINE TO INITIALIZE COHHUNICATIONS UITH CROHEHCO

INTEGER IU0RD(2)»IDEL<2)

COHHON ISTATSdo)

*#*GLOBAL SHOULD BE BOUNDED AT THE DCB'S LO

DATA IUORD/2tO/ DATA ITIME/Z8004/tIDEL/Or1/ DATA 1/0/

***CHECK CALLING PARAHETERSM*

H0DE=0 IF<LINE.LT.0.0R.LINE.GT,63) RETURN

***INHIBIT NULL OUTPUT ON URITE

r

107

oo26:c 0027! 0028'C 0029JC 0030!C 0031! 0032tC 0033!C 0034:c 0035! 0036!C 0037!C 0038!C 0039 J 0040! 0041IC 0042 :c 00435C 0044'10 0045! 00461c 0047IC oo4s:c 0049! ooso: 0051! 00521C 0053JC 0054IC 0055! 00S6!C 0057!C 0058!C 00595 0060:C oo6i:c 0062SC 0063: 0064! 0065:100 0066!

ISTATS<10)=ISTATS(10).AND.X'FDFF'

miNHIBIT <LF> ON INPUT

ISTATS(11 ) = ISTATS<11).OR.X'100'

***ENABLE USER PROHPT

ISTATS(2)=ISTATS(2).OR.X'200'

***SET BAUD RATE TO 2400

ISTATS(9)=X'127' CALL F$OPN(LINE)

«**ENABLE INPUT WITH TIME-OUT

CONTINUE CALL ItCLCK(LINE»ITIMEiMODE)

mtlAIT FOR CROHEMCO TO BE TURNED ON

READ(LINEilOO) IUORD CALL DELtl(IDEL) IF(IU0RDC2)»NE.'OK') GO TO 10

***DISABLE USER PROMPT

ISTATS(2>=ISTATS<2>.AND.X'FDFF'

mENABLE <LF> ON INPUT

1ST ATS <11> =ISTATS(11>.AND.X'FEFF'

tttCOHMUNICAT IONS SHOULD NOU BE ESTABLISHED

M0DE=1 RETURN F0RMAT(A2/A2) END

TERROR COUNT! OOOOi PSECT SIZE! 0113F DSECT SIZE! 0012! REV. 5 LABELS

) 10 ) 100

0031) 006D

VARIABLES

LINE 0009 MODE OOOA ITIME 0004 P I 0005 P •ALA OOOB

ARRAYS

IUORD 0000 P IDEL 0002 P ISTATS 0000 C

PROCEDURES

F*SBT F*MD1 F$RET FIOPN ITCLCK 0068 F$REF 0069 F$ARF FITEF

0064 0065 0066 0067

09/16/80 BLOCKNAHES

0010

006A 006B

DEL«1 006C

0001JC 0002!C= 0003:c 0004! 0005 :c. 0006:c 0007!C 0008'C= 0009!C ooio: oon:c 0012: 0013! 0014! 0015! 0016! 0017!

INTEGER FUNCTION Z80FUN(K)

THIS ROUTINE CONVERTS ASCII HEX TO BINARY

DATA ITEHPljITEHP2/2*0/

ITEMP1=(K.AND.X'7FOO')/X'100'-X'30'

IF<ITEMP2.GT.9)ITEMP2=ITEHP2-7 Z80FUN=ITEMP1*X'10'.OR.ITEMP2 RETURN

108

0018: END »ERR0R COUNT! OOOOr PSECT SIZE! 0061f DSECT SIZE! 0011. REV. 5

1 LABELS VARIABLES ARRAYS PROCEDURES 09/16/80 BLOCKNAMES

0001 C 0002 C= 0003 C 0004 0005 C 0006 C 0007 C 0008 C 0009 0010 C 0011 0012 0013 C 0014 0015 0016 C 0017 0018 C 0019 0020 c 0021 0022 c 0023 0024 0025 c 0026 c 0027 c 0028 002? 0030 0031 0032 0033 0034 0035 0036 0037 0038 0039 0040 20 0041 0042 0043 0044 30 0045 0046 10 0047 C 0048 C 0049 C 0050 0051 0052 0053 0054 0055 0056 0057 0058 40 0059 0060 0061

Z80FUN OOOA K 0009 ITEMP1 OOOO P ITEHP2 0001 P

SUBROUTINE DOEDEL

FSSBU 0038 F$DOO 0039 FtHDl 003A FSHOO 003B F*REI 003C

THIS ROUTINE ALLOWS THE OPERATOR TO DELETE SELECTED DATA RECORDS OR INITIALIZE THE ENTIRE DATA BASE.

COMMON /LUN/ TTYrDISKfMAXRECflREC COMMON /DATA/ RDATA

INTEGER RANGETrRANPUTfRECORD INTEGER TTYfDISK

INTEGER RDATAU02)

EQUIVALENCE (RECORDtRDATA(2>)

DATA RANGET/Z105F/f RANPUT/Z109F/

DATA IfJfM/310/ DATA IANS/O/

CHECK FOR FILE INITIALIZATION

WRITE(TTYtlOO) READ(TTY1104)IANS IF(IANS.NE.1HY) GO TO 10 URITECTTY r102) REAIKTTY f 104) IANS IF(IANS.NE.IHY) GO TO 10 DO 30 1=1fHAXREC

RECORH=I CALL FtOPN(DISK) CALL F$IOS(RANGETrRDATAfDISKfH) DO 20 J=3f102

RDATA(J)=0 CONTINUE

RDATA<4)=-1 CALL F»IOS(RANPUTfRDATAfDISKfM) CALL FtCLS(DISK) CONTINUE

RETURN CONTINUE

CHECK FOR SINGLE RECORD DELETION

URITEtTTYf106) READ(TTYt108) IANS IF(IANS.GT.MAXREC.OR.IANS.LT.1) RETURN RECORD=IANS CALL FtOPN(DISK) CALL F$IOS(RANGETfRDATAfDISKfM) DO 40 1=3 r102

RDATA(I)=0 CONTINUE

RDATA(4)=-1 CALL FtIOS(RANF'UTiRDATAfDISKfH) CALL FtCLS(DISK)

109

0062! 0063:c 0064:100 0065!102 0066!104 0067!106 0068:108 0069: »ERR0R COUNT!

GO TO 10

FDRMAT('... FORMATC... FORMAT(Al) FORMATC.., FORMAT(V) END

0000. PSECT SIZE! 0252. DSECT SIZE? 0011! REV. 5

Delete all data? Y/N') Delete every record? Y/N')

Input record nunber to be Deleted')


) 100 00C3 TTY 0000 C RDATA 0000 C FSURF 00B6 )104 00E3 DISK 0001 C FtTEF 00B7 ) 10 006E MAXREC 0002 C FiREF 00B8 >102 00D2 IREC 0003 C F*ARF 00B9 130 0065 RANGET 0000 P FtMDl OOBA ) 20 0054 RANPUT 0001 P FtOPN OOBB ) 106 00E5 RECORD 0001 c FtlOS OOBC 1108 OOFA I 0002 p FiCLS OOBD ) 40 00A6 J 0003 p FtRET OOBE

M 0004 p IANS 0005 p *AIA 0009 *ALA OOOA

09/16/80 BLOCKNAMES

LUN DATA

0004 0066

0001SC 0002!C== 0003!C 0004! 0005!C 0006!C 0007JC 0008iC ooo9:c== Qoio: c ooii: 0012: c 0013! 0014! oois:c 0016! ooi7:c 0018! 0019: oo2o:c 0021: c 0022 :c 0023:c 0024:c 0025! 0024! 0027! 0028'. 0029! 0030IC 0031: c 0032JC 0033! 0034! 0035:10 0036! 0037SC 0038 !C 0039!C 0040: 0041: 0042! 0043! 0044! 00455 0046:

SUBROUTINE DOESEA

THIS SUBROUTINE SEARCHES FOR RECORDS OBTAINED ON A GIVEN DATE.

INTEGER D>Y.ANS.TTYiDISK.RANGET»RECORD.RDATA

COMMON /DATA/ RDATA<102) COMMON /LUN/ TTYrDISKfMAXREC.IREC

EQUIVALENCE <RDATA<2).RECORD)

DATA RANGET/Z105F/ DATA M>D.Y1I»MD»J.ANS/7*0/

GET RECORD DATE*.

CHECK FOR DEFAULT

WRITE(TTY r100) READ(TTY»102) ANS IF(ANS.EQ.1H ) RETURN CALL DATEiB(Y»M»D) IF(ANS.EQ.IHY) GO TO 10

INPUT DATE

URITE<TTY.103) READ(TTYil06) MiDFY CONTINUE URITE(TTYrl04) M.D.Y

HATCH RECORD DATE UITH SEARCH DATE

DO 20 1=1.HAXREC RECORD=I CALL FIOPN(DISK) CALL F$IOS(RANGET.RDATA.DISK.MD) CALL FtCLS(DISK) IF(RDATA(4).NE.M) DO TO 20 IF(RDATA(5).NE.D) GO TO 20

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DATA IOSPUT.IOSGET/Z109F.Z105F/ DATA PUSH.PULL/0.1/. I»JrH/3*0/ DATA NUORDS/O/. NRECRD/7/F NULL/1.0.0/

NMORDS=(RDATAtl)+l)/2

CALL FIOPN(DISK) IFUOPT.ECI.PULL) GO TO 25

SAVE LABELED COHHON ON THE DISK

DO 10 1=1INRECRD DO 20 J=1RNUORDS

RDATA(J+2>=BUFFER(J+(I-1)#NU0RDS) CONTINUE

RDATA(2)=HAXREC+I+3 CALL^SIOSaOSPUT.RDATA.DISK.H)

CALL FiCLS(DISK)

DISABLE "C WHILE SWAPPING TASKS

CALL U$INTR(TTY..FALSE.)

RETURN CONTINUE

ENABLE "C AFTER THE JOB NUMBER IS IN THE DCB

CALL F$IOS(IOSPUT»NULL.TTYIH) CALL U»INTR(TTYF.TRUE.)

CALL FIOPN(DISK)

RETRIEVE DATA FROH THE DISK

DO 30 1=1.NRECRD RDATA<2)=HAXREC+4+NRECRD-I CALL FSIOS(IOSGET.RDATA.DISK.H) DO 40 J=1.NUORDS

BUFFER <J+(NRECRD-I)*NUORDS)=RDATA < J+2) CONTINUE

CONTINUE CALL FiCLS(DISK)

t

RETURN END

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READ(TTY.IOO) <A<K.J),J=lr4) •CONTINUE

GO TO 15

ENTER THE PT/PT-RHODIUM THERMOCOUPLE CONSTANTS

CONTINUE K=0 DO 72 1=1>8

URITE(TTYfl06) TNAHEliK REAIt(TTYilOO) TBASEU>fTSLOPE(I) K=K+1 CONTINUE

GO TO 15

ENTER THE CHROMEL/ALUMEL THERMOCOUPLE CONSTANTS

CONTINUE KS8 DO 74 1=9.NTC

URITE(TTY»106) TNAME2»K READtTTY1100) TBASE(I)»TSLOPE(I) K=K+1 CONTINUE

GO TO 15

1

FORMAT(V) FORMAT(Al) FORMATC... List the calibration assignments? Y/N') FQRMAT(/'... Enter the intercept and slope for! 'rA4iI3> FORMAT, Enter the constants: A0»Al»A2rA3 for! '»A4) FORMAT(/'CHANNEL'i15X»'SLOPE'rl3X»'INTERCEPT'> F0RMAT(I4»8XIA4»' = '.1PE10,3»' * '»A4»' + 'f1PE10.3> FORMAT!/'... Enter the calibration option!') FORMAT(//'*** Calibration options!'/ 4Xf'1 = P/E Transducers'/ 4X»'2 = Analyzers'/ 4Xi'3 = Pt/PT-Rhodiu« Thermocouples'/ 4Xr'4 = Chroitel/Aluael Thermocouples') FORMAT </'CHANNEL = AO + A1IADC + A2*ADC**2 + A3*ADC**3'> FORMAT(10X»'AO'r10X»'Al'110X r'A2'?10X>'A3') FORMAT(A4rlX»4(1PE10.3>2X)) END

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1 1 7

0034! 0035! 0036: 0037! 0038! 0039! 00405 0041! 0042! 0043! 0044*. 004S! 0046! 0047! 0048! 0049! 0050! 0051! 0052:c 0053! 0054! 0055! 0056! 0057! 0058! 0059!C 0060! 0061!C 0062! 0063! 0064!C 0065! 0066! 0067! 0068!C 0069!C 0070!C 0071!C 0072!C 0073? 0074! 0075!C 0076! 0077!C 0078!C 00795C 0080: 0081! 0082! 0083! 0084110 0085JC 0086!C 0087!C 0088! 0089*. 0090! 0091SC 0092! C 0093:c 0094!20 0095! 0096! 0097!C 0098SC 0099!C 0100! oioi: 0102.C 0103JC 0104SC

EQUIVALENCE

EQUIVALENCE

EQUIVALENCE

(DATE d)F RDATA(4 >) F (TIHE(1)FRDATA(7))F (TSAHPL»RI<ATAdO))» (AIR(1T»RDATAU2>)f (FLUE <1»rRDATAdB)> F (PROX(1)rRDATA(42))r (ULTIM(l)fRDATA(50>)t (SHOKEd) FRDATA(60))F (C0ALFRDATA(68))> (NAMEt1)fRDATA(70)) (KDATAd)iUNITS(40))t (PRESSRd)»KDATA(34)> t (AIRTNPfKDATA(40)> t (KPROX(l)iKDATA<42))? (KULTIHd) FKDATA(50))t (KSMOKE <1)rKDATA(60))t (KC0AL>KDATA(68))> (KNAMEd)»KDATA(70>)

(IDATA(1)RIDATA1d)) F (JDATA(1)>JDATA1(1))F (A(1>1)>IDATA(3)) i (TSLOPE(1)»JDATA (3)) F (TBASEd)fJDATA(51)) (Z80DAT(1)fKDATAld))

INTEGER RANGETFRANPUTFDISKFTTY

DATA RANGET /Z105F/. RANPUT /Z109F/ DATA I0SPUT/Z009F/

DATA JFNREC/2*0/F BLANK/.TRUE./ DATA IfK/2*0/» ZERO/O.0/ DATA SCFMFPCNTFPPHV/'SCFN'F'Z 'F'PPMV'/

LAHINAR FLOU ELEMENT SPECIFICATIONS

SPECIFICATIONS UNITS ARE [=1] SCFH/INCH H20

DATA LFE/3.2F20.0F17.0/ DATA RANKINFTSTANDfHGIATHFTUCSONFGAUGE/460.F70.F760.F692.F14.7/

DATA CNTRLA/1F0FZ0100/F CNTRLD/1I0FZ0400/

SEARCH FOR AN EMPTY RECORD

CH.L FtOPN(PISK) DO 10 REC0RD=1iHAXREC

CALL F$IOS<RANGETFRDATAFDISKFM> IF(DATEd).EQ.-l) GO TO 20 CONTINUE

ALL RECORDS FILLED

CALL FiCLS(DISK) URITECTTYFIOO) RETURN

EMPTY RECORD FOUND

CONTINUE CALL TIHE*B(T1ME(1)FTIME(2)FTIHE(3)) CALL DATE«B(DATE(3)fDATE(1)FDATE<2>)

SAVE TIME AND DATE ON DISK

2ALL"£*58S(RANPUTFRDATAfDISKFH>

SAVE RECORD NUMBER IN CONSTANTS RECORD

1 1 8

0105! 0106! 0107: 0108! o i o 9: c ono:c OllliC 0112! 0113! 0114:22 oiis:c o 116: c 0117SC 0118! 0119! 0120! 01215 0122!C 0123! 0124! 0125 * C 01261C 012 7: c 0128: 0129! oi3o: oi3i: 0132! 0133: 0134! 0135S25 0136JC 0137:C 0138:c 0139:c oi4o:c 0141 :c 0142IC 0143! 0144: 0145:c oi^6:c 0147SC 0148: 0149! 0150132 o 151: c 0152:c 0153!C 0154! 0155: 0156133 015 7: c 0158:c 0159 :c 0160: oi6i:c 0162IC 0163: c 0164! 0165:c 0166!C 0167!c 0168: 0169: 0170: oi7i:c 0172:c 0173SC 0174! 0175:c

KDATA<1)=RDATA<1) KDATA(2)=MAXREC+1 CALL FiIOS(RANGET»KDATAiDISK.M) KDATA(3)=NREC

USE DEFAULT COAL AND FLUE SOLIDS ANALYSIS

DO 22 I=42>102 RDATA(I)=KDATA(I) CONTINUE

RETRIEVE THE CALIBRATION CONSTANTS FROH DISK

IDATA(1)=RDATA(1) JDATA(1)=RDATA(1) IDATA<2)=MAXREC+2 JDATA<2)*HAXREC+3

CALL FtIOS(RANGET>IDATA«DISKrH) CALL FtIOS(RANGET>JDATAiDISKiH)

OBTAIN THE UPDATED STATIC PRESSURES AND AIR TEHPERATURE

URITE(TTY rll4) CALL DOEINP(ANS»BLANKfTTY) IFC.NOT.BLANK) AIRTMP=ANS DO 25 1=1.3

URITE(TTY»116) GNAMECI) CALL DOEINP < ANS? BLANK tTTY) IF(.NOT.BLANK) PRESSR(I>=ANS CONTINUE

RETRIEVE MULTIPLEXED DATA FROM THE CROHEMCO

T-l HINUTE IS IN Z80DAT< 1 - 32 ) T-15 HINUTES IS IN Z80DAT< 33 - 64 ) T—11 HINUTES IS IN Z80DAT< 65 - 96 )

CALL F*IOS(IOSPUT»CNTRLAfTTY.M) READ<TTYi104) Z80DAT

CONVERT PT/PT-RHODIUM T.C. DATA

DO 32 1=1F8 T(I>=TSLOPE<I)*Z80DAT(I)+TBASE(I) CONTINUE

CONVERT CHROHEL/ALUHEL T.C. DATA

DO 33 1=9.24 T < I) =TSLOPE<I)*Z80DAT <I)+TBASE(I) CONTINUE

SAVE THE FLUE GAS TEMPERATURE

TSAHPL=T(2)

CONVERT THE P/E TRANSDUCER DATA

DO 36 1=1r 3

CONVERT ADC VALUES TO INCHES H20

BASE=Z80DAT(24+I) UNITS(I)=A(I.l)+A(I.2)*BASE+A<I»3)*BASE**2+A(Ir4>*BASE**3 IF(UNITS(I).LT.ZERO) UNITSCI)=ZERO

CONVERT INCHES H20 TO SCFH

AIR(I)=UNITS(I)*LFE(I)

1 1 9

0176 C 0177 C 0178 0179 0180 36 0181 C 0182 C 0183 C 0184 0185! 0186 0187 0188 0189 38 0190 C 0191 C 0192 C 0193 0194 C 0195 C 0196 C 0197 0198 0199 C 0200 C 0201 C 0202 0203 0204 C 0205 C 0206 C 0207 40 0208 C 0209 C 0210 C 0211 45 0212 C 0213 0214 0215 0216 0217 0218 50 0219 0220 C 0221 C (P09 C 0223 0224 0225 0226 0227 0228 C 0229 100 0230 102 0231 0232 104 0233 106 0234 108 0235 110 0236 0237 112 0238 114 0239 116 0240 C 0241

CONVERT CUBIC FEET PER MINUTE TO STANDARD CONDITIONS

AIR<I)=AIR<I)*<TUCS0N+HG1ATH*PRESSR<I)/GAUGE)/HG1ATH AIR(I) =AIR< I)*CRANKIN+TSTAND)/ < RANKIN+AIRTMP) CONTINUE

CONVERT THE ANALYZER DATA

DO 38 I=l»4 K=I+3 BASE=Z80DAT(27+I> FLUE (I)=A(K.1)+A(K»2)*BASE+A<K(3)*BASE**2+A(K(4)#BASE**3 IF(FLUE(I).LT(ZERO) FLUE(I)=ZERO CONTINUE

RETRIEVE CHROMATOGRAPH BUFFER

CALL F*IOStIOSPUT»CNTRLD»TTY.H)

GET NUMBER OF RECORDS TO BE SENT

READ(TTY >106) IF<NREC<EG<0)

NREC GO TO 45

RETRIEVE THE BUFFER

DO 40 1=1»NREC READITTY.108) (Z80DAT(J).J=1.40)

SAVE DATA ON DISK

CONTINUE

OUTPUT THE T-1

CONTINUE

HINUTE ANALYZER AND TRANSDUCER VALUES

»ERROR COUNT? 1 LABELS

URITEtTTY.102) RECORD.TIME(DATE URITE(TTY»112) DO 50 1=1.3

URITE<TTY.110) YNAME<I).FLUE(I).PCNT. GNAHECI).AIR(I)>SCFH.UNITS(I) CONTINUE

URITE(TTY.llO) YNAHE(4)»FLUE(4).PPHV

SAVE DATA ON DISK

CALL F$OPN(DISK) CALL .FtIDS(RANPUT.RDATA.DISK.H) CALL F*IOS<RANPUT.KDATA.DISK.H) CALL FiCLS(DISK) RETURN

FORHAT(/'*** ALL RECORDS FILLED. DELETE REQUIRED') FORHATC/'*** RECORD'.13.5X>'TIME'.13.'i'.I2»'!'.I2.

5X.'DATE'.13.'/'.12.'/'.125 FORHATt16Z4) FORHAT(Z2) F0RHAT(40A2) FORMAT <10X.A4.F8.2.IX.A4.6X.A4.F8.2.IX.A4. 4X.F8.2.' inches H20') FORHAT(/'*** ANALYZER AND TRANSDUCER OUTPUTS!'/) FORHATt/'... Enter the air temperature: C=D Fahrenheit') FORHATt'... Enter '»A4.' pressure: t=J psia')

END

) 10 ) 20

0041 0051

0000. PSECT SIZE! VARIABLES

RECORD 0001 C LPROBE 0002 C

0922. DSECT SIZE! ARRAYS

0026i REV. PROCEDURES

DATE TIME

0003 C 0006 C

F«OPN F*MD1

00E8 00E9

09/16/80 BLOCKNAHES

DATA 0066 TEMPER 0030

120

)100 02FS KCOAL 0091 C RDATA 0000 c FIIOS 02F5 LUN 0004 )22 0085 BLANK OOOC P IDATA 0000 c F*CLS 02F6 NAME 0040 >114 036C TTY 0000 C JDATA 0000 c F»URF OOEC MAXPIW 00C1 >25 00E2 DISK 0001 C KNAME 0093 c F*TEF OOED SYSTEM 0078 >116 0386 HAXREC 0002 C NAME 0045 c F»RET 02F7 SEARCH 0078 >104 0332 IREC 0003 C Z80DAT 0000 c TIMEIB OOEF VECTOR 00B1 >32 0125 M OOCO C CNTRLD 0000 p DATEIB OOFO

VECTOR 00B1 ) 33 0148 RANGET OOOD P CNTRLA 0003 p DOEINP 00F1 >36 01CE RANPUT OOOE P KDATA 004E c FIARF 00F4 ) 38 0234 IOSPUT OOOF P AIR OOOB c FiREF 01D5 ) 106 8225 J 0010 P PRQX 0029 c F*V01 01D6 >45 0270 NREC 0011 P ULTIH 0031 c F*E10 OlDA >40 0269 I 0012 P FLUE 0011 c >108 0337 K 0013 P SHOKE 003B c >102 030E ZERO 0014 P PRESSR 006F c >112 0357 SCFM 0016 P KPROX 0077 c >50 02C7 PCNT 0018 P KULTIH 007F c >110 033A PPMV 001A P KSMOKE 0089 c

RANKIN 001C P LFE 0006 p TSTAND 001E P A 0002 c HG1ATM 0020 P TSLOPE 0002 c TUCSON 0022 P TEASE 0032 c GAUGE 0024 P XNAHE 0000 c TSAMf'L 0009 c YNAME OOOC c COAL 0043 c SNAHE 0024 c AIRTMP 0075 c PNAME 002C c •AIA 0009 CNAHE 0034 c •AIB OOOA GNAME 0038 c ANS OOOB T 0000 c •AIC OOOD UNITS 0000 c •AID OOOE IDATA1 0000 c •AIE OOOF JDATA1 0000 c BASE 0010 KDATA1 0000 c •AIF 0012 •AIG 0013 •ARH 0014 •ARI 0016 • ARD 0018

0001SC 0002!C=== 00035C 0004: 0005!C 0006IC 00075C 0008:c 0009: c ~ ~ 38! ooio:c ooii: 0012'C 0013: 0014: 0015: ooi6: ooi7: 0018SC ooi9: 0020: 002:: 0022! 0023:c 0024: 0025: 0026: 0027: 0028!C 0029: 0030! + 003i: + 0032: +

sssssssssssss

SUBROUTINE DOENTR

THIS SUBROUTINE ALLOWS THE OPERATOR TO FILL A DATA RECORD FROM THE TELETYPE.

ssssBS5SESss:ssssass3EBss=SB:=s33:sss=ssss:8Bsssssas:ss:s3ssass

LOGICAL BLANK

INTEGER RECORD>LPROBE>DATE(3)rTIME(3> »RDATA<102) INTEGER HRSFD«R»RANPUT»RANGET INTEGER DISK»TTYrKDATA(102> INTEGER KNAME(20>>NAME(20) INTEGER IC0HP<12)

REAL AIR(3> fPR0X(4)»ULTIM(5>iFLUE(12)>SM0KE(4)>PRESSR(3) REAL KF'R0X<4) t KULTIM(5) r KSH0KEC4) »KCOAL REAL XNAHE<6>iYNAHE(12)»SNAHE<4> »PNAME<4) REAL CNAhE(2)rGNAHE(4)

S8BB8H flruiL / TTr.DISKfHAXREC.IREC COMMON /DATA / RDATA COMMON /MAXPIV/ UNITS(96)FM COMMON /NAME / XNAHErYNAHErSNAHErPNAMErCNAHErGNAME

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0104 0105 C 0106 c 0107 c 0108 5 0109 0110 0111 0112 0113 0114 c 0115 c 0116 r 0117 10 0118 0119 0120 0121 0122 0123 c 0124 c 0125 c 0126 c 0127 20 0128 012? 0130 0131 0132 0133 0134 22 0135 0136 C 0137 C 013B C 013? 25 0140 0141 0142 0143 0144 C 0145 0146 0147 0148 014? 0150 27 0151 0152 C 0153 C 0154 C 0155 30 0156 0157 otss 0159 0160 0161 0162 0163 32 0164 0165 C 0166 c 0167 c 0168 35 0169 0170 0171 0172 0173 0174

GO T0(45f30F35F50F25F60F20F40F10F55)iIANS

PUT CHANGES ON DISK

CONTINUE CALL FSOPN(DISK) CALL F$IOS(KANPUTfRDATAfDISKfM) CALL F$IOS<RANPUTFKDATAfDISKfM) CALL FiCLS(DISK) RETURN

OBTAIN FLUE GAS TEMPERATURE

CONTINUE URITE(TTYfHO) CALL DOEINPfANSfBLANKFTTY) IF(.NOT.BLANK) TSAMPL=ANS CALL DOECHO(TSAHPL) GO TO 1

OBTAIN AIR FLOUS

CONTINUE HO 22 1=1»3

URITE(TTYf 112) GNAME(I) CALL DOEINP(ANSrBLANKiTTY) IF(.NOT.BLANK) AIR(I)=ANS VALUE=AIR(I) CALL DOECHO(VALUE) CONTINUE

GO TO 1

OBTAIN THE AIR TEMPERATURE AND GAUGE PRESSURES

CONTINUE URITE(TTYf106) CALL DOEINP < ANSiBLANK»TTY) IF(.NOT.BLANK) AIKTMP=ANS CALL DOECHOtAIRTMP)

DO 27 1=1.3 URITE(TTYf117) GNAMEU) CALL DOEINPIANSiBLANKiTTY) IF<.NOT.BLANK) PRESSR(I)=ANS CALL DOECHO(PRESSRd)) CONTINUE

GO TO l

OBTAIN PROXIMATE ANALYSIS

CONTINUE URITE(TTYrl20) DO 32 1=1>4

URITEtTTYtllS) PNAME(I) CALL DOEINP(ANSfBLANKFTTY) IF(.NOT.BLANK) PROX(I)=ANS KPROX(I)=PRQX(I) CALL DOECHO<PROX(I)) CONTINUE

GO TO 1

OBTAIN ULTIMATE ANALYSIS

CONTINUE URITE(TTY f122) DO 37 1=1f5

MRITE(TTYf118) XNAME(I) CALL DOEINP(ANS.BLANK.TTY) IF(.NOT.BLANK) ULTIH(I)=ANS CALL DOECHO(ULTIM(I))

01755 0176*37

Bi ic 0179JC 0180'C 0181140 0182! 0183S 0184! 0185S 0186! 0187*. 0188:42 0189: 0190: 0191! 0192: 0193! 0194S43 0195! o m : c 0197-.C o i 9 8 : c 0199:45 0200: o ? o i : 0202: 0203: 0204! 0205: G206:c 0207JC 0208:c 0209:50 0210: 0211: 0212: 0213! 0214*. 0215! 021&: 0217:52 0218: 0'219:c 0220JC 0221:c 0222:55 0223! 0224! 0225! 0226! 0227! 0223: 0229! 0230:C 0231:c 0232:c 0233'.60 0234! 0235! 0236: 0237! 0238*. 0239S65 0240! 024i:C 0242:c 0243:100 0244:103 0245:104

KULTIMd>=ULTIM(I) CONTINUE

GO TO 1

OBTAIN FLUE GAS ANALYSIS

CONTINUE URITE(TTY»124) DO 42 1=1(6

URITE<TTY»118) YNAMEtICOMP(I)) CALL DOEINP(ANSIBLANKITTY) IF(.NOT.BLANK) FLUE(ICOMP(I))=ANS CALL POECHO < FLUE(ICOMPD))) CONTINUE

D0 URITE(TTYF 119) YNAME(ICOMPd)) CALL I'OEINP(ANS»BLANK»TTY) t _ IF(.NOT.BLANK) FLUE(ICOMP(I>)=ANS CALL DOECHO(FLUEdCOMPd))) CONTINUE

GO TO 1

OBTAIN COAL INPUT RATE

CONTINUE URITE(TTY F126) CALL DOEINP(ANS r BLANK»TTY) IFC.NOT.BLANK) COAL=ANS CALL DOECHO(COAL) KCOAL=CQAL GO TO 1

OBTAIN SMOKE ANALYSIS

CONTINUE URITE(TTY»128) DO 52 1=1>4

URITE(TTYill8) SNAME(I) CALL DOEINP(ANSFBLANK{TTY) IF(.NOT.BLANK) SMOKE(I)=ANS CALL DOECHO(SMOKEd)) KSMOKE(I)=SMOKE(I) CONTINUE

GO TO 1

OBTAIN PROBE POSITION

CONTINUE

CALLEDOEINP(ANS r BLANK.TTY)

IH?NOT!BLANK) JLPROBE=IANS VALUE=LPROBE CALL DOECHOtVALUE) GO TO 1

OBTAIN SAMPLE NAME

CONTINUE URITECTTY1132) READCTTY»103) NAME URITE(TTY»103) NAME 00 65 1=1F 20 KNAME(I)=NAHED)

CONTINUE GO TO 1

FORMAT(//'... Modify uhich data record?') F0RHAT(40A2) „ ^ FORMAT!/'... Data Entry Options*.'/

124

'i 0246i 0247! 0248'. 024?: 0250: 0251! 0252!105 02531106 0254:110 0255:112 0256!117 0257:118 0258!119 0259 J120 0260:122 0261U24 02621126 0263!128 0264:130 0265!132 0 2 6 6 : c 0267! »ERR0R COUNT!

1 LABELS

= Coal Feed Rate'rlOXi'7 = Air Input Rates'/ = Proxiaate Analysis'«6X»'8 = Flue Gas Analysis'/ = Ultimate Analysis'i7X»'9 = Flue Gas Temperature'/ = Flue Solids Analysis'i3X>'10 = Probe Position'/ = Air Teaperature and Pressures'/ = .Coal Sanple Naae')

. Enter the data option:') Air Tenperature: t=] Fahrenheit') Flue Gas Teaperature! C=] Celsius') '»A4»' Air = ? C=] SCFH') '>A4r' Pressure' t=] psia') Percent '»A4»' = ?') PPMV 'tA4f' = ?')

* Froxiaate Analysis! (As-Received Basis)') * Ultimate Analysis: (Dry* Ash-included Basis)') * Flue Gas Analysis:')

[=] lbs/hour') (Ash-Free Basis)')

F0RMAT(/ F0RHAT( " FORMAT < FORMAT( FORMAT( F0RHAT( FORMAT( FORMAT( FORMAT( FORMAT( FORMAT( FORMAT( FORMAT( FORMAT(

Coal Feed Rate = ? * Flue Solids Analysis! •• Probe Position = ?') .. Input Sanple Naite')

END OOOOf PSECT SIZE!

VARIABLES 1306r DSECT SIZE! 0012! REV. 5

ARRAYS PROCEDURES

) 100 ) 15 >12 )2 ) 104 )1 ) 105 )5 >45 >30 >35 >50 >25 >60 >20 >40 ) 10 >55 >110 > 2 2 >112 >106 >27 >117 >120 >32 >118 > 1 2 2 >37 >124 >42 >43 >11? > 1 2 6 >128 >52 >130 >132 >103 >65

oooi:c 0002!C= 0003IC 0004! 0005!C

037B 0084 007D 00A2 0390 00A8 0422 OOEC 02B3 0196 01E3 02K0 014B 033C 0115 022A OOFD 0317 0446 0144 045B 0432 018F 046B 0495 01DC 047C 04AD 0224 04C7 026A 02AC 0489 04D4 04E9 0311 0500 050D 038D 0367

BLANK RECORD LPROBE H S D Y RANPUT RANGET

KCOAL HAXREC IREC M NOPT I IANS VALUE ANS TSAMPL COAL AIRTMP •ALA •AIA • AIB

0000 0001 0002 0001 0002 0003 0004 0005 0006

m 0091 0002 0003 00C0 0013 0014 0015 0016 0018 0009 0043 0075 0009 000A 000B

p DATE 0003 C F»MRF 036E c TIHE 0006 C FSTEF 036F c RDATA 0000 C DOEINP 0370 p KDATA 004E C FtMDl 0371 p KNAME 0093 C FiVIO 0374 p NAME 0045 C FiRET 00D6 p ICOMP 0007 P F*0PN 00D7 p AIR 000B C FtlOS OOD8 p PROX 0029 C F$CLS OOD9 c ULTIM 0031 C QODA c FLUE 0011 C OODB c SMOKE 003B C FtGOT 01AA c PRESSR 006F C DOECHO 01AC c KPROX 0077 C F*ARF 01AD c KULTIM 007F c F$V01 0379 p KSMOKE 0089 c F*REF 037A p XNAME 0000 c p YNAME OOOC c p SNAME 0024 c p PNAME 002C c c CNAME 0034 c c GNAME 0038 c c UNITS 0000 c

09/16/80 BLOCKNAMES

LUN 0004 DATA 0066 HAXPIV 00C1 NAME 0040

SUBROUTINE DOEINP(ANSrBLANK>LUN)

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0034 0058

VALUE 0009 IOSTEH 0009 P FtSBU 0051 DISK 0001 C lOSBUF 0000 P F*MD1 0052 TTY 0000 C FtENC 0053 HAXREC 0002 C FtARF 0054 IREC 0003 C F»TEF 0055 IOSPUT 0014 P FSIOS 0056 I 0015 P F*RET 0057 NOUT 0016 P M 0017 P •AIA OOOA

09/16/80 BLQCKNAMES

LUN 0004

127

c c=== c c c

c c== c

D.O.E. COAL FURNACE COHHON ALLOCATION FOR SHARED DSECT

BLOCK DATA sss&sssssssassBsssssBssssassasssscsssssssssssBSSsaisasssi&sassa

INTEGER RDATA(102).DISK.TTY

LOGICAL 02RICH.COGGIN>CHROHO.DEBUG.RESET>SHIFT.SSQHIN

REAL CNAHE(2>.GNAME<4> REAL XNAME < 6).YNAHE <12).SNAHE(4)»PNAME<4)

DOUBLE PRECISION SRiAIRSR DOUBLE PRECISION Q.U.X.Y.S.P.T. QDATA.UDATA.XDATA.YDATA.SDATA.PDATA.TDATA DOUBLE PRECISION LASTZ<22>.DELZC22)

COMMON /DATA / RDATA COMHON /INDEX / INDEX(30) COMMON /TEHPER/ TAXIS(24) COMHON /UEIGHT/ UEIGHT(30) COMHON /GAHHA / SR.AIRSR COMMON /LUN / TTY.DISK.HAXREC.IREC COMMON /DEBUG / DEBUG.RESET.SHIFT.SSQHIN COMHON /BURN / 02RICH.COGGIN.CHROHO COHHON /NAME / XNAHE .YNAHE .SNAHE .PNAHE.CNAHE .GNAHE COMHON /SYSTEM/ G<4)>U<2)»X<6).Y<12).S<4).P.T COMHON /SEARCH/ QIiATA(4)»UDATA(2).XDATAI6)»YDATA(12).

SDATA(4).PDATA.TDATA COMHON /VECTOR/ LASTZ . DELZ»NSERCH COHHON /HAXPIV/ UNITS<96).NSIZE

DATA TTY.DISK.HAXREC.IREC/20.53.90.0/

DATA RDATA/200i1»100*0/

DATA CNAHE/'COAL' 0042 DATA XNAHE/' C ' ' H ' ' 0 0043 + ' S ' ' N ' ' H20' / 0044 DATA YNAHE/' C02' ' CO ' ' 02 . 0045 ' NO ' ' HCN' ' CH4 . 0046 + ' H2S' ' S02' ' NH3' » 0047 + ' H2 ' ' H20 ' N2 ' / 0048 DATA SNAHE/' C ' ' H ' ' N . S / 0049 DATA PNAHE/'F.C.' 'V.M.' ' ASH' . H20' / 0050 DATA GNAHE/'TRNS' 'PRHT' 'STGD' . FLUE' /

FLUE'/

»ERROR COUNT! 1 LABELS

DATA INDEX/1>2»3»8r9»10.11»12»13.15.16»5»26»27>28»30r17t18*19»21/ DATA UEIGHT/29*1.0.10.0/

END 0000. PSECT SIZE!

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ARRAYS PROCEDURES 09/16/80 BLOCKNAHES

DISK TTY 02RICH COGGIN CHROHO DEBUG RESET

IÎN SR AIRSR P

0001 0000 0000 0001 0002 0000 0001

88§§ B 0000 c 0004 C 0070 C

RDATA CNAHE GNAHE XNAHE YNAHE SNAHE PNAHE Q U X Y S

0000 0034 0038 0000 OOOC 0024 002C

88?8 0018 0030 0060

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0060: 0061! 0062! 0063140 0064SC 0065: c 0066:c 0067! 0068: 0069: 0070: oo7i:c 0072! 0073:c 0074!

IF<IOPT.NE.3) GO TO 40 J0BSJ0B27 CALL DOERPT CONTINUE

SUAP TASKS TO EXECUTE THE OPTION

CALL DOESTK(PUSH) CALL TPNf1(JOB*NOUfMODE) CALL RSFOF IF<.TRUE.) GO TO 10

A=ALOG(A)

.END

1 »ERROR COUNTS 0000> PSECT SIZE*. 0122» DSECT SIZES 0001! REV. 5 09/16/80

LABELS VARIABLES ARRAYS PROCEDURES BLOCKNAMES )10 001B RECORD 0003 C NOU 0000 P FREMAT 006D DATA 0066 )20 0044 ANS 0002 P RDATA 0000 C DOESTK 006E LUN 0004 )30 0053 TTY 0000 C FSOPN 006F DEBUG 0004 >40 005A DISK 0001 c FSIOS 0070

DEBUG 0004

RANGET 0003 p F*CLS 0071 RANPUT 0004 p F$MD1 0072 PUSH 0005 p DOEOUT 0073 PULL 0006 p DOERPT 0074 DEBUG 0000 c TPN«1 0075 RESET 0001 c RiFOF 0076 SHIFT 0002 c ALOG 0077 SSQMIN 0003 c FIXIT 0079 MAXREC 0002 c JOB 0007 p J0B27 0008 p J0B3 0009 p MODE OOOA p IOPT OOOB p NO OOOC p M OOOD p A OOOE p •ALA 0000

OOOliC 0002 SC 0003SC 0004: 0005SC 0006:c 0007SC ooo8:c=» 0009:c ooio: ooii:c 0012: 0013! 0014!C 0015: 0016: 0017! oois: ooi9:c 0020: 0021: 0022! 0023! 0024: 0025: 0026: 0027: 0028*. 0029! 0030:c

SUBROUTINE DOERPT

THIS ROUTINE OUTPUTS THE RESULTS OF THE COGGIN SEARCH.

EXTERNAL DOEBTA

INTEGER TTY.BISK INTEGER IY(10)>I TEMP(40)>INDEX(25)

LOGICAL 02RICH>C0GGINrCHROMO LOGICAL DELETE(30) tREJECT(30) LOGICAL VERIFY>DEBUG>RESETtSHIFTrSSQHIN LOGICAL TRUE>FALSE>CONSIS

COMMON /LUN / TTY>DISK>MAXREC»IREC COMMON /BURN / 02RICHiCOGGIN*CHROMO COMMON /NAME / XNAME(6>.YNAME(12)»SNAME(4)r

PNAME (4). CNAME (2). GNAME (4) COMMON /SYSTEM/ 0(4)fU(2)»X(6)rY(12)»S<4)»P»T COMMON /SEARCH/ QDATA(4)»UDATA(2)»XDATA(6)»YDATA<12)»

SDATA(4)rPDATAiTDATA COMMON /VECTOR/ DELZ<44)rNSERCH COMMON /MAXPIV/ UNITS(96)»K COMMON /DEBUG / DEBUG>RESETiSHIFTfSSQHIN

130

0031! 0032! 0033! 0034: 0035: 0036! 0037:C 0038: 0039JC 0040! 0041: 0042! 0043! 0044! 0045: 0046! 0047! 0048: 0049: ooso: oo5i: 0052! 0053:c 0054! 0055! 005&: 0057! 0058: 0059! 0060: 0061! 0062: 0063iC 0064: 0065:c 0066ZC 0067:c 0068: 0069! 0070! 0071! 0072! 0073!1 0074:c 0075!c 0076:c

m\ 0079! ooeo: oo8i: 0082: 0083: 0084:2 0085: 0086SC 0087:c 0088JC 0089:4 0090! 0091: 0092: 0093: 0094: 0095: 0096! 0097! 0098: 0099: oioo: oioi: A

DOUBLE PRECISION DMEAN.DSIGHA DOUBLE PRECISION DELZ.DZERO DOUBLE PRECISION Z(1)»ZDATA(1) DOUBLE PRECISION Q.U.X.Y.S.P.T.TEMP1.TEMP2 DOUBLE PRECISION SCFHTDECISN.ACCPT.REJCT.

+ QDATA.UDATA.XDATARYDATA.SDATARPDATA.TDATA

REAL TVALUE(30)(CHANGE(30)

EQUIVALENCE (BETA.UNITS(2)). <N.UNITS(3>> EQUIVALENCE <Z<1)»QU)>» (ZDA1A(1).QDATA<1)) EQUIVALENCE (RMEAN.DHEAN)» (SIGMA.DSIGHA) EQUIVALENCE (TVALUED) »UNITS(37)) » (CHANGE (1) .UNITS(67)) EQUIVALENCE (DELETE(L)»UNITS(22)). (REJECT(L)»UNITS(7>) EQUIVALENCE (DHEAN»DELZ(31))» <DSIGHA.DELZ(32)) EQUIVALENCE (TEHP1.DELZ(33)>T (TEMP2.DELZ(34>> EQUIVALENCE (ITEHP(1)>BELZ(35))> (J.ITEMP(1>> EQUIVALENCE ITEHP(2> >» (NUIITEHP(3)> EQUIVALENCE (BSAVE.ITEHP(5))» (DEGREE.ITEMP(7)) EQUIVALENCE (F.ITE«P(9)). (DF.ITEMP(11)) EQUIVALENCE (GAMMA.UNITS(4>>. (C.UNITS(5)> EQUIVALENCE (DECISN.ITEMPU3))

DATA TRUE.FALSE/.TRUE...FALSE./. VERIFY/.TRUE./ DATA FILTER/0.0005/. A>B.C0EF/0.0»0.5»0.0/ DATA ACCPT.REJCT/' YES '/ DATA DZERO/O.ODO/. ZERO.ONE.TUO/O.0.1.0.2.0/ DATA ALPHA.TOLER.PI/O.95.0.001I3.14159/ DATA NYDATA /10/» IFORM /ZOCOO/. SCFH /0.1705DO/ DATA IY/1.2.3.4.5.7.9.6.10.12/. BLANK/' '/ DATA INDEX/1.2.3.7.8.9.10.11.12.13.14.15.16.

+ 25.26.27.28.5.30.17.18.19.21.22.24/

URITE(TTY.116) IFORM

DETERMINE THE NUMBER OF POSSIBLE DATA POINTS

NSERCH=13 IF(02RICH) GO TO 1 NSERCH=19 IF(.NOT.CHROMO) GO TO 1 NSERCH=25 CONTINUE

INTIALIZE THE LOGICAL VECTORS

D0 J=1NJEX?5)CH REJECT(J)=FALSE DELETE(J)=TRUE TVALUETJ)=ZERO IF(ZDATA(J).EQ.DZERO) GO TO 2 DELETE(J)=FALSE CONTINUE

IF(RESET.OR..NOT.SHIFT) DELETE(30)=TRUE

COMPUTE THE MEAN DATA ADJUSTMENT

CONTINUE N=0 DMEAN=DZERO DEGREE=ZERO DO 6 I=1.NSERCH

J=INDEX(I) IF(DELETE(J).OR.REJECT(J)) GO TO 6 N=N+1 DELZ(N)=DABS((ZDATA(J)-Z(J)>/ZDATA(J)) CHANGE(J)=SNGL(DELZ(N)) IF(CHANGE(J).GT.DEGREE) DEGREE=CHANGE(J) DMEAN=DMEAN+DELZ(N) CONTINUE

131

0102: 0103! 0104: oios:c 0106SC oio7:c oio8: 0109! o i io: 0111:10 0112: 0U31C oii4:c 0115:c 0116: 0117! 0118: oii?:c 0120:0 oi2i:c 0122: 0123:15 0124IC 0125SC 0126:c 0127:c 0128! 0129:c 0130:c oi3i:c 0132! 0133: 0134! 0135: 0136: 0137! 0138! 0139! 0140: 0141: 0142:20 0143:c 0144: c 0145:c 0146: 0147! 0148! 0149'.C oiso:c 0151:c 0152! 0153: 0154i 0155! ois&:c 0157:c 0158:c 0159:28 oi6o:c 0161 :c 0162SC 0163! 0164:c oi65:c 0166IC 0167! 0168! 0169! 0170! oi7i: 0172:

CONSIS=DEGREE.LT.FILTER DMEAN=DMEAN/N NU=N-1

COMPUTE THE STANDARD DEVIATION OF DATA ADJUSTMENTS

DSIGMA=DZERO DO 10 1=1»N

DSI GMA=DSI GMA+ < DELZ11) -DME AN) **2 CONTINUE

DSIGHA=DSQRT(DSIGMA/NU)

COMPUTE THE STUDENT-T VALUES FOR EACH DATA ADJUSTMENT

DO 15 1=1rNSERCH J=INDEX(I) IF(DELETE(J>.OR.REJECT(J)) GO TO 15

FORH THE NORMALIZED STUDENT-T VARIABLE

TVALUE < J)=ABS ( CHANGE(J >-RMEAN)/SIGHA CONTINUE

DETERMINE THE REJECTION CONSTANT FOR A GIVEN CONFIDENCE: ALPHA/2. UITH A NEUTON RAPHSON ALGORITHM

BETA=0NE-4.0*FL0AT(N)/NU**2

EVALUATE THE COEFFICIENT OF THE BETA FUNCTION

A=(FLOAT(NU)-ONE)/TUO DEGREE=A CALL DOEGMAtDEGREE 1 GAMMA) COEF=GAMMA DEGREE=B CALL DOEGMA(DEGREE»GAMHA> COEF=COEF*GAHMA DEGREE=AiB CALL DOEGMA(DEGREE tGAMMA) COEF=GAHMA/COEF CONTINUE

EVALUATE THE DERIVATIVE

BSAVE=8ETA DEGREE=(NU+ONE)/TUO [iF=COEF*(BETA**(A-ONE))/SORT(ONE-BETA)

EVALUATE THE FUNCTION

F=DOEGAU( DOEBTA )-(ONE-ALPHA)/TMO BETA=BETA-F/DF BSAVE=ABS(<BETA-BSAVE)/BETA) IF(BSAVE.GT.TOLER) GO TO 20

CONVERGENCE ACHEIVED

CONTINUE

COHPUTE THE ANSCOMBE CONSTANT FOR OUTLYING T-VALUES.

C=SORT((ONE-BETA)/FLOAT(N))*NU

CHECK FOR OUTLYING T-VALUES

IF(CONSIS) GO TO 60 DO 35 1=1iNSERCH

J=INDEX(I) IF(DELETE(J).OR.REJECT(J)) GO TO 35 CHANGE(J)=ABS(CHANGE(J))*100.0 IFUVALUE(J).LE.C) GO TO 35

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EQUIVALENCE (DOEGAU•SUN)

REAL X(7>,U<7)

DATA ZER0,0NE/0.0,1.0/, 1/0/

CONSTANTS FOR GAUSSIAN QUADRATURE

DATA X

DATA U

/.20119409,.39415135,.57097217, .72441773,.84820658,.93727339,.98799252/

/.19843149,.18616100,.16626921, .13957068,.10715922,.07036605,.03075324/

DATA UO/.20257824/

COKPUTE THE INTEGRAL

SUM=FOFX(ZERO)*UO DO 10 1=1.7

SUM=SUM+FOFX(X(I))*U(I> SUM=SUM+FOFX(-X(I>>*U<I) CONTINUE

RETURN END

»ERROR COUNT: 0000, FSECT SIZE. 0099, DSECT SIZE! 00175 REV. 5 LABELS VARIABLES ARRAYS PROCEDURES

09/16/80 BLOCKNAHES

) 10 0054 DOEGAU OOOA X 0000 P FOFX 0009 ZERO 001C P U OOOE P FtSBU 005D ONE 001E P F«RER 0062 I 0020 P UO 0021 P SUM OOOA •AIA OOOC *AIB OOOD tAIC OOOE •ARD OOOF

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881 1 0028! 0029: 0030:

SUBROUTINE DOESTK(IOPT)

THIS ROUTINE STORES/RETRIEVES LABELED COMMON DATA TO/FROM THE DISK DURING TASK SWAPPING.

INTEGER RDATA(102),DISK,TTY INTEGER BUFFER(l),PULL,PUSH,NULLC3)

LOGICAL 02RICH.C0GGIN,CHR0M0,DEBUG,RESET,SHIFT,SSQMIN

REAL CNAHEI2),GNAME(4) REAL XNAME(6 >,YNAME(12),SNAME(4),PNAME< 4 >

DOUBLE PRECISION SR,AIRSR DOUBLE PRECISION Q,U,X,Y,S,P,T, QI1ATA,UDATA,XDATA,YHATA,SDATA,PDATA,TDATA DOUBLE PRECISION LASTZ(22),DELZ(22)

EQUIVALENCE (RDATAC3),BUFFER(1))

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X(I)=X(I)*<100.-PROX<3)) CONTINUE

Y(IF(7))=Y(IF<7))*100.

DO 30 I=8>12 Y(IF(I) )=Y(IF(I) X1000000. CONTINUE

DO 45 1 = 1 F4 S( I)=S(I)*(1.0-SASH)*100. CONTINUE

SASH»SASH*100.

URITE(TTY»115) URITE(TTY»120) X(1)TXNAME(1)IS(1)ISNAME(1)>Y(1)IYNAME(1)>Y(4)

+ FYNAHE<4) URITETTTY1120) X(2)FXNAHE(2)»S(2)RSNAHEC2)TY(2)RYNAHEC2)IY(5)

+ FYNAME(5) URITE(TTYI120) XC3)»XNAHE(3)»S(3)»SNAHE(3)»Y(3)»YNAHE<3>FY<7>

+ >YNAME<7) URITE(TTYF120) X(4)FXNAME<4)FS<4)FSNAHE<4)FY(6)FYNAHEC6)FY<8)

+ FYNAHE(8) URITE(TTYF120) X(5)FXNAHE(5)FSASHFASHFY(10)FYNAHE(10)FY(9)

+ IYNAME(9) URITE(TTYF122) X(6)FXNAHE(6)FY(LL)FYNAHE(11) URITE(TTYF122) PR0X<3)FASHFY<12)FYNAME<12)

RESTORE FLUE FRACTIONS FROH PERCENTAGES AND PPHV

DO 25 1=1F 6 YTIF(I))=Y(IF(I))/100. X(I)=X(I)/(100.-PR0XC3)) CONTINUE

Y(IF(7))=Y(IFC7))/100.

DO 35 IS8F12 Y(IF(I))=Y(IF(I))/L000000. CONTINUE

DO 40 1=1F4 S( I)=S(I)/<100.-SASH) CONTINUE

HRITE(TTY F124)

RETURN

F0RHAT(//A2F'*** RECORD'.I3F5XF'PROBE'FI3F5XF + I2F'/'FI2F'/'FI2F5XFI2F':'FI2F'!'FI2F5XF40A2) F0RHAT(//24XF' [=]'F2XF'LB/HR'.13XF'KG/S'//

+ '***'F6XF' COAL INPUT RATE = 'F1PE10.3F7XF1PE10.3/ + '***'F3XF' FLUE SOLIDS OUTPUT = 'F1PE10.3F7XF1PE10.3) FORMAT(/24XF ' C = 3' F2XF 'SCFM' F 13XF 'MM3/S'//

+ '***'F6XF' FLUE GAS OUTPUT = 'F1PE10.3F7XF1PE10.3/ + '***',7X.' AIR INPUT RATE = 'F1PE10.3F7XF1PE10.3//F12X T 'TRANSPORT AIR = 'F1PE10.3F7XF1PE10.3/F12X + 'SECONDARY AIR = 'F1PE10,3F7XF1PE10.3/F12X + ' STAGED AIR = 'F1PE10.3F7XF1PE10.3// + '***'F3XF' STOICHIOMETRIC AIR = 'F1PE10.3F7XF1PE10.3// + ' STOICHIOMETRIC RATIO = 'FOPF5.2) F0RMAT</4XF'COAL'FIIXF'FLUE SOLIDS'F8XF'FLUE GAS'F9XF'FLUE GAS'

+ ' PERCENTAGES 'F5XF' PERCENTAGES 'F5XF' PERCENTAGES 'F5XF + 'TRACE PPHV'/) F0RMAT(4(F8.2FA4F5X)) F0RHAT(F8.2FA4F5XF17XF2(F8.2FA4F5X)> F0RMAT(11(/))

END »ERROR COUNT: OOOOF PSECT SIZE! 1461F DSECT SIZES 00258 REV. 5 1 LABELS VARIABLES ARRAYS PROCEDURES

09/16/80 BLOCKNAHES

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0031: END »ERROR COUNT: 0000. PSECT SIZE: 0095. DSECT SIZE: 0018? REV. 5 1 LABELS VARIABLES ARRAYS PROCEDURES

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T 0074 C QDATA 0000 c PDATA 0070 C UDATA 0010 c TDATA 0074 C XDATA 0018 c MAXREC 0002 C YDATA 0030 c IREC 0003 C SEAT A 0060 c NSERCH OOBO C LASTZ 0000 c NSIZE OOCO C DELZ 0058 c

INDEX 0000 c TAXIS 0000 c UEIGHT 0000 c UNITS 0000 c

MAXPIV 00C1

0001:c 0002.C 0003SC 0004:c ooos:c 0006!C=== ooo7:c 0008: ooo?: ooio:c ooii: 0012JC ooi3: ooi4: 0015! ooi&:c ooi7: 0018: 0019! 0020: 0021:c 0022: 0023!c 0024:10 0025SC 0026:c 0027:c 0028: 0029 JC 0030:c oo3i:c 0032: 0033: 0034: 0035! 0036: 0037!C 0038! 0039:c 0040:c 004i:c 0042! 0043! 0044: 0045: 0046! 0047:20 0048!C 0049:c 0050:c oosi: 0052! 0053: 0054! 0055*. 0056J30 0057:c 0058:c 0059:c

:SSG33SSS3SSSSSSS3SSSSSS23SS5 = ESSSSSS3SS=SS88SS8a3ZaS5ESSSSSMES

D.O.E. FURNACE CPU INTENSIVE MAIN-LINE

= SS3 = SS = = = FI3:S

INTEGER RDATA(102)FTTYfDISKFN0U(2) INTEGER RANGETFRANPUTIPUSHFPULL

LOGICAL DEBUGFRESETFSHIFTFSSQHIN

COMMON /DATA / RDATA COMMON /LUN / TTYFDISKFMAXRECFIREC COMMON /DEBUG / DEBUGFRESETFSHIFTFSSQHIN

DATA JOBfJ0B6FJ0B27/0F6F27/ DATA M0DEFI0PT/2*0/F N0U/0F4/ DATA RANGETFRANPUT/Z105FFZ109F/ DATA PUSHFPULL/0F1/F A/O.O/

CALL FREMAT

CONTINUE

RETRIEVE LABELED COMMON

CALL DOESTK(PULL)

GET THE OPTION FROM THE STATUS RECORD

RDATA(2)=MAXREC+1 CALL FiOPN(IiISK) CALL F«IOS(RANGET»RDATAFDISK»HODE> CALL FtCLS(DISK) I0PT=RDATA<4)

IF(IDPT.LT•1.OR)IOPT.GT.2) GO TO 10

CHECK FOR MASS BALANCE

IF(IOPT.NE.l) GO TO 20 JOB—J0B6 RESET=.FALSE. CALL DOECNV CALL DOENEU CONTINUE

CHECK FOR A COGGIN SEARCH

IF(IOPT.NE.2) GO TO 30 J0B=J0B6 DEBUG=.FALSE. CALL DOESET

JMP J0B=JGB27

PUT THE OPTION ON THE DISK

145

0060! 0061! 0062*. 0063! 0064! 0065! 0066S 0067JC 0068:c 006?:c 0070: 0071! 0072 J 0073! 0074! 0075J 0076SC 0077!

I0PT=I0PT+1 RDATA(2)=MAXREC+1 CALL F»0PN(DISK> CALL F*IOS(RANGET>RDATA»DISK.MODE) RDATA<4)=I0PT CALL F$IOS(RANPUT>RDATAfDISKfHODE) CALL FtCLS(DISK)

SWAP TASKS TO EXECUTE THE OPTION

CALL DOESTK(PUSH) CALL TPNf1(JOBrNQUiMODE) CALL RiFOF IF(.TRUE.) GO TO 10 A=ALOG(A) A=DLOG(A)

END ERROR COUNT! OOOOr PSECT SIZE! 0156. DSECT SIZE! 0001; REV. 5 LABELS VARIABLES ARRAYS PROCEDURES

) 10 0018 TTY 0000 C RDATA 0000 c FREMAT 008B >20 0046 DISK 0001 C NOU 0000 P DOESTK 008C >30 0058 RANGET 0002 P F*OPN 008D

RANPUT 0003 P F$IOS 008E PUSH 0004 P F$CLS 008F PULL 0005 P FtMDl 0090 DEBUG 0000 C DOECNV 0091 RESET 0001 c DOENEU 0092 SHIFT 0002 c DOESET 0093 SSQMIN 0003 c TPNI1 0094 MAXREC 0002 c RIFOF 0095 IREC 0003 c ALOG 0096 JOB 0006 p DLOG 0097 J0B6 0007 p FIMD4 0099 J0B27 0008 p F$V41 009A MODE 0009 p FIX1T 009B IOPT OOOA p A OOOB p •ALA 0000

09/16/80 BLOCKNAMES

DATA 0066 LUN 0004 DEBUG 0004

oooi: c 0002!C 0003!C 0004! 0005!C 0006IC 0007!C 0008!C 00095C 0010! ooii:c 0012! 00131c 0014!C 0015:C 0016!C 0017! 0018! 0019! 0020! 0021! 0022! 0023!C 0024! 0025!

SUBROUTINE DQESET

THIS ROUTINE INITIALIZES THE COGGIN SEARCH SPACE SSSSSSSS3SS3SSSSSS3

5027:c 0028! 0029!C 0030!C

LOGICAL 02RICH>C0GGINrCHR0M0>DEBUG»RESETrSHIFTrSSQMIN

INTEGER TTYiDISK

INPUT IS FROH LABELED COHHON /SYSTEM/ OUTPUT IS TO LABELED COMMON /SEARCH/

COMMON /LUN / TTY«BISK>MAXREC»IREC COMMON /BURN / 02RICH.COGGIN.CHROMO COMMON /DEBUG / DEBUGrRESETiSHIFTrSSQHIN COMMON /SYSTEM/ Q<4)»U(2)»X<6>»Y(12)rS<4)»P»T COMMON /SEARCH/ QDATA(4).UDATA(2).XBATA(6)»YDATAC12>»

SDATA(4>rPDATA>TDATA

DOUBLE PRECISION QDATA>HDATA>XDATAiYDATAiSDATArPDATAiTDATAi QrUfXrYfSfPiT

DATA 1/0/

INITIALIZE ALL VARIABLES FROM DATA

146

0031!C 0032! 0033! 0034J10 0035SC 0036: 0037: 0038:c 003?: 0040: 0041:20 0042SC 0043: 0044S 0045130 0046:c 0047! 0048*. 0049:60 0050:c oosi: 0052:c 0053:c 0054:c 0055: 0056:c 0057! 0058 :c 0059:c 0060: »ERROR COUNT: OOOOj PSECT SIZE: 0125>

DO 10 1=1 »4 QDATA(I)=Q(I> CONTINUE

WDATA(1)=U(1) UDATA(2)=U<2>

DO 20 1=1(6 XDATA(I)=XCI) CONTINUE

DO 30 1=1 »4 SDATA(I)=S(I) CONTINUE

DO 60 1=1R12 YDATA(I)=Y(I) CONTINUE

TDATA=T

START COGGIN SEARCH

IF(.NOT.RESET) CALL DOECOG

RETURN

END

LABELS VARIABLES ARRAYS

>10 001C 02RICH 0000 C a 0000 c >20 0039 COGGIN 0001 C U 0010 C >30 004E CHROHO 0002 C X 0018 C >60 0063 DEBUG 0000 C Y 0030 C

RESET 0001 C S 0060 C SHIFT 0002 C QDATA 0000 C SSQMIN 0003 C UDATA 0010 C TTY 0000 C XDATA 0018 c DISK 0001 c YDATA 0030 c HAXREC 0002 c SDATA 0060 c IREC 0003 c P 0070 c T 0074 c PDATA 0070 c TDATA 0074 c I 0000 p •AIA 0009 *AIB OOOA

DSECT SIZE: OOII; REV. PROCEDURES

F«HD4 0074 DOECOG 007B F»RET 007C

5 09/16/80 BLOCKNAHES

LUN 0004 BURN 0003 DEBUG 0004 SYSTEM 0078 SEARCH 0078

OOOliC 0002!C= 0003:C 0004: 0005!C ooo6:c ooo7:c 0008 :c ooo9:c==> ooio:c oon: 0012: ooi3:c 0014! oois'.c 0016: 0017! 0018:c 0019:

SUBROUTINE DOESTK(IOPT)

THIS ROUTINE STORES/RETRIEVES LABELED CONHON DATA TO/FROH THE DISK DURING TASK SWAPPING.

SS8SSS85SA9BSB3SSSSBSSSSS3SSBS:S:S338&33SSSSSBS8SSA33

INTEGER RDATA(102)RDISK.TTY INTEGER BUFFER<1)RPULLIPUSHINULL(3)

LOGICAL 02RICH>C0GGINICHR0H0»DEBUG>RESETRSHIFTRSSQMIN

REAL CNANE(2)RGNAME<4> REAL XNAHE<6) R YNAHE (12). SNANE<4) >PNAHE (4)

DOUBLE PRECISION SR.AIRSR

147

0020 0021 0022 0023 C 0024 0025 C 0026 0027 0026 0029 0030 0031 0032 0033 0034 0035 0036 0037 0038 0039 0040 C 0041 0042 0043 0044 C 0045 0046 C 0047 0048 0049 C 0050 C 0051 C 0052 0053 0054 0055 20 0056 0057 0058 10 0059 0060 C 0061 C 0062 C 0063 0064 C 0065 0066 25 0067 C 0068 C 0069 C 0070 0071 0072 C 0073 0074 C 0075 C 0076 C 0077 0078 0079 0080 0081 0082 40 00B3 30 0084 0085 C 0086 0087

DOUBLE PRECISION Q>U>XrYrS>P>Tr QDATA.UDATA.XDATA.YDATA.SDATA.PDATArTDATA DOUBLE PRECISION LASTZ<22>»DELZ(22)

EQUIVALENCE <RDATA<3)»BUFFER<1))

COMMON /DATA / RDATA COMMON /INDEX / INDEXOO) COMMON /TEMPER/ TAXIS(24> COHMON /UEIGHT/ UEIGHTC30) COMMON /GAMMA / SR.AIRSR COMMON /VECTOR/ LASTZrDELZfNSERCH COMMON /LUN / TTY.DISK.MAXREC.IREC COMMON /DEBUG / DEBUGtRESET»SHIFTiSSQMIN COHHON /BURN / 02RICH.C0GGIN.CHR0M0 COMMON /NAHE / XNAHEiYNAMEiSNAMErPNAMEiCNAHEiGNAME COMMON /SYSTEM/ 0(4)»U<2)»X<6)rY(12)iS<4),P»T COMMON /SEARCH/ QDATA<4)fUDATA(2>»XDATA(6>»YDATA<12)i

SDATA(4)1PBATA1TDATA COMMON /MAXPIV/ UNITS(96)»NSIZE

DATA IOSPUT rI0SGET/Z109FiZ105F/ DATA PUSH»PULL/0f1/F I»JIM/3*0/ DATA NUORDS/O/, NRECRD/7/r NULL/1t 0 , 0 /

NUORDS=<RDATA<1)+l)/2

CALL F$OPN<DISK) IF(IOPT.EQ.PULL) GO TU 25

SAVE LABELED COHHON ON THE DISK

DO 10 I=liNRECRD DO 20 J=1rNUORDS

RDATA(J+2)-BUFFER(J+(I-1)*NUORDS) CONTINUE

RDATA(2)*MAXREC+I+3 CALL F$IOS(IOSPUT>RDATArDISK>M) CONTINUE

CALL FtCLS(DISK)

DISABLE "C WHILE SWAPPING TASKS

CALL UMNTR(TTY».FALSE.)

RETURN CONTINUE

ENABLE ~C AFTER THE JOB NUMBER IS IN THE DCB

CALL F$IOS(IOSPUT»NULL»TTY»M) CALL U$INTR(TTY».TRUE.>

CALL FIOPN(DISK)

RETRIEVE DATA FROM THE DISK-

DO 30 I=liNRECRD RDATA(2)=MAXREC+4+NRECRD-I CALL F*IOS(IOSGET>RDATArDISKrM) DO 40 Jsl»NUQRDS

BUFFER < J+(NRECRD-I)*NUORDS)=RDATA t J+2) CONTINUE

CONTINUE CALL FtCLS(DISK)

»ERROR COUNT! 1 LABELS

RETURN END

0000» PSECT SIZE: VARIABLES

0175* DSECT SIZE! 0012$ REV. S ARRAYS PROCEDURES

09/16/80 BLOCKNAHES

148

)25 005D IOPT 0009 RDATA 0000 c FtSBU 00A4 DATA 0066 )10 004E DISK 0001 C BUFFER 0002 c FSDOO 00A5 INDEX 001E )20 003A TTY 0000 C NULL 0002 p FIOPN 00A6 TEMPER 0030 >30 0099 PULL 0000 P CNAME 0034 c F$MD4 00A7 UEIGHT 003C >40 0092 PUSH 0001 P GNAME 0038 c F$MOO 00A8 GAMMA 0008

02RICH 0000 C XNAME 0000 c FtlOS 00A9 VECTOR 00B1 COGGIN 0001 C YNAME OOOC c FtCLS OOAA LUN 0004 CHROMO 0002 C SNAME 0024 c UtINTR OOAB DEBUG 0004 DEBUG 0000 C PNAME 002C c F$RET OOAD BURN 0003 RESET 0001 c 0 0000 c NAHE 0040 SHIFT 0002 c U 0010 c SYSTEM 0078 5SQHIN 0003 c X 0018 c SEARCH 0078 SR 0000 c Y 0030 c HAXPIV OOCl AIRSR 0004 c S 0060 c

OOCl

P 0070 c QDATA 0000 c T 0074 c UDATA 0010 c PDATA 0070 c XDATA 0018 c TDATA 0074 c YDATA 0030 c N5ERCH OOBO c SDATA 0060 c MAXREC 0002 c LASTZ 0000 c IREC 0003 c DELZ 0058 c NSIZE OOCO c INDEX 0000 c IOSPUT 0005 p TAXIS 0000 c IOSGET 0006 p UEIGHT 0000 c I 0007 p UNITS 0000 c J 0008 p H 0009 p NUORDS OOOA p NRECRD OOOB p •A1A OOOA *AIB OOOB

oooi:c 0002:c 0003JC 0004.C 0005SC 0006!C 0007!C 0008JC ooo?:c ooio: ooii:c 0012: 0013!C 0014! 0015: 0016: 0017 5 OOlBiC 0019! oo2o:c 0021: 0022: 0023:0 0024: 0025: 0026:c 0027! 0028! 0029! 0030: 0031: 0032! 0033! 0034: 0035: 0036SC 0037:1 0038! 0039:

THIS SUBROUTINE IMPLEMENTS THE MODIFIED COGGIN ALGORITHM TO MINIMIZE INSTRUMENTATION ERROR ON THE D.O.E. COAL FURNACE.

SSSCSS3S=SS23==S==2SSSSS

SUBROUTINE DOECOG

IMPLICIT DOUBLE PRECISION <A-H»0-Z)

COMMON /VECTOR/ LASTZ,DELZ,NSERCH COMMON /LUN / TTY.DISKrHAXRECfIREC COMMON /BURN / 02RICH»COGGIN,CHROMO COMMON /DEBUG / DEBUG*RESET.SHIFTrSSQHIN

DOUBLE PRECISION LASTZ<22>,DELZ<22>,STPSIZ(23),F<4>,Z<4>

INTEGER I VIA IT C 2) INTEGER TTYfDISK

LOGICAL DEBUG,RESET,SHIFT,SSQMIN,DONE,FACTOR LOGICAL 02RICHtCOGGINrCHROMOrTRUErFALSE

DATA SSQMAX/1.0D10/, IUAIT/0.1/ DATA FACTOR/.FALSE./, DONE/.TRUE./ DATA TRUE,FALSE/.TRUE.,.FALSE./ DATA DENOM,TOLER?CONVRG/1.0D-10,1.0D-6,1.OD-5/, Z»F/8*0.0D0/ S5W ITER/O/ DATA ZEROrONE/O.ODO,1«0D0/ DATA CHECK/0.ODO/, STPSIZ/23*-O.01D0/ DATA I,J/0,0/ DATA STEP,BASE/2*0.ODO/

CONTINUE COGGIN=TRUE ITER=0

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0019! COHHON /SYSTEH/ QrU»X.YrS.POSITNfT oo2o: COHHON /MAXPIV/ A(6r6)>B(6)>Z(6)rNAX 0021! COHHON /BURN / 02RICH»COGGIN.CHROHO 0022! COHHON /DEBUG / DEBUGFRESET.SHIFT*SSQMIN 0023SC 0024! DOUBLE PRECISION 0(4)»U(2>»X(6>»Y<12)»S(4)»PDSITN 0025! DOUBLE PRECISION ZNEU<6)>OLD(6)fTESTf TOLER 0026! DOUBLE PRECISION ZEROiSRrAIRSR 0027SC 0028*. DOUBLE PRECISION A»B»Z 0029:c 0030! DATA T0LER.ZER0/1.0D-7.0.0D0/ 0031! DATA ITER>11TEST> ZNEU(1)>0LD(1)/2*0r3*0.ODO/ 0032!C 0033! HAX*4 0034! IF(COGGIN) MAX=6 0035! IF(.NOT.CHROMO.AND.COGGIN) HAX=5 0036! IF(.NOT.SHIFT.AND.COGGIN) HAX=5 0037! IF(COGGIN.AND.RESET) MAX=5 0038! ITER=0 0039!C 00401C GET INITIAL GUESSES 0041: c 0042! ZNEU(1)=Q(4) 0043! ZNEHC2)=Y(11) 0044! ZNEU < 3)=U(2) 0045! IF(02RICH) 0046! + ZNEU(3)=U(1) 0047! ZNEU(4)=Y<8) 0048! ZNEU(5)=Y(2)

88lo!c ZNEU(6)=Y(10)

0051110 CONTINUE 0052iC 0053SC 0054 iC

CALCULATE FUNCTION VECTOR FOR THIS ITERATION

0055! CALL DOEFVC 0056!C 0057!C SET UP JAC0B1AN MATRIX 0058!C 0059! CALL DOEJAC 0060SC 0061;c SOLVE FOR ITERATION STEP VECTOR 0062!C 0063! CALL DOEPIV 0064!C 0065!C UPDATE INDEPENDENT VARIABLES 0066!C 0067! DO 20 I=1»HAX 0068! OLD(I)=ZNEU(I) 0069! ZNEU(I)=Z(I)+OLD(I) 0070!20 CONTINUE 0071!C 0072! Q(4)=ZNEU(1) 0073! Y(11)=ZNEU(2) 0074! IF(.NOT.02RICH) 0075! U(2)=ZNEU(3) 0076! IF(02RICH) 0077! + U<1)=ZNEU(3) 0078! Y(8)=ZNEU(4) 0079! Y(2)=ZNEU(5) 0080! Y(10)=ZNEU(6) 0081SC 0082! ITER=ITER+1 0083! IF(ITER.GT.25) RETURN 0084!C 0085!C TEST FOR CONVERGENCE 0086:c 0087! DO 30 I=1FHAX 0088! TEST=DABS((OLD(I)-ZNEU(I))/ZNEU(I)) 0089! IF(TEST.GT.TOLER) GO TO 10

1 5 3

0090S30 0091SC 0092SC 0093:c 0094SC 0095SC 0096S 0097! 00985 00995C oioo: OIOI:

CONTINUE

CONVERGED

CALCULATE STOICIOMETRIC RATIO AND THEORETICAL AIR

SR=0.21*(Q(l)tQ(2>+Q<3))/«<!>/ (X?l)/12+X(2)/4-X(3)/32+X(4)/32)

AIRSR=(Q(1)+Q(2)+Q(3))/SR/0.1705

RETURN END

1 >ERROR COUNT: 0000r PSECT SIZE! 0369f DSECT SIZE: 0028> REV


)10 0097 02RICH 0000 c Q 0000 C FIMD4 01 ID >20 00B4 COGGIN 0001 c U 0010 c DOEFVC 012B )30 0104 CHROMO 0002 c X 0018 c DOEJAC 012C

DEBUG 0000 c Y 0030 c DOEPIV 012D RESET 0001 c S 0060 c F$RET 012E SHIFT 0002 c A 0000 c F$D40 0133 SSQMIN 0003 c B 0090 c FtM41 016D TTY 0000 c 7. 00A8 c F*U41 016F DISK 0001 c ZNEU 0000 p SR 0000 c OLD 0018 p AIRSR 0004 c MAXREC 0002 c IREC 0003 c POSITN 0070 c T 0074 c MAX OOCO c TEST 0030 p TOLER 0034 p ZERO 0038 p ITER 003C p I 003D p *AIA 0009 *AIB OOOA *AIC OOOB •ADA OOOC *ADB 0010 •ADC 0014 *ADD 0018

09/16/80 BLOCKNAMES

GAMMA 0008 LUN 0004 SYSTEM "0078 MAXPIV 00C1 BURN 0003 DEBUG 0004

OOOliC 0002!C=== 0003!C 0004: 0005SC 0006IC 0007JC 0008:c 0009:c ooio:c=== OOlltC 0012: 0013: 0014SC oois: ooi6: ooi7: ooi8:c 0019: 0020: 0021: 0022:C 0023: 0024! 0025:c 0026: 0027:

SUBROUTINE DOECNV

sssssssssssssa

THIS ROUTINE PULLS A GIVEN RECORD OFF THE DISK AND CONVERTS THE RAU DATA TO DATA WITH THE UNITS REQUIRED FOR THE MASS BALANCE.

DOUBLE PRECISION 0(4)>U(2)>X(6)iY(12)rS(4)rPOSITNrTO DOUBLE PRECISION DZERO.OHE.DTEMP

INTEGER REC0RD>DATE(3)>TIME(3)rRDATA<102) INTEGER KNAME(20)r NAME(20) INTEGER KDATA<102)iIC0MP(12)

REAL LFE(3)>PRESSR(3> tAXIS(8)

LOGICAL 02RICH>C0GGINrCHR0M0 LOGICAL DEBUGtRESETtSHIFTrSSQMIN

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0029! 0030:c 0031: 0032! 0033! 0034!

8§II?5 0037! 0038! 0039SC 0040SC 0041:c 0042! 0043! 0044S 0045!15 0046! 0047! 0048110 0049SC OOSOiC 0051!C 0052SC 0053!C 0054! 0055!C 0056!C 0057!C 0058! 0059! 0060!C 0061IC 0062SC 0063! 0064! 0065!C 0066SC 00671C 0068! 0069!C 0070!C 0071!C 0072! 0073!C 0074!C 0075!C 0076! 0077! 0078!C 0079!C 0080!C 0081! 0082SC 0083!C 0084!C 0085! 0086! 0087120 0088!C 0089! 0090! »ERROR COUNT! 1 LABELS

DATA R/1.987D0/

QSUM=CK1)+Q(2)+Q(3) SUh=Y«12> DO 5 1=1.10

SUM=SUH+Y(I) CONTINUE

FACT0R=(0NE-Y(11))/SUM*Q(4) IF<.NOT.COGGIN) GO TO 10 FACT0R»Q(4)

ENSURE THE SUM OF HOLE/HASS FRACTIONS IS ONE

Y(12)*0NE DO 15 1=1.11

YC12)=Y(12)-Y(I) CONTINUE

XU)=0NE-X(2>-X<3>-X(4>-X<5)-X<6> S(1)=0NE-S(2)-S(3)-S<4) CONTINUE

CALCULATE STANDARD FREE ENERGY

H2 + C02 = H20 + CO

G=86SO.DO-7.59DO*T

NITROGEN BALANCE FUNCTION

B(l)=S(3)tU(2)/14-X(5>*U<l)/14-1.58*QSUH B(1)=B(1)+FACT0R«(Y<4)+Y<5)+Y(9)+2*Y(12>)

HYDROGEN BALANCE FUNCTION

B(2)=S(2)*U(2)-U(1)*(X(2)+X(6)/9)+2*Y(11)|Q(4) B<2)=B<2>+FACTOR*<Y?5>+4*Y<6>+2*Y<7>+3*Y<9>+2*Y<10>>

CARBON BALANCE FUNCTION

B<3)=SU)*W<2>/12-X<1>*U<1)/12+FACT0R*( Y<1 W<2W<5W<6) >

SULFUR BALANCE FUNCTION

B<4)=S(4)*U(2)/32-X(4)*U(l)/32+FACT0R*(Y(7>+Y(8)>

OXYGEN BALANCE FUNCTION

B<5>=-0.42*GISUM-U<n*<X<3)/16+X<6>/18>+Q<4>*Y<ll> B(5>=B(5>+FACT0R*<2*Y<lW<2>+2*Y(3W(4>+2tY<8)>

UATER GAS SHIFT EQUILIBRIA

B(6)=Y(11)/Y(10)*Y(2)/Y(1)*Q(4)/FACTOR-DEXP(-G/R/T)

NEGATE FUNCTIONS

DO 20 1=1.MAX B(I)=-B(I) CONTINUE

RETURN END

0000. PSECT SIZE! VARIABLES

0506. DSECT SIZE! 0082$ REV. 5 ARRAYS PROCEDURES

)5 0040 L 0070 C Q 0000 C FIHD4 00D9 )10 0086 T 0074 C U 0010 C DEXP OIDD )15 0069 MAX OOCO c X 0018 C FSH41 OOFE )20 01CF 02RICH 0000 c Y 0030 C F*D40 0101

COGGIN 0001 c S 0060 C FIM40 0105 CHROHO 0002 c A 0000 C F*RET 01F9

09/16/80 BLOCKNAHES

SYSTEH 0078 MAXPIV OOCl BURN 0003

1 5 8

ZERO 0000 P ONE 0004 P G 0008 P R OOOC P QSUH 0010 P FACTOR 0014 P SUM 0018 P I 001C P •ADA 0009 *ADB OOOD •ADC 0011 • ADD 0015 *ADE 0019 •ADF 001D •ADG 0021 •ADH 0025 *ADI 0029 • ADJ 002D •ADK 0031 •ADL 0035 •ADH 0039 •ADN 003D •ADO 0041 •ADF' 0045 •ADQ 0049 • ADR 004D •AIA 0051

0090 00A8

OOOliC 0002!C==== 0003:c ooo4i 0005:c ooo6:c 00075C ooo8:c 0009:c OOlOiC oou:c 0012:c ooi3:c 0014 5 C==== ooi5:c 0016! ooi7:c ooi8: 0019! 0020! 0021:c 0022! 0023SC 0024! 0025! 0026!C 0027! 0028! 0029! 0030!C 0031: 0032: 0033: 0034:10 0035: 0036: 0037: 0038: 0039:c oo4o:c oo4i:c 0042: 0043:

SUBROUTINE DOEJAC

JACOBIAN-MATRIX SUBROUTINE FOR FURNACE

THIS SUBROUTNE CALCULATES THE JACOBIAN ELEHENTS FOR THE MASS BALANCE EQUATION SET.

INPUT IS FROM LABELED COMMON /SYSTEH/ OUTPUT IS TO LABELED COMMON /HAXPIV/

LOGICAL 02RICH.C0GGINFCHR0M0

COMMON /SYSTEM/ Q»U»XrY.S»L»T COMMON /MAXPIV/ A<6>6)>B(6)>Z(6)iHAX COMMON /BURN / 02RICH»C0GGIN»CHROMO

DOUBLE PRECISION Q<4).U<2),X<&><Y(12)»S<4>rLfT

DOUBLE PRECISION A»B»Z»ZEROfONE DOUBLE PRECISION YSUM.ATEMP.FACTR1.FACTR2

DATA ZERO/O.0D00/» ONE/1.ODOO/ DATA YSUMiFACTRl»FACTR2»ATEMP/4*O.ODO/ DATA 1/0/

YSUM=Y(12) DO 10 1=1 * 10

YSUM=YSUM+Y(I) CONTINUE

FACTR1=(QNE-Y(11))/YSUM FACTR2»-Q(4)/YSUM IF(COGGIN) FACTR1=0NE IF(COGGIN) FACTR2=ZER0

NITROGEN BALANCE JACOBIAN ELEMENTS

ATEMP=(Y(4)+Y(5)+Y(9)+2*Y(12)) A(lfl)=FACTRl*ATEMP

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0115! RETURN 0116: END »ERROR COUNT! OOOOF PSECT

LABELS VARIABLES SIZE! 0689, DSECT SIZE! 0033! REV. S

ARRAYS

>10 0034 02RICH COGGIN CHROMO L T MAX ZERO ONE YSUM ATEMP FACTR1 FACTR2 I •ADA #ADB • ADC • ADD •AHE *ADF

0000 0001 0002 0070 0074 OOCO 0000 0004 0008 OOOC 0010 0014 0018 0009 OOOD 0011 0015 0019 001D

c Q 0000 C F$MD4 c U 0010 C FIM40 c X 0018 C FID40 c Y 0030 C F*RET c S 0060 c c A 0000 c p B 0090 c p Z 00A8 c

PROCEDURES

00E3 OOEF 00F7 02B0

09/16/80 BLOCKNAHES

SYSTEM 0078 MAXPIV 00C1 BURN 0003

oooi:c ooo2:c= ooo3:c 0004! 0005!C

IE 0008SC 0009!C ooio:c OOlliC 0012!C ooi3:c 0014SC==== oois:c ooi6: 0017! ooi8:c ooi9: 0020:c 0021! 0022!C 0023: 0024!C 0025: 0026:c 0027JC 0028:c 0029! 0030: 0031! 0032: 0033! 0034: 0035: 0036: 0037: 0038: 0039: 0040: 0041:30 0042:20 0043SC 0044SC 0045:c 0046IC

SUBROUTINE DOEPIV

GAUSS - riffiUDHRraSTz8VRlifiBvTHE

A = COEFFICIENT MATRIX B = CONSTANTS VECTOR X = SOLUTION VECTOR MAX = NUMBER OF EQUATIONS

SS3Sa8SSSSS8SSSSS3SSS8SSS3S6BSSSS8SB8SSSS3SS8388SSSSSSS8BSSa85SSa

IMPLICIT DOUBLE PRECISION (A-H) IMPLICIT DOUBLE PRECISION (0-Z)

COMMON /MAXPIV/ A(6r6)rB(6>tX(6)>HAX

INTEGER C(6)>R(6)

DATA C(1)rR(1)/Or0/> K.I.JtM0DE/4*0/i TEMP.AMAX/2*O.ODOO/

DO 10 K=1»MAX

CHOOSE THE PIVOT

AMAX=0.0D+00 DO 20 1=1fMAX

CALL DOEMAT(I»K.R»MODE> IF(MODE.EQ.O) GO TO 20 DO 30 J=1iMAX

CALL DOEMAT(J»K»C»MODE) IF<M0DE<EQ<0) GO TO 30 TEMP=DABS(A(I»J>) IF(TEMP.LT.AMAX) GO TO 30 AMAX=TEMP R(K)=I C(K)=J CONTINUE

CONTINUE

K-TH PIVOT = A(R(K>iC(K)>

NORHALIZE THE PIVOT'S ROU

161

0047SC 0048:

550 i 0051140 0052: 0053IC 0054:c 0055!C 0056: 0057: 0058! 0059J 0060*. 0061! 0062:60 0063: 0064 *.50 0065:10 0066:c 0067:c 0068:c 0069! 0070: . 0071! 0072: 0073!80 0074!70 0075: 0076! »ERR0R

TEMP=A(R(K)rC<K)> DO 40 J=1»HAX

A(R(K)»J>=A(R(K)»J)/TEMP CONTINUE

B(R<K))=B(R(K))/TEMP

REDUCTION OF THE MATRIX

DO 50 I=1»HAX IF(I.EQ.R(K)) GO TO 50 B<I)=B(I)-B(R(K))*A(IfC(K)) DO 60 J=1»HAX

IF(J.EQ.C(K)) GO TO 60 A(IiJ>=A<I»J)-A<R<K)»J)*A(I»C<K>) CONTINUE

A(I>C(K))=0>OD+00 CONTINUE

CONTINUE

UNSCRAMBLE THE SOLUTION VECTOR

DO 70 DO

1

K=1rMAX 80 I=liHAX

IF(A(IIK).EQ.O.00+00) GO TO 80 X(K)=B(I) CONTINUE

CONTINUE RETURN

END COUNT! OOOOr PSECT SIZE: 0396. DSECT SIZE! 0014. REV. 5


)10 014F HAX OOCO C A 0000 C F«HD4 OOFC ) 20 0070 K OOOC P B 0090 C DOEMAT OOFF >30 0069 I OOOD P X 00A8 C F*MOO 0100 >40 00A3 J OOOE P C 0000 P F*RET 018B ) 50 0148 MODE OOOF P R 0006 P

012D TEMP 0010 P >70 0182 AMAX 0014 P >80 0178 *A1A 0009

•AIB OOOA •AIC OOOB •AID OOOC *AIE OOOD

09/16/80 BLOCKNAHES

MAXPIV 00C1

0001:c 0002!C===== 888888888888888888888888888881 ooo3:c 0004: SUBROUTINE DOEMAT (JiKtLrH) ooossc ooo6:c SUPPORT ROUTINE FOR GAUSS - , 0007:c ooo8:c THIS ROUTINE UNSCRAMBLES THE 0009SC ooio:c===== 8S8S8SSSSS888SSS88SS88S8888SS! oon :c 0012: DIMENSION L(6) 0013! DATA MAXII/OIO/ ooi4:c 0015! IF(K.NE.l) GO TO 10 0016! H=1 0017: RETURN 0018:10 CONTINUE 0019! H=1 0020! MAX=K-1

»: DO 20 1=1>MAX »: IF(L(I>.EQ.J> M=0 0025120 CONTINUE 0024: RETURN 0025! END

3SSSasSS3SS8BS36888l

SSSS8.»S8S8aS8SS888883S88S

162

»ERROR COUNT! 0000» PSECT SIZE: 0048r DSECT SIZE? 0014? REV. 5 1 LABELS VARIABLES ARRAYS PROCEDURES

09/16/80 BLOCKNAMES

>10 >20

0014 0026

oooi:c ooo2:c== 0003 :c 0004! ooos:c 00065C ooo7:c ooo8:c ooo9:c ooio:c OOll.'C 00125C 0013JC 0014 S C ooi5:c== 0016!C 0017! 0018IC 0019! 0020! 0021! 0022:C 0023: 0024:c 0025: 0026:C 0027! 0028! 0029! 0030: 003UC 0032: 0033:c 0034:c 0035:c 0036!C 0037: 0038:c 0039JC oo4o:c 0041:c 0042!C 0043! 0044:c 0045! 0046! 0047:c 0048: 0049! 0050:c 0051! 0052! 0053: 0054:c 0055:10 0056:c 0057JC 0058!C 0059:c 0060:c 0061:

J K H MAX I •AIA

0009 OOOA OOOC 0000 P 0001 P OOOD

OOOB FtSBT 002D F*MD1 002E F*RET 002F

Esas&s8«ssss=sssssssss:assc8accssss3«sss3ass»sssss=3&sssssi

DOUBLE PRECISION FUNCTION DOESSQ(NULL)

THIS ROUTINE CALCULATES THE SUM OF SQUARES FUNCTIONAL FOR THE FURNACE. THE FUNCTIONAL INCLUDES CALCULATED VARIABLE CONTRIBUTIONS AND SEARCH VARIABLE CONTRIBUTIONS

INPUT IS VIA COMMON /SEARCH/ INPUT IS VIA COMMON /SYSTEM/

FOR DATA FOR CALCULATED VARIABLES AND SEARCH VARIABLES.

IMPLICIT DOUBLE PRECISION (A-HiO-Z)

DOUBLE PRECISION Oi4> t W (2>.X(6)»Y<12)»S(4)»P»T DOUBLE PRECISION QDATA(4)>UDATA(2)rXDATA(6> rYDATAC12) DOUBLE PRECISION SDATA<4)rPDATA.TDATA

LOGICAL 02RICH>COGGIN>CHROHO

REAL UEIGHT(30>

COMMON /HEIGHT/ HEIGHT COMHON /BURN / 02RICH.C0GGIN.CHR0H0 COMMON /SYSTEM/ Q.U>X»YrSrPrT COMHON /SEARCH/ QDATAiUDATArXDATArYDATAtSDATArPDATA1TDATA

DATA ZERO/O.ODO/

COMPUTE HASS BALANCE

CALL DOENEU

COMPUTE CALCULATED VARIABLES CONTRIBUTION

DOESSQ=ZERO

DOESSO=DOESSO+DOESQR(XDATA(1> rX(l)> + +D0ESQR(YDATA(2>fY(2)>

IF(.NOT.02RICH) + DOESSQ=DOESSQ+DOESQR(SDATA(1), S(1) >

IF(.NOT.CHROMO) GO TO 10 DOESSQ=DOESSQ+DOESQR(YDATAt10)»Y<10)>

+ +DOESQR(YDATA(12)tY(12))

CONTINUE IF(COGGIN) RETURN

INCLUDE SEARCH VARIABLES CONTRIBUTION

DOESSQsDOESSQ+DOESQR(XDATA(2) >X<2))

163

0062: 0063! 0064: 0065: 0066! 0067: 0068! 0069: oo7o: 0071! 0072:c 0073S 0074S 0075: 0076: 0077! 0078! 0079SC 0080: 0081! 0082! 0083! 0084! 0085!C 0086! 0087:C 0088! END >>ERR0R COUNT! 0000r 1 LABELS

+D0ESQR<XDATA<3)»X<3>> . +D0ES0R(XDATA(4)iX(4)) +DOESQR XDATAC5)»X<5>) +D0ESQR(XDATA(6)tX(6J) +D0ESQR(YDATA(1)»Y(1)) +D0ESQR(YDATA(3)»Y(3)) +D0ES0R(YDATA(4)fY(4)) +D0ESQR(QDATA(1).Q(1)) +D0ESQR(QDATA<2)>0(2)> +D0ESQR(QDATA(3)>Q(3))

IF(02RICH> RETURN DOESSQoDOESSQ+DOESQR(SDATA(2 > > S (2 > >

+D0ESQR(SDATA(3)>S(3)) +D0ES0R(SDATA(4)>S(4)) +DOESQR(UDATA<1)iU(1)) +D0ESQR(TDATA>T)*UEIGHT<30)

IF(.NOT.CHROMO) RETURN D0ESSQ=D0ESSQ+D0ESQR(YDATA(7) rY(7))

+D0ESQR<YDATA(5)>Y(5)) +D0ESQR(YDATA<6)>Y(6)> +D0ESQR(YDATA<9)>Y(9))

RETURN

PSECT SIZE: 0261i DSECT SIZE! 0054> REV. 5 09/16/80

)10 0044

VARIABLES ARRAYS PROCEDURES BLOCKNAKES DOESSQ OOOA Q 0000 C FtSBU 00B7 UEIGHT 003C NULL 0009 U 0010 C DOENEU 00B8 BURN 0003 P 0070 C X 0018 c DOESQR 00B9 SYSTEM 0078 T 0074 C Y 0030 c FIMD4 OOBA SEARCH 0078 PDATA 0070 C S 0060 c FtRER 00C7 TDATA 0074 C QDATA 0000 c F««41 OOC8 02RICH 0000 C UDATA 0010 c COGGIN 0001 C XDATA 0018 c CHROMO 0002 C YDATA 0030 c ZERO 0000 P SDAT A 0060 c *ADA OOOE UEIGHT 0000 c *ADB 0012 •ADC 0016 • ADD 001A *ADE 001E •ADF 0022 •ADG 0026 *ADH 002A •ADI 002E *ADJ 0032

oooi:c 0002JC 0003 :c 0004! 0005 :c 0006:c ooo7:c ooo8:c ooo9:c ooio :c oon: 0012! 0013JC ooi4: 0015*. ooi6: ooi7:c ooi8: ooi9: 0020:

sssssssassssssssasssssaB

DOUBLE PRECISION FUNCTION DOEZVL(IrZSTEPrZl)

COGGIN SUPPORT ROUTINE TO ALLOU INDIRECT-INDEXED ADDRESSING OF THE SEARCH VARIABLES.

SS8SSC:SBSS2SSS398rnSSSaSdS3B8aa3SSSaSBESZ8SSS

IMPLICIT DOUBLE PRECISION (A-H>0-Z) COMMON /VECTOR/ 0LDZC22)»DELZ<22>fNSERCH

DATA J/0/ DATA ZTEHPiSCALAR/0.ODO.1.000/ DATA ONE>ZERO/1.ODO>0.0D0/

J=NSERCH+1 IF(I.EQ.J) GO TO 10 DOEZVL=DQEFVL(IiZSTEPtZl)

:SSS88aSSSSSSSSSBSSS88S

1 6 4

0021! 0022:C 0023110 0024IC 0025:c 0026!C 0027: 0028: 0029: 0030: 0031*. 0032:20 0033! 0034: »ERR0R COUNT: 1 LABELS

RETURN

CONTINUE

SEARCH ALONG HYPERVECTOR

SCALAR=Z1+SCALAR*ZSTEP DOEZVL=SCALAR DO 20 J=1rNSERCH

ZTEMP=OLDZ(J)-DELZ(J)+SCALAR*DELZ(J) ZTEHP=DOEFVLt J.ZERO > ZTEHP > CONTINUE

RETURN END

0000 r PSECT SIZE! 0097» DSECT SIZE: 0019S REV. 5

>10 ) 20

002A 0052

VARIABLES

DOEZVL OOOC I 0009 ZSTEP OOOA Zl OOOB NSERCH OOBO C J 0000 P ZTEMP 0001 P SCALAR 0005 P ONE 0009 P ZERO OOOD P *AIA 0010 •AIB 0011 #AIC 0012

ARRAYS

OLDZ DELZ

0000 0058

PROCEDURES

F$SBT 005B DOEFVL 005C F$RER 005D

09/16/80 BLOCKNAMES

VECTOR 00B1

oooi: c 0002!C= 0003JC

>:c 0006SC ooo7:c 0008IC ooo?:c ooio:c ooii :c '0012!C 0013:c 0014! 0015IC 0016: 0017! 0018!C 0019! oo2o:c 0021! 0022SC 0023: 0024:c 0025! 00265C 00275C 00282C 0029SC 0030iC 0031 :c 0032:c 0033 :c 0034JC 0035 :c 003&:c 0037SC 0038!C 0039:c 0040:

:B68SSS::sa88S&S8aSZS583S8SSSSSSSSSSSS38BSS&S3S18l8IS3SSSS3BB8a88S8

DOUBLE PRECISION FUNCTION DOEFVLd iZSTEP>Zl)

THIS FUNCTION INCREMENTS A SPECIFIED SEARCH VARIABLE BY THE GIVEN FRACTION 'ZSTEP' FROM THE BASE POINT Zl.

INPUT IS FROM THE PARAMETER LISTt OUTPUT IS VIA COMMON.

IMPLICIT DOUBLE PRECISION (A-HrO-Z)

COMMON /SYSTEM/ 0(4)»U(2)»X(6>»Y(12)»S<4)»P»T COMMON /INDEX/ INDEX

EQUIVALENCE <Z(1)»Q(1>)

INTEGER INDEX(30)

DOUBLE PRECISION Z(30)

DATA J/0/

0(1-4) = Z(l-4) W<1-2) = Z<5-6> X(1—6) = Z < 7—12) Y(1-12)= Z(13-24) S<l-4) = Z(25-28) P « Z<29) T = ZOO)

INDEX/1.2.3,8i9»10»11.12.13.15»16»5»26.27»28r30rl7,18.19r21/

UPDATE THE SPECIFIED SEARCH VARIABLE

Z(INDEX(I))=Z1+Z(INDEX(I))*ZSTEP

1 6 5

0041! 0042! 0043iC 0044! »ERR0R COUNT! 0000 1 LABELS

DOEFVL=Z(INDEX(I)) RETURN

END PSECT SIZES 0033» DSECT SIZE! 0018! REV. 5

PROCEDURES VARIABLES ARRAYS

DOEFVL OOOC 0 0000 C I 0009 U 0010 C ZSTEP OOOA X 0018 C 21 OOOB Y 0030 C P 0070 C S 0060 C T 0074 C INDEX 0000 C J 0000 P Z 0000 C tAIA 0010 *AIB 0011

FtSBT FiRER

001F 0020

09/16/80 BLOCKNAMES

SYSTEM 0078 INDEX 001E

0001 *.C 0002:c== 0003IC 0004! 0005:c 0006 :c 0007!C 0008!C== ooo?:c 0010! 0011 s 00125C 0013! 0014! 0015JC 0016! 0017! 0018! 0019! 0020!C oo2i:c 0022:c 0023! 0024! 0025! 0026: 0027: 0028: 0029120 0030:io 0031: 0032!

SUBROUTINE DOESRTtF.Z)

BUBBLE SORT ROUTINE FOR THE COGGIN ALGORITM

IMPLICIT DOUBLE PRECISION (A-HfO-Z) DIMENSION F(4)>Z<4)

DATA FTEHPfZTEMP/2*O.ODO/ DATA IiJ»K/3*0/

DO 10 J=lf3 K=4-J DO 20 1 = 1 fK

IF(F(I).LE.F(I+1)) GO TO 20

VECTORS F AND Z ARE ORDERED PAIRS

FTEMP=F(I> ZTEMP=Z(I) F<I)=F(1+1) Z(I)=Z(I+1) F(I4" X+l)®FTEMP Z<1+1)=ZTEHP CONTINUE

CONTINUE RETURN END

»ERROR COUNT! OOOOr PSECT SIZE! 1 LABELS

) 10 ) 20

0069 0062

VARIABLES

FTEMP 0000 P ZTENP 0004 P I J K *AIA •FTIB *AIC •A I [i *AIE *AIF

0008 P 0009 P OOOA P OOOB OOOC OOOD OOOE OOOF 0010

0119» DSECT SIZE! 0017J REV. ARRAYS PROCEDURES

F 0009 FtSBT 0072 Z OOOA FSMD4 0073

F*RET 0076

09/16/80 BLOCKNAHES

0001!C 0002:c=

OOOSiC 0006'C 0007!C

BSS33SS3SSSSS83SSSSBSSSaSSSSSSS8=SS8BaaSBS3S3SSaSSSS8SSSSSS8SS3S

DOUBLE PRECISION FUNCTION DOESOR'(DtX)

THIS ROUTINE COHPUTES THE SQUARE OF THE RESIDUALS AND INCLUDES A PENALTY TERM IF THE PREDICTION

1 6 6

0008JC IS NEGATIVE. ooo?:c 0010! CSSSC£ = S = = - = S = = = S~==SS = = SSSSE=SSS = SSS»=3SSSSS8S3C3SSS333SSSEaSB3SSSE

ooii:c IMPLICIT DOUBLE PRECISION (A-H>0-Z) 0012!

0013IC 00141 oois:c ooi&: ooi7: 0018! 0019S 0020JC 0021IC 0022.C 0023: 0024: 0025! 0026:

DATA CONSTIZERO/IOOO.ODOFO.ODO/

DOESQR=ZERO IF(X.EQ.ZERO) RETURN IF(D.EQ.ZERO) RETURN D0ESQR=<CX-D)/D>**2

ADD PENALTY TERHS IF VALUE IS NEGATIVE

IF(X.GE.ZERO) RETURN DOESQR=DOESQR*DEXP<CONST*DABS((X-D)/D>> RETURN END

»ERROR COUNT: OOOOr PSECT SIZE! 0089. DSECT SIZE! 0019? REV. 5 1 LABELS VARIABLES ARRAYS PROCEDURES

09/16/80 BLOCKNAHES

DOESDR OOOB D 0009 X OOOA CONST 0000 P ZERO 0004 P •ADA OOOF

FSSBT 0052 F*RER 0055 DEXP 0057

00011 c 0002:c 0003SC 0004!C 0005JC 0006:c ooo7:c 0008SC 0009SC ooio:c 0011SC 0012 * C ooi3:c 0014SC ooi5:c 0016SC 0017IC 0018IC 0019! 0020:c 0021IC 0022! 0023: 0024SC 0025! 0026IC 0027JC 0028! 0029! 0030! 0031: 0032SC 0033SC 0034:C oo3s:c 0036:c 0037SC 0038:c 0039! 0040! 0041! 0042: 0043! 0044! 00455C 0046! 0047:C 0048! 0049! ooso: 0051: 0052!11 0053: 0054! 0055! 0056110 0057!C 0058IC 0059:c 0060! 0061! 0062! 0063! 0064:C 0065JC 0066:c 0067!C 0068IC 0069! 0070:

LINKING PROCESSOR FOR CROHEHCO

THIS PROGRAH LINKS CONTROL BASIC PROGRAHS WITH Z80 HACHINE LANGUAGE SUBROUTINES.

LUNSi

SI = USER BASIC FILE SO - US IS = DP LO = TY OM = TY U1 = 63 = UKZ80DIR)

IHPLICIT INTEGER (A-Z)

INTEGER SYHB0L<60>11> >ASCII(80)>SUBNAH(60i11) INTEGER Z80DIR<4>rNAHSAVUO)rLOADER(64>

LOGICAL FOUNDiNEUREC

DATA LOADSZ /64/i LOADER /64K1H0/ DATA SYHB0LC1>1)rASCII(1)iSUBNAH(1t1)rLOADER*1)/4*0/ DATA Z80DIR/'DS'»'Z8'»'00'»'IR'/ DATA I0SGET/Z205F/

PASS ONE

INITIALIZE SYHBOL TABLE

SI = 1 S0=2 L0=5 IS=6 0H=7 Ul=63

HAXREF=60

URITE(L0>501) DO 10 I=1»HAXREF

DO 11 J=l,8 SYHBOL(I>J)=1H CONTINUE

SYHBOL(Ir9)=0 SYMBOL!Ir10)=0 SYMBOL*It11)=0 CONTINUE

INITIALIZE COUNTERS

NCALL=0 NREC=0 NBYTES=X'2200' DIhSAV=0

GO TO TOP OF FILES

REUIND SI REWIND SO

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ACCOUNT FOR DIFFERENCE FOR SUBSTITUTIONS IN THE NUMBER OF BYTES

ISUM=0 DO 40 1=1rNCALL

£ON?INUEm+syhbol<i'11>-symbol<i'10>"5 IF(ISUM.GT.O) NBYTES=NBYTES+ISUM

COHPUTE PAGE FOR START OF SUBROUTINE

NBYTES=NBYTES+DIMSAV*2+X'80'

SUBROUTINE PAGE START

LOCBGN=NBYTES/X'100' L0CBGN=L0CBGN*X'100' LOCSUB=LOCBGN

GET NAME OF ALL SUBROUTINE ON FILE AND THEIR SIZE NSUB=0 CONTINUE READ(U1»500> (ASCII(I)* 1=1»BO> IF(ASCII(1).EQ•1H-) GO TO 56 NSUB=NSUB+1 SUBNAM(NSUBr9)=0 SUBNAHCNSUBt10>=0

PACK SUBNAH. LEFT JUSTIFY IT

K=0 DO 52 1=1>8

SUBNAH(NSUB>I)=1H IF(ASCII(I).EQ.1H ) GO TO 52 K=K+1 SUBNAM(NSUB f K)=ASCII(I) CONTINUE

GO TO 50

COUNT NUHBER OF BYTES IN EACH ASSEHBLED Z-80 SUBROUTINE

mm™ LINE=JHAX HO 300 I=1»NSUB

FIND SUBROUITNE

CONTINUE LINE=LINE+1

READ(U1>500> (ASCII(J)»J=1>9) IF(ASCII(7).EQ.1HE.AND.ASCII(8).EQ.1HN •AND•ASCII(9)lEQflHD) GO TO 60 IF(ASCII(1).EQ.1H ) GO TO 325

DO 311 11=1rNSUB ISUB=II DO 310 J=l»8

IF( ASCIK J) •NEiSUBNAHdl 1 J)) GO TO 311 CONTINUE

NATCH FOUND

GO TO 312 CONTINUE GO TO 300

028 41C 0285SC 0286!C 0287SC 0288S312 0289! 0290J315 02915 0292! 02935 0294! 0295! 0296! 0297! 02985 02995330 03005 0301!C 0302!C 0303:c 03041320 0305! 03061300 0307!C 03085C 0309!C 0310!C 0311:c 03125C 03135C 0314: C 03155C 03165C 03175C 03185C 0319560 03205 03215 0322!70 0323! 0324!C 0325! 0326! 0327574 0328! 0329!C 0330!C 0331!C 0332! 0333! 0334!C 0335!C 03365C 0337S76 033B5C 03395C 03405C 03415 0342! 0343! 0344!82 0345!C 0346!C 03475C 0348! 0349!C

8IS9iE 0352! 0353! 0354!C

MATCH FOUND. COUNT NUMBER OF BYTES UNTIL END OF DATA 'EOD' FOUND

SUBNAM(ISUBt11)-LINE NBYTES=0 CONTINUE READ(UlfSOO) (ASCII(J)>J=1r9) LINE=LINE+1 IF(ASCII(l).EQ.lHE.AND.ASCII(2).EQ.1H0 •AND.ASCII(3).EQ.1HD) GO TO 320 IF(ASCII<1).EQ.1H ) GO TO 315 DO 330 J=l»8

IF( ASCIK J) .EQ. 1H ) GO TO 315 NBYTES=NBYTES+1 CONTINUE

GO TO 315

'EOD' FOUND* SAVE NUMBER OF BYTES OF SUB

CONTINUE SUBNAM(ISUB»9)=(NBYTES+1)/2 CONTINUE

NSUB=NUMBER OF SUBROUTINES IN LIBRARY

SUBNAM(SUBrl)

1<I<8 1=9 1=10

SUBROUTINE NAME SUBROUTINE SIZE ABSOLUTE LOADING ADDRESS

READ BASIC FILE NREC TIMESi REPLACE CALL SUBNAH WITH CALL ZHHLL

CONTINUE K=1 REC=0 CONTINUE READ (SO 1500) (ASCIK I) • 1 = 1 >80) URITE(L0>500) (ASCIK I)»1 = 1 »80) REC~REC+1 J GUIQ'NREC) G0 T0 72 IF(SYMBOL(Ki9).EQ.REC) GO TO 76

NO CALL IN THIS RECORD

URITE(ISf500> (ASCIKI)11 = 1 >80) GO TO 70

CALL IN THIS STATEMENT RECORD

CONTINUE

FIND SUBROUTINE IN LIBRARY DIRECTORY

DO 80 I=1>NSUB DO 82 J=li8

IF(SYMBOL(KfJ).NE.SUBNAM(IiJ)) GO TO 80 CONTINUE

HATCH FOUND* CHECK IF PREVIOUSLY REF'D

IF(SUBNAM(I>10).GT.O) GO TO 84

FIRST REFERENCE FOR SUBNAM

SUBNAH(I>10)=L0CSUB LOCSUB=LOCSUB+SUBNAM(If9)

172

0355:c 0356JC 0357: 0358:80 0359SC 0360SC 03615C 0362: 0363! 0364: 0365:c 0366:c 0367:c 0368!C 0369SC 0370:84 03715 0372: 0373: 0374! 03755 C 0376: 0377! 0378! 0379! 0380iC 03815C 03825C 0383! 0384! 0385:C 0386:C 0387:C 0388: 0389: 03905 0391! 03925 0393:92 03945 0395JC 0396SC 03975C 0398: 0399! 04005 04015 04025 0403594 0404590 04055C 04065C 04075C 0408! 0409! 0410: 04ii: 0412: 0413! 0414! 0415IC 04165C 04175C 04185 04195 04205 0421598 0422596 0423 5 C 04245C 04255C

REPLACE CALL SUBNAH UITH CALL ZHHLL

GO TO 84 CONTINUE

UNSATISFIED REFERENCE

URITE<0H>506) <SYMBOL(K>I)r1=1F9) K=K+1 GO TO 74

REPLACE CALL SUBNAH UITH CALL ZHHLL

CHANGE HEX ADDRESS TO ASCII ADDRESS

CONTINUE 1HEX1=SUBNAH(I»10)/X'1000' IHEX2=(SUBNAM(I»10>-<IHEX1*X'1000'))/X'100' IHEX3=(SUBNAN(I»10)-(IHEX1*X'1000')-(IHEX2*X'100'))/X'10' IHEX4=SUBNAM(I»10)-(IHEX1*X'1000')-(IHEX2*X'100')-(IHEX3*X'10')

CALL HTOC(IHEXl) CALL HTOC(IHEX2) CALL HT0CUHEX3) CALL HT0CCIHEX4)

CHECK FOR SHIFT RIGHT

ISIZE=SYMBOL(Ki11)-SYMBOL(K»10) IF(ISIZE.GE.5) GO TO 90

SHIFT RIGHT

ISHIFT=80-5+ISIZE

J=80+SYMB0L(K>11)-I ASCII(J)=ASCII(J-l) CONTINUE

SYMBOL(KF11)=SYMBOL(K»10>+5

UPDATE OTHER REFERENCES ON THIS RECORD

ISTRT=K+1 DO 94 I=ISTRTrNCALL

IF(SYMBOL!I»9).NE.REC) GO TO 90 SYHBOL(I»10)=SYMB0L(I»10)+5-ISIZE SYMBOL(III1)=SYMB0L(IF11)+5-ISIZE CONTINUE

CONTINUE

URITE ASCII ADDRESS INTO RECORD

I=SYHBOL(Ki10) ASCII(I)=1H% ASCII(I+1)*IHEX1 ASCII(1+2)=IHEX2 ASCII(I+3)=IHEX3 ASCII(I+4)=IHEX4 IF(ISIZE.LE.5) GO TO 96

SET REMAINDER OF SIZE TO BLANKS

ISIZE=SYMBOL(K>11)-SYMBOL(K»10)-5 DO 98 J-liISIZE

ASCII(I+4+J)=lH CONTINUE

CONTINUE

READY FOR NEXT REFERENCE

173

0426! 0427! 042B!72 0429!C 0430!C 0431: c 0432!C 0433!C 0434!C 0435!C 0436!C 0437! 0438! 0439! 0440! 0441! 0442! 0443! 0444!73 0445!C 04461C 04471C 0448! 0449! 04501100 0451!C 0452!C 0453!C 0454 !C 04555 0456! 0457! 0458! 0459S62 0460! 0461! 0462!64 0463! 04641C 0465IC 0466 !C 0467! 110 0468! 0469! 0470SC 0471iC 0472! 0473! 0474! 0475!C 0476!C 0477!C 0478!120 0479! 0480! 0481! 0482! 0483! 04841121 0485! 0486! 0487! 0488!122 0489!C 0490!C 0491!C 0492! 0493!C 0494!C 0495!C 0496!C

K=K+1 GO TO 74 CONTINUE

ALL SUBSTITUTIONS HADE

ATTACH SUBROUTINES TO LOADER FILE

LOAD=LOCBGN NEED«LOADSZ URITE(ISi508) LOCBGN URITE(L0i520) DIHSAV URITE(L0>514) LOCBGN NREAD=0 REUIND U1 CONTINUE

LOOK FOR A LOADING ADDRESS MATCH

DO 100 1=1»NSUB IF(SUBNAMCIflO).EQ.LOAD) GO TO 110 CONTINUE

NO MATCH FOUNDf ALL REFERENCES SATISFIED fclRITE LAST RECORD

CALL OUTPUT(LOADERfISfLOADSZ) WRITE(ISr502) WRITE(L0r510) DO 62 1=1fNSUB URITE(L0>511) CSUBNAM(I.J)»J=1.10) URITE(L0r512) DO 64 1=1iNCALL URITE(LOf511) (SYMBOL(I»J)jJ=119) STOP

MATCH FOUNDfPICK UP REFERENCE

CONTINUE SUB=I L0AD=L0AD+SUBNAH<SUBf9>

SKIP PAST DIRECTORY ASCII(1)=80 ASCII(2)=SUBNAH(SUBf11>-2 CALL FilOSCIOSGETrASCII>UlrI>

FIND MACHINE LANGUAGE SUBROUTINE

CONTINUE READ(UliSOO) (ASCII(I)rl=lr80) IF(ASCII(7)»NE>1HE•OR•ASCII(8)«NE»1HN .OK.ASCII(V).NE.1HD) GO TO 121 URITECOMi522) (SUBNAM(SUBrI)r1=1>8) GO TO 73 CONTINUE DO 122 1=1i80

J=81-I IF(ASCII(J).NE.1H ) GO TO 124 CONTINUE

BLANK RECORD FOUNDf SKIP IT

GO TO 120

NON-BLANK RECORD FOUND SEARCH FOR SUBNAM MATCH

1 7 4

04971124 0498! 0499SC 0500:c 0501!C 0502! 0503! 0504! 0505! 0506! 05075126 0508! 05095 0510'. 05111127 0512: C 0513IC 0514:C 0515: 0516! 0517:128 0518:c 0519SC 0520!C 0521! 0522! 0523: 0524! 0525! 0526! 0527: 0528:130 0529! 0530! 0531*. 0532'. 0533! 0534: 0535! 0536: 0537:132 0538:C 0539:c 0540!C 0541!131 0542JC 0543JC 0544iC 0545! 0546! 0547:C 05481133 0549: 0550! 0551! 0552: 0553:c 0554:c 0555:c 0556:c 0557:c 0558:134 0559! 0560: 0561: 0562: 0563: 0564: 0565: 0566iC 0567!C

CONTINUE IF(J.6T.8> 60 TO 120

PACK ASCII LEFT K=0 DO 126 1=1*8

IF(ASCII(I) .EQ.1H ) GO TO 126 K=K+1 ASCII(K)=ASCII(I) CONTINUE

K=K+1 DO 127 J=K»9

ASCIK J)=1H CONTINUE

HATCH CHAR. BY CHAR.

DO 128 I=li8 IF(ASCII(I).NE.SUBNAH(SUB>I)) GO TO 120 CONTINUE

HATCH FOUND PICK UP SUBROUTINE

URITE(L0i507) (SUBNAh(SUBiI>»1=1»8) URITE(LD.SOB) SUBNAH(SUBilO) LOCABS=SUBNAH(SUB>10) L0CREL=0 TEST=SUBNAM(SUBf9)*2 SCHCNT=0 FQUND=.FALSE. CONTINUE NEUREC=.TRUE. READ(U1 >500) (ASCIKI)11 = 1.80) IF(ASCII(7).EQ.1HE.AND.ASCII(B).EQ.IHN .AND.ASCII(9).EQ.1HD) GO TO 133 IF<ASCII(1).EQ.1H ) GO TO 131 DO 132 I=li80

^FtfticiK J) .NE.1H ) GO TO 134 CONTINUE

BLANK RECORD

CONTINUE

COHHENT

URITE(L0.500) (ASCII(I)t1=1>60) GO TO 130

CONTINUE IF(.NOT.FOUND) GO TO 130 URITE(0H>516) (SUBNAM(SUB»I)»1=1»8) URITE(0Hr518) SUBNAM(SUB»9) GO TO 73

NON-BLANK RECORD*

SEARCH FOR '*+LL'

CONTINUE FOUND*.TRUE. JSAV=J+1 DO 136 1=1rJSAV

HCHAR=I-1 IF(ASCII(I),EQ.1H ) GO TO 138 IF(ASCII(I).EQ.1H0) GO TO 137 IF<ASCII(I).NE.lHt) GO TO 136

'*+LL' FOUND* REPLACE IT UITH

MACHINE LANGUAGE START

'LLHH'

1 7 5

0568JC 056?:

137

h\ 0602:200 0603:c 0604:c 060s:c

0607::c 0608:c

!!!

c 202

C c

7!

06 0 0 0

m\ 8S5?I810

m\i %m2n

mi c 0628:c 0629IC 0630.212 0631!C 0632JC 0633:c

m\ 0636S218 0637!C 0638!

IHEX1=ASCII(1+2) IHEX2=ASCII(I+3) CALL CTOH(IHEXl) CALL CT0HCIHEX2) IHEX1=16*IHEX1+IHEX2 LOCSUB=SUBNAM(SUB»10)+IHEX1 CONTINUE

IHEXl-LOCSUB/X'lOOO' IHEX2=<L0CSUB-(IHEX1*X'1000'>)/X'100' IHEX3=(L0CSUB-( IHEX1*X' 1000')-(IHEX2IX' 100') )/X' 10' IHEX4=L0CSUB-( IHEX1*X' 1000' > - (IHEX2*X' 100') - (IHEX3*X '10')

CALL HTOC(IHEXl) CALL HTOC(IHEX2) CALL HT0C(IHEX3) CALL HTOC(1HEX4) ASCIHI ) = IHEX3 ASCII(1+1)=IHEX4 ASCII(I+2 >=IHEX1 ASCII(I+3)=IHEX2 60 TO 136 CONTINUE

SEARCH FOR GLOBAL REFERENCE

IF(ASCII(I+1>.NE.IHO) GO TO 136 IF(ASCII(1+2).NE.1H0) GO TO 136 IF(ASCII(I+3).NE.IHO) GO TO 136

SEARCH FOR GLOBAL FLAG ' * '

00 200 K=IiJSAV IF(ASCII(K).NE.lHt) GO TO 200 GO TO 202 CONTINUE

NO GLOBAL IN THIS STATEMENT

GO TO 136

PICK UP GLOBAL REFERENCE

CONTINUE

SEARCH LEFT

KSAU=K DO 210 K=1»8

J=KSAV-K IF(ASCII(J).EQ.1H ) GO TO 212 IF( ASCIH J) .EQ. 1H() GO TO 212 IF(ASCII(J)>EQ. IHi ) GO TO 212 CONTINUE

NO DELIMETER FOUND

CONTINUE URITE(0HrS26) (SUBNAh(SUBrK)»K=1.B),(ASCII(K)>K-JfKSAV) GO TO 136

VALID DELIMETER FOUND

CONTINUE

PICK UP GLOBAL NAME

DO §HPSL5VK?=LH CONTINUE

L=0

176

0639! 0640! 0641! 0642! 0643! 0644! 064S! 0646! 0647! 0648! 0649! 0650!220 0651!C 0652!C 0653!C 0654! 0655!C 0656!C 0657!C 06581222 0659! 0660! 0661! 0662! 0663! 0664! 0665!224 0666!C 0667!C 0668!C 0669! 0670! 0671! 0672!232 0673SC 0674SC 0675!C 0676! 0677! 06781230 0679!C 0680!C 0681!C 0682! 0683!136 0684!138 0685! 0686! 0687! 0688! 0689! 0690! 0691! 0692! 0693!139 0694! 0695! 0696!C 0697!C 0698!C 0699! 0700! 0701! 0702! 0703!140 0704!C 0705iC 0706iC 0707! 0708! 0709!C

J=J+1 KSAV=J+8 NAMSAV(9)=0 NAMSAV(10)=0 DO 220 K=J.KSAV

L=U+1 IF(ASCII(K).EQ.1H > GO TO 224 IF<ASCII(K>. EQ.1H)) GO TO 224 IF(ASCII(K)>EQ.1H.) GO TO 224 IF (ASCII (K) •EQilH'f > GO TO 222 NAHSAV(L)=ASCI1(K) CONTINUE

NO DELIMETER FOUND

GO TO 211

DISPLACEMENT DELIMETER FOUND • + •

CONTINUE NAMSAV(9)=ASCII(K+1) NAhSAV(10)=ASCII(K+2> CALL CT0H(NAHSAV(9)) CALL CTOH(NAMSAV(10)) IF(NAMSAV(10).EO.-l) GO TO 224 NAMSAV<9)=NAMSAV(9)*X'10'+NAMSAVU0) CONTINUE

FIND NAME IN DIRECTORY

DO 230 J=1»NSUB DO 232 K=l .8

IF(NAMSAV(K).NE.SUBNAM(J>K)) GO TO 230 CONTINUE

MATCH FOUND..SUBSTITUTE CORRECT ADDRESS

LOCSUB=SUBNAM<J.10>+NAMSAV(9) GO TO 234 CONTINUE

UNSATISFIED GLOBAL REFERENCE

HRITE(0H.506) (NAMSAV(K)fK=1»0) CONTINUE

CONTINUE IF(NEMREC)URITE(LO.509) LOCABS.LOCREL.(ASCII(I>.1=1.JSAV) IF <NEMREC) LOCREL=LOCREL+ <NCHAR+1)/2 IF<NEMREC>LOCABS=LOCABS+(NCHAR+1)/2 NEMREC=.FALSE. CHECK=SCHCNT+NCHAR IF(CHECK.LE.TEST) GO TO 139 MRITEtOKi516) (SUBNAM(SUB.I).1=1.8) MRITE(0M>518) SUBNAM(SUB.9> CONTINUE IF(NCHAR.GT.NEED) GO TO 150 IF(NCHAR.LT.NEED) GO TO 160

NCHAR = NUMBER NEEDED BY LOADER

K=LOADSZ-NEED DO 140 1=1(NEED

L=K+I LOADER(L)=ASCII(I) CONTINUE

LOADER FULL. DUMP TO OUTPUT

SCHCNTsSCHCNT+NEED CALL OUTPUT(LOADER.IS.LOADSZ)

177

0710 C 0711 C 0712 0713 c 0714 c 0715 c 0716 0717 c 0718 c 0719 c 0720 0721 150 0722 C 0723 c 0724 c 0725 0726 0727 0728 072? 152 0730 C 0731 C 0732 C 0733 0734 0735 C 0736 C 0737 C 0738 073? 0740 C 0741 c 0742 c 0743 0744 0745 0746 154 0747 c 0748 C 074? C 0750 0751 0752 0753 156 0754 0755 0756 C 0757 C 0758 C 075? 0760 0761 160 0762 C 0763 C 0764 C 0765 0766 0767 0768 076? 162 0770 C 0771 c 0772 c 0773 c 0774 0775 0776 c 0777 c 0778 c 0779 0780 c

DONE WITH THIS RECORD

NEED=LOADSZ

TEST FOR COMPLETION (CHECKSUM)

IF(SCHCNT.LT.TEST) GO TO 130

DONE UITH THIS SUBROUTINE

GO TO 73 CONTINUE

NCHAR > NUMBER NEEDED BY LOADER

K=LOADSZ-NEED DO 152 1=1rNEED

L=K+I LOADER(L)=ASCII(I> CONTINUE

LOADER FULLi DUMP TO OUTPUT

SCHCNT=SCHCNT+NEED CALL OUTPUT(LOADER>ISfLOADSZ)

TEST FOR COMPLETION (CHECKSUH)

IF(SCHCNT.LT.TEST) GO TO 154 IF(SCHCNT.EQ.TEST) GO TO 73

ERROR IN CHECKSUM

NEEIicLOADSZ URITE(0M»516> (SUBNAM(SUB»I)»I=l»8) GO TO 73 CONTINUE

SHIFT ASCII LEFT 'NEED' TIMES

JFIN=80-NEED DO 156 J=l»JFIN

ASCII(J)=ASCII(J+NEED) CONTINUE

ASCII(JFIN+1)=1H NEED=LOADSZ

SIMULATE NEU RECORD UITHOUT READ

J=JFIN GO TO 134 CONTINUE

NCHAR < NUMBER NEEDED BY LOADER

K=LOADSZ-NEED DO 162 1=1iNCHAR

L=K+I LOADER (L)sASCII(I) CONTINUE

LOADER NOT FULL DONE UITH THIS RECORD

SCHCNT=SCHCNT+NCHAR NEED=NEED-NCHAR

TEST FOR COMPLETETION

IF(SCHCNT.LT.TEST) GO TO 130

178

0781JC DONE UITH THIS SUBROUTINE 07825C 0783! GO TO 73 0784 SC 07851500 F0RMAT(80A1> 0786*501 F0RMAT(/'SPC-16/CR0MEMC0 LINKER? '» 07875 + ' CONTROL BASIC / ZBO ASSEHBLY'//) 0788(502 F0RMAT(9H END) 07891504 F0RMAT(8A1>F10>0) 0790!506 FORMAT(/'UNSATISFIED REFERENCE: 'F8A1 07915507 FORHAT(//BOA1/) 0792!508 FORMAT('*='»Z4> 0793:509 FORMAT(Z416X r Z4»6X.80A1) 0794S510 FORMAT(///'REFERENCE MAP'/' 07955511 FORMAT(8A1>3XrI4«5X>Z4) 0796S512 FORMAT(///'SYMBOLS LINE #'/' 07975514 FORMAT(/'SUBROUTINES BEGIN AT!'»Z6> 0798J516 FORHAT(/'CHECKSUM ERROR IN! '»8A1) 0799:518 FORMAT('* BYTES IN ROUTINE NOT EQUAL T05 '.14 08001520 F0RMAT(/I4(' WORDS RESERVED FOR 0(1)') 0801*522 FORMATt/'ERROR! '»8Ali' NOT FOUND IN LIBRARY 0802J524 FORMATt/'UNMATCHED PARENTHESES') 08035526 FORMAT(/'INVALID GLOBAL VARIABLE IN! '»8Alf' 08045 END »ERROR COUNTS OOOOr PSECT SIZE! 4446f DSECT SIZE! 0071 r REV. 5

B LINE'>14)

'/)

)

***'rBAl)

VARIABLES

>501 )10 >11 )20 )500 ) 22 ) 24 )26 )400 ) 402 )404 ) 414 )406 )40B >410 ) 524 ) 412 >30 >32 >34 >36 >502 >40 >50 )56 >52 )300 >325 ) 60 >311 >310 ) 312 >315 >320 1330 )70 ) 72 >74 )76 >80 > 8 2 ) 84 ) 506 >90

1055 0609 05F2 061C 1052 063F 0647 OBOE 0761 06C7 06DC 0766 0709 0703 072A

0808 07EB 0795 07E5 1077 082C 0849 08A8 08A1 096D 08AE 0973 0907 0900 090F 0917 0963 095C 0977 OAFA 0996 09B4 09EA 09CC OAOE 1084 OAAC

FOUND NEUREC LOADSZ IOSGET SI SO LO IS OM U1 MAXREF I J •AIA •AIB

NCALL NREC NBYTES DIMSAV •ALD •ALE NCHAR LSTRT L K H N IHEX1 JSTRT ISUM LOCBGN LOCSUB NSUB JHAX LINE •ALA •ALB II ISUB REC IHEX2 IHEX3 IHEX4

OOOA OOOB 05BC P 05BD P OOOC OOOD OOOE OOOF 0010 0011 0012 0013 0014 0015 0016 0017 001B 0019 001A OOIB 001C 001D 001E 001F 0020 0021 0022 0023 0024 0025 0026 0027 0028 0029 002A 002B 002C 002D 002E 002F 0030 0031 0032 0033

ARRAYS PROCEDURES

SYMBOL 0000 P F$URF 1024 ASCII 0294 P F*TEF 0EF2 SUBNAM 02E4 P FtHDl OEOE Z80DIR 0578 P F$H00 0EF3 NAMSAV 0000 FtREU 0B53 LOADER 057C P FIREF 0C44

F*ARF 0EF4 CTOH OEOF F$E00 07A2 FIDOO OEIO HTOC 0E11 OUTPUT 1027 F$STO 0C46 F*IOS 0C47

09/16/80 BLOCKNAHES

179

>92 0A6C •All 0034 )94 0AA7 *AIE 0035 >96 0AF7 •AIF 0036 >98 0AF1 ISIZE 0037 >508 10A0 ISHIFT 0038 >520 1113 I TUP 0039 >514 10E1 ISTRT 003A >73 0B21 LOAD 003B >100 0B2B NEED 003C >110 0B91 NREAD 003D >510 10AE SUB 003E >62 0B43 LOCABS 003F >511 10C1 LOCREL 0040 >512 10CA TEST 0041 >64 0B6F SCHCNT 0042 >120 OBAE JSAV 0043 >121 OBFE KSAV 0044 >522 1123 CHECK 0045 >122 OCOB JFIN 0046 >124 0C12 >126 0C2F >127 0C48 >128 OC6O >507 109B >130 0CA2 >133 0B06 >131 OCFO >132 OCEA >134 0D38 >516 10F0 >518 10FF >136 OFOO >138 0F06 >137 0DC3 >234 0D7C >200 0DE7 >202 ODEF >210 0E1B >212 0E5Q >211 0E22 >526 1145 >218 0E5A >220 0E98 >224 OEBB >222 OEAO >230 OEEO >232 OEDO >509 10A5 >139 0F73 >150 OFAA >160 101E >140 0F92 >152 OFCO >154 0FF7 >156 100C >162 103D >504 107E

SUBROUTINE HTOC(I> INTEGER CHR(15) DATA CHR/'l'r#2/i'3'»'4,f'5'r'A'f'7'r'8'i/9#f 'A'»'B'»'C'f'D'f'E'»'F'/ J=I IF(J.NE.O) GO TO 10 I=1H0 RETURN I=CHR(J) RETURN END

»ERROR COUNTS 0000» PSECT SIZES 0046» DSECT SIZES 0012! REV. 5 1 LABELS VARIABLES ARRAYS PROCEDURES

00015 0002S 0003! 0004 S 0005S 0006! 0007! 0008! o°mi10

o o i i : 09/16/80 BLOCKNAMES

180

)10 0023 I J •AIA

0009 000A OOOB

CHR 0000 P F*SBU 002B F*HD1 002C F«RET 002D

0001J 0002: 00035 DATA CHAR/'l'i'2'i'J i'4 i'5'i'i' 0004: + 'A'f'B'»'C'»'D'f'E'I'F'/ 0005! 0006! 0007 J 0008: 000?: IF(J.EQ.CHAR(K>) I=K 0010! IF(J.EQ.CHAR(K>) RETURN 0011:10 0012: ooi3: 0014! »ERROR COUNT! 0000. PSECT SIZE: 0072. DSECT SIZE*. 0013f REV. 5 1 LABELS VARIABLES ARRAYS PROCEDURES

SUBROUTINE CTOH(I) INTEGER CHAR(16) DATA CHAR/'1'»'2'. 'A'f'B'.'C'.'D'.'E' J=I IF(J.EQ.IHO) 1=0 IF(J.EQ.IHO) RETURN DO 10 K=l«15

IF(J.EQ.CHAR(K>) IF(J.EQ.CHAR(K)) CONTINUE

1=-1 RETURN END

09/16/S0 BLOCKNAHES

) 10 003B I 0009 J OOOA K OOOB »AIA OOOC

CHAR 0000 P F$SBU 0045 FtHDl 0046 FiRET 0047

OOOi: SUBROUTINE OUTPUT<LOADER»LUN.LOADSZ> 0002! DIMENSION L0ADER(64) 0003! URITE(LUNrlO) (LOADER(I>>I=liLOADSZ> 0004: DO 5 1=1iLOADSZ 0005! LOADERCI)=1H0 0006S5 CONTINUE 0007! RETURN 0008!10 FORNAT(80A1) 0009! END »ERROR COUNT: 0000. PSECT SIZES 0058. DSECT SIZE*. 00145 REV, 1 LABELS VARIABLES ARRAYS PROCEDURES

09/16/80 BLOCKNAHES

>10 >5

0037 002B

LUN OOOA LOADSZ OOOB I OOOC •AIA OOOD

LOADER 0009 FSSBT 0031 F*URF 0032 FtHDl 0033 F»ARF 0034 FtTEF 0035 FIRET 0036

SPC-16 CLOB REV 7 T PSECT RANGE DSECT RANGE DYNS DEF VALUE DEF VALUE DEF VALU

181

SPC-16/CR0MEMC0 LINKERS CONTROL BASIC / Z80 ASSEKBLY

0 UORDS RESERVED FOR 6(1)

SUBROUTINES BEGIN ATS 2500

CHKjSUH *=2500

CHECK - SUM ROUTINES 3 PARAMETERS

1. STARTING ADDRESS 2. NUMBER OF BYTES 3. CHECK-SUM

2500 0 FDE1 POP IY 2502 2 DDE1 POP IX 2504 4 FD6E00 LD L,(IY+O) 2507 7 FD6601 LD H»(IY+1) 250A A DD4E00 LD C,(IX+0) 250D D DD4601 LD B»(IX+1) 2510 10 1600 LD D,00 2512 12 7A NEXT LD A,D 2513 13 B6 ADD Ar(HL) 2514 14 23 INC HL 2515 15 OB DEC BC 2516 16 57 LD Dt A 2517 17 3E00 LD A ,00 2519 19 B9 CP C 251A 1A 20F6 JR NZ NEXT 251C 1C B8 CP B 251D ID 20F3 JR NZ NEXT 251F IF El POP HL 2520 20 7E LD A,(HL) 2521 21 BA CP 0 2522 22 C8 RET Z 2523 23 3E03 LD A»"C 2525 25 D301 OUT (01),A 2527 27 C35204 JP BASIC

GET START OF CHKSUM A GET NUHBER OF BYTES A SET HL TO STARTING AD

SET BC TQ NUMBER OF BYTES TO BE ADDED INITIALIZE CHKSUM

UPDATE CHKSUM POINT TO NEXT BYTE DECREMENT BYTE COUNT SAVE CHKSUM IN D

CHECK IF DONE

GET ADDRESS OF CHKSUM GET L.S.B. OF CHKSUM COMPARE WITH COMPUTED RETURN IF CHKSUMS ARE CHKSUHS ARE NOT EQUAL SEND "C TO SPC-16 TRY AGAIN

SETUP *=252A

INITIALIZATION ROUTINE

252A 0 3E09 LD A»09 252C 2 D302 OUT " (02) iA 252E 4 3E09 LD A,09 2530 6 D3A2 OUT (A2)»A 2532 8 3E09 LD A,09 2534 A D3B2 OUT (B2), A 2536 C 3E30 LD A,30 2538 E D303 OUT (03)fA 253A 10 3E3B LD A»3B 253C 12 D3A3 OUT (A3)>A 253E 14 3E10 LD AilO 2540 16 D3B3 OUT (B3) ,A 2542 18 3E10 LD A,10 2544 1A D300 OUT (00) ,A 2546 1C 3E04 LD A,04 2548 IE D3A0 OUT (AO),A 254A 20 3E08 LD A,08 254C 22 D3B0 OUT (BO),A 254E 24 3E3E LD A,3E 2550 26 ED47 LD I,A

RESET SCC

RESET UART-A

RESET UART-B

MASK FOR SCC

MASK FOR UART-A

MASK FOR UART-B

BAUD SCC = 2400

BAUD UART-A = 300

BAUD UART-B = 1200

SET PAGE OF INTERRUPT

182

2552 28 ED5E IM 2 2554 2A El POP HL 2555 2B 31B030 LD SPi30B0 2558 2E E5 PUSH HL 2559 2F CD3C28 CALL IT«MAP 255C 32 0EA1 LD C>A1 255E 34 210E04 LD HL>040E 2561 37 CD3029 CALL PSMSG 2564 3A 3E80 LD At 80 2566 3C D3A5 OUT <AS)iA 2568 3E FB EI 2569 3F 1SFE LOOP JR LOOP

SET Z-80 MODE INTERRU

SET TOP OF SYSTEM STAC

FILL ISR TABLE

'CROMEHCO SCCHON'

START TIMER-1

UAIT FOR AN INTERRUPT

T*ISR *=256B

TABLE OF INTERRUPT SERVICE ROUTINES ( ISR )

256B 0 1C26 DU HtISR+50 A - TIMER1 256D 2 2C26 DU HtISR+60 A - TIMER2 256F 4 0000 DU A - SENS 2571 6 3C26 DU HtISR+70 A - TIMER3 2573 8 EC25 DU HSISR+20 A - RDA 2575 A FC25 DU H*ISR+30 A - TBE 2577 C 0000 DU A - TIMER4 2579 E 0000 DU A - TIHERS 257B 10 0000 DU B - TIHER1 257D 12 0000 DU B - TIMER2 257F 14 0000 DU B - SENS 2581 16 0000 DU B - TIMER3 2583 18 0C26 DU HIISR+40 B - RDA 2585 1A 0000 DU B - TBE 2587 1C 0000 DU B - TIMER4 2589 IE 0000 DU B - TIMERS 258B 20 000000 DBDU 258E 23 00000000 DUDU 2592 27 00000000 DUDU SCC - TIMER1 2596 2B 00000000 DUDU 259A 2F 00000000 DUDU SCC - TIHER2 259E 33 00000000 DUDU 25A2 37 00000000 DUDU SCC - SENS 25A6 3B 00000000 DUDU 25AA 3F 00000000 DUDU SCC - TIHER3 25AE 43 00000000 DUDU 25B2 47 CC25CC25 DUDU HiISR+0 SCC - RDA 25B6 4B 00000000 DUDU 25BA 4F DC25DC25 DUDU HtISR+10 SCC - TBE 25BE 53 00000000 DUDU 25C2 57 00000000 DUDU SCC - TIMER4 25C6 SB 00000000 DUDU 25CA 5F 0000 DU SCC - TIMER5

HtlSR *=25CC

INTERRUPT SERVICE ROUTINE HANDLER

SCC RDA ENTRY

25CC 25CF 25D3 25D6 25D9

25DC

CD4C26 DD2A7626 CD9E26 CD5D26 FBC900

SCC TBE ENTRY

10 CD4C26

CALL LD CALL CALL RETI

CALL

SARSt IXi(TfPUT+8) DtRDA LARS*

SARSt

SAVE ALL REGISTERS GET DCB ADDRESS CALL INPUT DRIVER LOAD ALL REGISTERS RETURN FROM INTERRUPT

SAVE ALL REGISTERS

183

25DF 13 DD2A7826 LD IX»(TtPUT+A) GET DCB ADDRESS 25E3 17 CDDD26 CALL D*TBE CALL OUTPUT DRIVER 25E6 1A CD5D26 CALL LARSt LOAD ALL REGISTERS 25E9 10 FBC900 RETI RETURN FROH INTERRUPT

UART-A RDA ENTRY

25EC 20 CD4C26 CALL SARSt 25EF 23 DD2A8626 LD IX»(T*PUT+18) 25F3 27 CD9E26 CALL DtRDA 25F6 2A CD5D26 CALL LARS* 25F9 2D FBC900 RETI

UART-A TBE ENTRY

25FC 30 CD4C26 CALL SARSt 25FF 33 DD2A8826 LD IX»(TtPUT+lA) 2603 37 CDDD26 CALL DtTBE 2606 3A CD5D26 CALL LARSt 2609 3D FBC900 RETI

UART-B RDA ENTRY

260C 40 CD4C26 CALL SARSt 260F 43 DD2A9626 LD IX r(TtPUT+28) 2613 47 CD9E26 CALL DtRDA 2616 4A CD5D26 CALL LARSt 2619 4D FBC900 RETI

TUART A TIHER-1 ENTRY

261C 50 CD4C26 CALL SARSt 261F 53 DD2A7E26 LD IXr(TtPUT+10) 2623 57 CDC32A CALL DtTIHR 2626 5A CD5D26 CALL LARSt 2629 5D FBC900 RETI

TUART A TIMER-2 ENTRY

262C 60 CD4C26 CALL SARSt 262F 63 DD2AB026 LD IXt(TtPUT+12) 2633 67 CDC32A CALL DtTIHR 2636 6A CD5D26 CALL LARSt 2639 6D FBC900 RETI

TUART A TIMER-3 ENTRY

263C 70 CD4C26 CALL SARSt 263F 73 DD2A8426 LD IX>(TtPUT+16) 2643 77 CDC32A CALL DtTIHR 2646 7A CD5D26 CALL LARSt 2649 7D FBC900 RETI

SARSt *=264C

SAVE ALL REGISTERS

264C 0 D9 EXX 264D 1 El POP HL SAVE RETURN ADDRESS 264E 2 FDE5 PUSH IY SAVE IY ON STACK 2650 4 E5 PUSH HL HOVE RETURN ADDRESS TO IY 2651 5 FDE1 POP IY 2653 7 D9 EXX 2654 a F5 PUSH AF 2655 9 C5 PUSH BC 2656 A D5 PUSH DE SAVE ALL REGISTERS 2657 B E5 PUSH HL 2658 C DDE5 PUSH IX

184

265A E FDE5 PUSH IY 265C 10 C9 RET

LARS* M265D

LOAD ALL REGISTERS

265D 0 FDE1 POP IY 265F 2 DDE1 POP IX 2661 4 El POP HL 2662 5 D1 POP DE 2663 6 CI POP BC 2664 7 F1 POP AF 2665 8 D9 EXX

AF

2666 9 FDE5 PUSH IY 2668 B El POP HL 2669 C FDE1 POP IY 266B E E5 PUSH HL 266C F D9 EXX 266D 10 C9 RET

RESTORE RETURN ADDRESS

SAVE RETURN ADDRESS

LOAD ALL REGISTERS

MOVE RETURN ADDRESS TO HL

RESTORE IY RESTORE RETURN ADDRESS

T$PUT *=266E

TABLE OF PHYSICAL UNITS

266E 0 0000 DU 2670 2 0000 DU 2672 4 0000 DU 2674 6 0000 DU 2676 8 2D2A DU 2678 A 4E2A DU 267A C 0000 DU 267C E 0000 DU 267E 10 602C DU 2680 12 732C DU 2682 14 0000 DU 2684 16 7F2C DU 2686 18 4E2A DU 2688 1A 2D2A DU 268A 1C 0000 DU 26BC IE 0000 DU 268E 20 0000 DU 2690 22 0000 DU 2692 24 0000 DU 2694 26 0000 DU 2696 28 6F2A DU 2698 2A 0000 DU 269A 2C 0000 DU 269C 2E 0000 DU

SSDCB A$DCB

AltDCB A2SDCB

A3IDCB AtDCB StDCB

BtDCB

SCC TIHER1 DCB SCC TIHER2 DCB SCC SENS DCB SCC TIHER3 DCB SCC RDA DCB SCC TBE DCB SCC TIMER4 DCB SCC TIHER5 DCB

TIHER1 DCB TIMERS DCB SENS DCB TIMER3 DCB RDA DCB TBE DCB TIHER4 DCB TIMERS DCB TIMER1 DCB TIMER2 DCB SENS DCB TIMER3 DCB RDA DCB TBE DCB TIMER4 DCB TIMER5 DCB

DtRDA *=269E

DRIVER FOR RECEIVER DATA AVAILABLE ( RDA )

269E 0 DD4E08 LD C»(IX+B) 26A1 3 CD6E29 CALL H*INPT 26A4 6 0E11 LD Cill 26A6 8 0600 LD BiOO 26A8 A DDE5 PUSH IX 26AA C FDE1 POP IY 26AC E FD09 ADD IY.BC 26AE 10 CD6427 CALL HiRDA 26B1 13 DD6E02 LD Lf(IX+2) 26B4 16 DD6603 LD Hr(IX+3)

GET INPUT PORT NUMBER GET CHARACTER GET OPTION LIST

TRANSFER IX TO IY

CALL CHARACTER HANDLE PUT CHARACTER IN BUFF

185

26B7 19 DD7E09 LB A»(IX+9) 26BA 1C 77 LD (HL)IA 26BB ID 23 INC HL 26BC IE DD4E06 LD CF(IX+6) 26BF 21 DD4607 LD B»(IX+7) 26C2 24 78 LD AFB 26C3 25 BC CP H 26C4 26 200A JR NZ RDA1 26C6 28 79 LD AFC 26C7 29 BD CP L 26C8 2A 2006 JR NZ RDA1 26CA 2C BD6E04 LD LF(IX+4) 26CD 2F DD660S LD HF (IX+5) 26D0 32 DD7502 RDA1 LD (1X4-2) >L 26D3 35 DD7403 LD (IX+3)FH 26D6 38 CDA92A CALL X$OFF 26D9 3B CD4D29 CALL 0$CHK 26DC 3E C9 RET

POINT TO NEXT LOCATIO

CHECK FOR END OF BUFF

IF POINTER IS AT ENDI RESET POINTER TO BEGINNING.

UPDATE RDA POINTER

BiTBE *=26DD

DRIVER FOR TRANSMITTER BUFFER EMPTY ( TBE )

26DB 0 DD4E0A LD C R <IX+A) 26E0 3 DD6E00 LD LF(IX+O) 26E3 6 DD6601 LD HF(IX+1) 26E6 9 DD5E02 LD EF(IX+2) 26E9 C DD5603 LD DF(IX+3) 26EC F 7B LD AFE 26ED 10 BD CP L 26EE 11 2008 JR NZ TBE1 26F0 13 7A LD AFD 26F1 14 BC CP H 26F2 15 2004 JR NZ TBEL 26F4 17 CD2828 CALL H»DPLX 26F7 1A C9 RET 26F8 IB CD1D27 TBE1 CALL HtTBE 26FB IE DD6EOO LD LF(IX+O) 26FE •21 DD6601 LD HF(IX+1) 2701 24 23 INC HL 2702 25 DD5E06 LD EF(IX+6) 2705 28 DD5607 LD DF(IX+7) 2708 2B 7B LD AFE 2709 2C BD CP L 270A 2D 200A JR NZ TBE2 270C 2F 7A LD AFD 270D 30 BC CP H 270E 31 2006 JR NZ TBE2 2710 33 DD6E04 LD LF(IX+4) 2713 36 DD6605 LD HF(IX+5) 2716 39 DD7500 TBE2 LD (IX+O)FL 2719 3C DD7401 LD (IX+1) FH 271C 3F C9 RET

GET OUTPUT PORT NUMBE

CHECK FOR TBE POINTER EQUAL TO RDA POINTER

IF TBE POINTER EQUALS POINTERI BUFFER IS EH

SCHEDULE FULL DUPLEX

CALL CHARACTER HANDLE UPDATE TBE POINTER TO NEXT BUFFER ADORES

CHECK IF TBE POINTER IS AT THE END OF BUFF

IF TBE POINTER IS AT OF BUFFERF SET POINTE THE BEGINNING OF BUFF

PUT UPDATED POINTER I

H*TBE M271D

HANDLER FOR TRANSMITTER BUFFER EMPTY

271D 271E 2720 2722 2723 2725 2726 2728

79 FEA1 2016 OD ED78 OC E6C4 EE84

LB CP JR NZ DEC IN INC AND XOR

A>C A1 TBE1 C AF (C) C AFC4 A>84

CHECK FOR TTY OUTPUT

IF NOT TTY OUTPUT TEST UART STATUS

GET RDAR TBE. AND SRV TEST FOR RDA SETF

186

272A D 2802 JR Z TBEO TBE RESET. OR SRV RES 272C F El POP HL RETURN TO INTERRUPT D 272D 10 C? RET 272E 11 7E TBEO LD Ar(HL) TTY OUTPUT ONLY 272F 12 ED79 OUT (C) r A OUTPUT CHARACTER 2731 14 DD770B LD (IX+B)»A SAVE DATA IN DCB 2734 17 CD902A CALL XtON

SAVE DATA IN DCB

2737 1A C9 RET 2738 IB FD2A7626 TBE1 LD IYf(T$PUT+8) SET IY TO ADDRESS 273C IF FD7E0B LD A»(IY+B) OF SCC RDA DCB 273F 22 FEAE CP / /

* CHECK IF LAST CHARACT 2741 24 2803 JR Z TBE2 FROM SPC UAS A PROMPT 2743 26 FDE1 POP IY POP STACK SO RETURN I 2745 28 C9 RET THE INTERRUPT DRIVER 2746 2? 7E TBE2 LD At (HL) PROMPT FOUND SO SEND 2747 2A FEOD CP <CR> CHARACTER TO SPC 274? 2C 2004 JR NZ TBE3 CHECK FOR <CR> TO BE 274B 2E FD360B00 LD (IY+B)»00 SENTi CHANGE LAST CHA 274F 32 DD770B TBE3 LD CIX+B)> A SAVE DATA IN DCB 2752 35 C5 PUSH BC SAVE BC 2753 36 0EA1 LD CrAl 2755 38 CDDF28 CALL OUT$ ECHO TO TTY 2758 3B OD DEC C 275? 3C ED78 TBE4 IN A r (C) GET PORT STATUS 275B 3E E680 AND A>80 WAIT FOR TBE SET 275D 40 28FA JR Z TBE4 275F 42 CI POP BC RESTORE BC 2760 43 7E LD At(HL) 2761 44 ED79 OUT (C) iA SEND CHARACTER TO SPC 2763 46 C? RET

HtRDA *=2764

HANDLER FOR RECEIVER 1 DATA AVAILABLE

2764 0 DD7E09 LD A>(IX+9) GET CHARACTER 2767 3 FDBEOO CP (IY+O) 276A 6 CABC27 JP Z DUMP SEND DATA TO REQUESTI 276D ? FDBE01 CP (IY+1) 2770 C CAC327 JP Z CNTRLO STOP SPC-16 OUTPUT 2773 F FDBE02 CP (IY+2) 2776. 12 CACA27 JP Z GOSCC GO TO SCC MONITOR 277? 15 FDBE03 CP (IY+3) DUMP CHROHATOGRAPH 277C 18 CACF27 JP Z CHRTTY TO TTY 277F IB FDBE04 CP (IY+4) DUMP CHROMATOGRAPH 2782 IE CAD827 JP Z CHRSPC TO SPC 2785 21 FDBE05 CP (IY+5) 2788 24 CAE127 JP Z CHRDEL DELETE CHROMATOGRAPH 278B 27 FDBE08 CP (IY+8) 278E 2A CAE627 JP Z CNTRLS STOP SPC OUTPUT 27?1 2D FDBEO? CP (IY+9) 2794 30 CAFA27 JP Z CNTRLQ CONTINUE SPC OUTPUT 27?7 33 FDBEOA CP (IY+A) 279A 36 CA0228 JP Z CNTRLU CHANGE <DEL> TO "U 279D 39 FDBEOB CP (IY+B) DISABLE CHROHATOGRAPH 27 AO 3C CA0828 JP Z NOCHR 27A3 3F FDBEOC CP (IY+C> ENABLE CHROMATOGRAPH 27A6 42 CA1028 JP Z ONCHR 27A? 45 FDBEOD CP (IY+D) IGNORE CONTROL R 27AC 48 CA1828 JP Z IGNORE 27AF 4B FDBEOE CP (IY+E) IGNORE CONTROL I 27B2 4E CA1828 JP z IGNORE 27B5 51 FDBEOF CP (IY+F) CHROMATOGRAPH EOT 27B8 54 CA1C28 JP z CHREOT 27BB 57 C9 RET

RDA HANDLER OPTIONS

187

27BC 58 CDD02C DUMP CALL DUHPf DUMP DATA BUFFER 27BF 5B El POP HL 27C0 5C C34D29 JP OfCHK 27C3 5F CDD529 CNTRLO CALL CNTLf0 STOP SPC-16 OUTPUT 27C6 62 El POP HL 27C7 A3 C34D29 JP OfCHK 27CA 66 CD8729 GOSCC CALL GOfSCC CALL CONTROL C HANDLE 27CD 6? El POP HL 27CE 6A C9 RET 27CF 6B 0EA1 CHRTTY LD CrAl SET OUTPUT TO TTY 27D1 6D CD4A28 CALL CfDUMP DUHP BUFFER TO TTY 27D4 70 El POP HL RETURN TO INTERRUPT D 27D5 71 C34D29 JP OfCHK 27D8 74 OEOl CHRSPC LD CfOl SET OUTPUT TO SPC 27DA 76 CD4A28 CALL CfDUHP DUMP BUFFER TO SPC 27DD 7? El POP HL RETURN TO INTERRUPT D 27BE 7A C34D29 JP 0*CHK 27E1 7D CDE828 CHRDEL CALL C*DEL DELETE CHROHATORAPH B 27E4 80 El POP . HL 27E5 81 C9 RET 27E6 82 3E13 CNTRLS LD Af "S "S TO SPC-16 27ES 84 D301 OUT (01)>A

"S TO SPC-16

27EA 86 FD212D2A LD IYfSiDCB 27EE 8A FD7E0D LD A.(IYtD) GET -Q ENABLE BIT 27F1 8D E6FE AND AiFE RESET BIT TO DISABLE 27F3 8F FD770D LD (IY+D)»A 27F6 92 El POP HL 27F7 93 C34D29 JP OfCHK 27FA 96 3E11 CNTRLQ LD A.~Q "Q TO SPC-16 27FC 98 D301 OUT (01> fA 27FE 9A El POP HL 27FF 9B C34D29 JP OtCHK 2802 9E 3E15 CNTRLU LD A»"U CHANGE <DEL> TO ~U 2804 AO DD7709 LD (IX+9)»A 2807 A3 C9 RET 2808 A4 3E00 NOCHR LD AtOO MASK FOR RDA DISABLE 280A A6 D3B3 OUT (B3) i A AT THE CHROMATOGRAPH 280C A8 El POP HL

AT THE CHROMATOGRAPH

280D A9 C34D29 JP OSCHK 2810 AC 3E10 ONCHR LD A«10 MASK FOR RDA ENABLE 2812 AE D3B3 OUT (B3)>A AT THE CHROMATOGRAPH 2814 BO El POP HL 2815 B1 C34D29 JP OfCHK 2818 B4 El IGNORE POP HL IGNORE CHARACTER 2819 B5 C34D29 JP OfCHK 281C B8 0EA1 CHREOT LD CiAl CHROMATOGRAPH END 281E BA 21AD29 LD HLiTtMSG OF TRANSMISSION 2821 BD CD3029 CALL PfhSG 'SEND DATA TO SPC-16' 2824 CO El POP HL 2825 CI C34D29 JP OfCHK

HtDPLX *=2828

FULL DUPLEX PROTOCOL

2828 0 DD7E08 LD Ar(IX+8) IF NOT UART-A TBEi RE 282B 3 FE01 CP 01 282D 5 CO RET NZ

01

282E 6 DD7E0B LD Ar(IX+B) IF NOT SPC PROMPTi RE 2831 9 FEAE CP 1 1

» 2833 B CO RET NZ 2834 C DD2A7826 LD IX>(TfPUT+A) 2838 10 CDDD26 CALL DfTBE SIMULATE AN INTERRUPT 283B 13 C9 RET

SIMULATE AN INTERRUPT

ITfMAP *=283C

188

MOVES PSEUDO ISR TABLE INTO WORKING ISR TABLE 283C 0 216B25 LD HLrTJISR 283F 3 ED57 LD Ail 2841 S 57 LD DrA 2842 6 1EA0 LD Er AO 2844 8 016100 LD BCt0061 2847 B EDBO LDIR 2849 D C9 RET

START ADDRESS IS PSEU INTERRUPT SERVICE ROU TABLE. DESTINATION I INTERRUPT SERVICE ROU TABLE. USES BLOCK TR TO MAP THE TABLE.

C*DUHP *=284A

HANDLER FOR DUMPING CHROHATOGRAPH BUFFER

284A 0 CDB82C CALL ENTRY* ENABLE TIHERS 284D 3 FD2A9626 LD IYf(T*PUT+28) GET B-DCB ADDRESS 2851 7 FD6E00 LD Lr(IY+O) 2854 A FD6601 LD H» <IY+1) SUMP BEGINNING 2857 D FD5E02 LD Ei(IY+2) 285A 10 FD5603 LD Di(IY+3) DUMP ENDING 285D 13 79 LD ArC 285E 14 FE01 CP 01 DETERMINE WHICH PORT 2860 16 28 ID JR Z SDMP

2862 2864 2867 2869 286C 286D 286E 2870 2871 2872 2874 2877 2878

DUMP TO TTY

18 1A ID IF 22 23 24 26 27 28 2A 2D 2E

3E0A CDDF28 3E0D CDDF28 7D BB 2008 7C BA 2004 CDC42C C9 7E

TDMP1

LD CALL LD CALL LD CP JR NZ LD CP JR NZ CALL RET

Ar<LF> OUT* Ar<CR> OUT* ArL E TDMP2 ArH D TDMP2 EXIT*

2879 2F CDDF28 CALL OUT* 287C 32 23 INC HL 287D 33 18ED JR TDMP1

DUMP TO SPC

287F 35 FD360C00 SDMP LD (IY+C>r00 2883 39 7D SDMP1 LD ArL 2884 3A BB CP E 2885 3B 201B JR NZ SDHP2 2887 3D 7C LD ArH 2888 3E BA CP D 2889 3F 2017 JR NZ SDMP2 288B 41 CD2229 CALL SHAKE* 28BE 44 FD7E0C LD Ar(IY+C) 2891 47 CD2B2D CALL P2*HEX 2894 4A CD2A29 CALL CR* 2897 4D FD7E0C LD Ai (IY+C) 289A 50 FEOO CP 00 289C 52 200F JR NZ SDMP3 289E 54 CDC42C CALL EXIT* 28A1 57 C9 RET 28A2 58 3E0D SDMP2 LD Ai<CR> 28A4 5A BE CP (HL) 28A5 SB 23 INC HL 28A6 5C 20DB JR NZ SDMP1 28A8 5E FD340C INC (IY+C) 28AB 61 18D6 JR SDMP1

INITIALIZE PRINTER

CHECK FOR END OF DUMP

ENABLE INTERRUPTS

GET CHARACTER OUTPUT CHARACTER POINT TO NEXT LOCATIO

INITIALIZE <CR> COUNT

CHECK FOR END OF DUMP

OUTPUT NUMBER OF RECO

CHECK FOR NULL DUHP

ENABLE INTERRUPTS

CHECK FOR <CR>

INCREMENT RECORD COUN

189

28AD 63 CD2229 SDHP3 CALL SHAKE* 28B0 66 FD6E00 LD Li(IY+O) 28B3 69 FD6601 LD Hi(IY+l) 28B6 AC 7D SDMP6 LD AiL 28B7 6D BB CP E 28B8 6E 200B JR NZ SDHP4 28BA 70 7C LD AiH 28BB 71 BA CP D 2BBC 72 2007 JR NZ SDMP4 28BE 74 CD2A29 CALL CR* 28C1 77 CDC42C CALL EXIT* 28C4 7A C9 RET 28C5 7B 7E SDMP4 LD At(HL) 28C6 7C 23 INC HL 28C7 7D CDDF28 CALL OUT* 28CA 80 FEOD CP <CR> 28CC 82 20E8 JR NZ SDMP6 28CE 84 7D LD AiL 28CF 85 BB CP E 28DO 86 2008 JR NZ C0NT2 28D2 88 7C LD A»H 28D3 89 BA CP D 28114 8A 2004 JR NZ C0NT2 28D6 8C CDC42C CALL EXIT* 28D9 8F C9 RET 28DA 90 CD2229 C0NT2 CALL SHAKE* 28DD 93 18E6 JR SDHP4

INITIALIZE DUMP POINT

CHECK FOR END OF BUFF

IF NOT END OF BUFFER


SEND LAST RECORD

GET CHARACTER UPDATE POINTER OUTPUT THE CHARACTER CHECK FOR <CR> IF NOT CARRIAGE RETUR CHECK FOR END OF BUFF


IF NOT END OF BUFFER END OF BUFFER

HANDSHAKE WITH SF'C-16

OUT* *=28DF

CHARACTER OUTPUT HANDLER UHEN INTERRUPTS ARE DISABLED

28DF 28E2 28E4 28E7

0 CD1729 3 ED79 5 CD1729 8 C9

CALL OUT CALL RET

0*D0NE <C)iA OSDONE

ENSURE BUFFER IS EHPT OUTPUT CHARACTER

CiDEL *=28E8

INITIALIZE THE CHROHATOGRAPH BUFFER

28E8 0 2A9626 LD HLi<T*PUT+28) GET B-DCB ADDRESS 28EB 3 E5 PUSH HL 28EC 4 FDE1 POP IY TRANSFER HL TO IY 28EE 6 FD6E04 LD L»(IY+4) 28F1 9 FD6605 LD Hi(IY+5) 28F4 C FD7502 LD CIY+2)iL SET RDA BUFFER POINTE 28F7 F FD7403 LD (IY+3)iH TO THE BUFFER BEGINNI 28FA 12 DD2A7E26 LD IXi<T*PUT+10> GET TIHER-1 DCB 28FE 16 DD6E0B LD L»(IX+B > 2901 19 DD660C LD Hi(IX+C) GET T-6 POINTER 2904 1C DD5E0D LD Ei(IX+D) 2907 IF DD560E LD D»(IX+E) GET T-15 POINTER 290A 22 FD750D LD <IY+D)iL 290D 25 FD740E LD (IY+E) iH SAVE T-6 POINTER 2910 28 FD730F LD (IY+F)»E 2913 2B FD7210 LD (IY+10)iD SAVE T-15 POINTER 2916 2E C9 RET

0*D9NE *=2917

WAIT UNTIL TBE HIGH

190

2917 0 F5 PUSH AF 2918 1 OD PEC C 2919 2 ED78 LOOP IN Ai (C) 291B 4 E480 AND Ar80 291D 4 28FA JR Z LOOP 291F 8 OC INC C 2920 9 F1 POP AF 2921 A C9 RET

SAVE AF AND BC

GET STATUS GET TBE BIT WAIT UNTIL TBE SET

RETORE AF AND BC

SHAKE* *=2922

HANDSHAKE ROUTINE FOR ZBO/SPC

2922 2925 2927 2929

CDA029 UAIT FE2E 20F9 C9

CAUL CP JR NZ RET

GETCH* / t UAIT

LOOK FOR PROMPT

LOOP UNTIL PROMPT

CR* *=292A

ROUTINE TO OUTPUT A CARRIAGE RETURN

292A 292C 292F

3E0D CDDF28 C9

LB CALL RET

At<CR> OUT*

OUTPUT A <CR>

PtMSG *=2930

PRINTS MESSAGE BEGINNING AT (HL) DONE WHEN PARITY BIT SET

2930 0 CDB82C CALL ENTRY* 2933 3 F5 PUSH AF 2934 4 E5 PUSH HL 2935 5 3E0A LB A.<LF> 2937 7 CDDF28 CALL OUT* 293A A 3E0D LD Ai<CR> 293C C CDDF28 CALL OUT* 293F F 7E PSl LD Ai(HL) 2940 10 23 INC HL 2941 11 CDDF28 CALL OUT* 2944 14 17 RLA 2945 15 30F8 JR NC PSl 2947 17 El POP HL 2948 18 F1 POP AF 2949 19 CDC42C CALL EXIT* 294C 1C C9 RET

SAVE ACCUMULATOR SAVE ADDRESS

OUTPUT <LF>

OUTPUT <CR>

OUTPUT MESSAGE

CHECK FOR PARITY SET

0*CHK *=294D

CHECK FOR OUTPUT INTERRUPT REQUEST

294D 0 DD4E0A LD C?(IX+A) 2950 3 79 LD AtC 2951 4 FEB1 CP B1 2953 6 2810 JR Z CHK 2955 8 OD DEC C 2954 9 ED78 IN A> (C) 2958 B E4C4 AND Af C4 295A D EE84 XOR A.84 295C F 2007 JR NZ CHK 295E 11 • ED78 IN Ar (C)

GET OUTPUT PORT NUMBE

CHECK FOR CHROMATOGRA

SET TO STATUS PORT GET OUTPUT PORT STATU GET RDAr TBEi AND SRV CHECK FOR RDA SETt SRV RESET» OR TBE RES GET STATUS

191

2960 13 E680 AND At 80 2962 15 C4DD26 CALL NZ DtTBE 2965 18 DD7E0A CHK LD

NZ AF <IX+A)

2968 IB FEA1 CP A1 296A ID C4FC25 CALL NZ HIISR+30 29 6D 20 C9 RET

HIISR+30

MASK FOR TBE SET

CHECK OUTPUT PORT NUM

IF OUTPUT NOT TO TTYf SIMULATE A TTY THE RE

HilNPT *=296E

INPUT CHARACTER AND CHECK FOR SPC-16 PROMPT

A> (C) B>A ArC 01 IN2 AiB A.7F (IX+9)»A

AfB

296E 0 ED78 IN 2970 2 47 LD 2971 3 79 LD 2972 4 FE01 CP 2974 6 2807 JR Z 2976 8 78 INI LD 2977 9 E67F AND 2979 B DD7709 LD 297C E C9 RET 297D F 78 IN2 LD 297E 10 FE2E CP 2980 12 20F4 JR NZ 2982 14 DD3609AE LD 2986 18 C9 RET

INI (IX+9) AE

GET INPUT DATA SAVE DATA IN B CHECK INPUT PORT

INPUT NOT VIA SPC-16 HASK OF PARITY SAVE IN DCB

INPUT VIA SPC-16 CHECK FOR PROMPT

PROMPT FOUND

GOSSCC *=2987

CONTROL C HANDLER

2987 0 3E13 LD 2989 2 D301 OUT 298B 4 CDB82C CALL 298E 7 0E01 LD 2990 9 3E03 LD 2992 B CDDF28 CALL 2995 E 3E00 LD 2997 10 CDDF28 CALL 299A 13 CDD529 CALL 299D 16 C3C42C JP

GETCHt *=29A0

CHARACTER INPUT HANDLER

29A0 0 OD DEC 29A1 1 ED78 CHKIN IN 29A3 3 E640 AND 29A5 5 28FA JR Z 29A7 7 OC INC 29A8 8 ED78 IN 29AA A E67F AND 29AC C C9 RET

A»"S (Ol)rA ENTRY* CfOl A."C OUTS Af 00 OUT« CNTLfO EXIT*

C Ai(C) A.40 CHKIN C A»(C> A.7F

STOP SPC-16 OUTPUT

ENABLE TIMERS

SEND "C TO SPC-16

SEND A NULL TO SPC-lo

INITIALIZE THE BUFFER RETURN TO THE HANDLER

SET TO STATUS PORT

UAIT FOR CHARACTER

INPUT CHARACTER

MASK OFF PARITY

TfHSG *=29AD

TABLE OF USER MESSAGES

29AD 29AE 29AF 29B0

OD OA 2A 2A

DB DB DB DB

<CR> <LF>

'*'

29B1 4 2A DB 29B2 5 20 DB <SP> 29B3 6 53 DB 'S' 29B4 7 68 DB 'H' 29B5 8 69 DB 'I' 29B6 9 70 DB /pi 29B7 A 20 DB <SP> 29B8 B 64 DB 'D' 29B9 C 61 DB 'A' 29BA B 74 DB 'T' 29BB E 61 DB 'A' 29BC F 20 DB <SP> 29BD 10 74 DB ' T 29BE 11 6F DB '0' 29BF 12 20 DB <SP> 29C0 13 74 DB 'T' 29C1 14 68 DB 'H' 29C2 15 65 DB 'E' 29C3 16 20 DB <SP> 29C4 17 53 DB 'S' 29C5 18 50 DB ,p, 29C6 19 43 DB 'C' 29C7 1A 2D DB / _ /

29C8 IB 31 DB '1' 29C9 1C 36 DB '6' 29CA ID 21 DB ' I' 29CB IE OD DB <CR> 29CC IF OA DB <LF> 29CD 20 0707 DU "G 29CF 22 0707 DU ~G 29D1 24 0707 DU "G 29D3 26 0787 DU "G

CNTHO *=29D5

INHIBIT OUTPUT ROUTINE

29D5 0 FD2A7626 LD IY(T*PUT+8) 29D9 4 FD7E0B LD At <IY+B) IGNORE IF INP 29DC 7 FEAE CP t t IS SOLICITED 29DE 9 C8 RET Z 29DF A 3E0F LD A r"0 29E1 C D301 OUT (01),A 29E3 E CDB82C CALL ENTRY* ENABLE TIMERS 29E6 11 0EA1 LD CiAl 29E8 13 3E0D LD A»<CR> 29EA 15 CDDF28 CALL OUT* OUTPUT A <CR> 29ED 18 3E0A LD Af<LF> 29EF 1A CDDF28 CALL OUT* OUTPUT A <LF> 29F2 ID FD7E09 LD A»(IY+9) 29F5 20 FEAE CP / /

29F7 22 2008 JR NZ CNTLO OUTPUT "0 IF 29F9 24 3EAE LD A.'.'

OUTPUT "0 IF

29FB 26 FD770B LD <IY+B)»A INITIALIZE 1/ 29FE 29 CDDF28 CALL OUT* PROMPT OPERAT 2A01 2C DD7E02 CNTLO LD Af(IX+2) 2A04 2F DD7700 LB (IX+O)»A SET SCC TBE P 2A07 32 DD7E03 LD Ai(IX+3) TO TTY RDA PO 2A0A 35 DD7701 LD (IX+1)»A 2A0D 38 FD7E02 LO AF(IY+2) 2A10 3B FD7700 LD (IYtO).A SET TTY TBE P 2A13 3E FD7E03 LD Ai<IY+3) TO SCC RDA PO 2A16 41 FD7701 LD (IY+l)fA 2A19 44 3E00 LD A,00 INITIALIZE BY 2A1B 46 FD7710 LD (IY+10)FA 2A1E 49 FDCB0D86 RES OidY+D) RESET "Q ENAB 2A22 4D 3E11 LD A»"Q 2A24 4F 0E01 LD CiOl SEND SPC-16 T

193

2A26 51 CDDF28 CALL OUT« 2A29 54 CDC42C CALL EXIT* EN* 2A2C 57 C9 RET

StDCB *=2A2D

see RDA DEVICE CONTROL BLOCK ( DCB )

2A2D 0 0037 DU 3700 TBE POINTER 2A2F 2 0037 DU 3700 RDA POINTER 2A31 4 0037 DU 3700 BUFFER BEGINNING 2A33 6 0038 DU 3800 BUFFER ENDING 2A3S 8 01 DB 01 INPUT PORT 2A36 9 00 DB 00 INPUT DATA 2A37 A A1 DB A1 OUTPUT PORT 2A3S B 30 DB 30 OUTPUT DATA 2A39 C 00 DB 00 FREE FOR EXPANSION 2A3A D 00 DB 00 STATUS BYTE 2A3B E 10 DB 10 LOU BYTE COUNT 2A3C F FO DB FO HIGH BYTE COUNT 2A3H 10 00 DB 00 BUFFER BYTE COUNT 2A3E 11 01 DB "A 2A3F 12 80 DB 80 2A40 13 03 DB "C 2A41 14 05 DB "E 2A42 15 04 DB "D 2A43 16 02 DB "B 2A44 17 80 DB 80 2A4S 18 80 DB 80 2A46 19 80 DB 80 2A47 1A 80 DB 80 2A48 IB 80 DB 80 2A49 1C 10 DB "P 2A4A ID 05 DB ~E 2A4B IE 80 DB 80 2A4C IF 80 DB 80 2A4D 20 80 DB 80

ENABLE CHARAC

AfDCB *=2A4E

UART-A RDA DEVICE CONTROL BLOCK ( DCB )

2A4E 0 0036 DU 3600 2A50 2 0036 DU 3600 2A52 4 0036 DU 3600 2A54 6 0037 DU 3700 2A56 8 A1 DB A1 2A57 9 00 DB 00 2A58 A 01 DB 01 2A59 B 30 DB 30 2A5A C 00 DB 00 2A5B D 00 DB 00 2A5C E 00 DB 00 2A5D F 00 DB 00 2A5E 10 00 DB 00 2A5F 11 01 DB "A 2A60 12 OF DB "0 2A61 13 03 DB "C 2A62 14 04 DB "D 2A63 15 80 DB 80 2A64 16 02 DB "B 2A65 17 80 DB 80 2A66 18 80 DB 80 2A67 19 13 DB ~s 2A68 1A 11 DB "Q 2A&9 IB 7F DB <R0>

TBE POINTER RDA POINTER BUFFER BEGINNING BUFFER ENDING INPUT PORT INPUT DATA OUTPUT PORT OUTPUT DATA FREE FOR EXPANSION FREE FOR EXPANSION FREE FOR EXPANSION FREE FOR EXPANSION FREE FOR EXPANSION

194

2A6A 1C 10 DB -P 2A6B ID 05 DB 'E 2A6C IE 12 DB "R 2A6D IF 09 DB "I 2A6E 20 06 DB "F

BtDCB *=2A6F

UART-B RDA DEVICE CONTROL BLOCK ( DCB >

2A6F 0 0038 DU 3800 TBE POINTER 2A71 2 0038 DU 3800 RDA POINTER 2A73 4 0038 DU 3800 BUFFER BEGINNING 2A75 6 003E DU 3E00 BUFFER ENDING 2A77 8 B1 DB B1 INPUT PORT 2A78 9 00 DB 00 INPUT DATA 2A79 A B1 DB B1 OUTPUT PORT 2A7A B 80 DB 80 OUTPUT DATA 2A7B C 00 DB 00 RECORD COUNT 2A7C D 0032 DU 3200 T-6 POINTER 2A7E F 0032 DU 3200 T-15 POINTER 2A80 11 80 DB 80 2A81 12 80 DB 80 2A82 13 80 DB 80 2A83 14 BO DB 80 2A84 15 80 DB 80 2A85 16 24 DB INITIALIZE BUFFER 2A86 17 80 DB 80 2A87 18 80 DB 80 2A88 19 80 DB 80 2A89 1A 80 DB 80 2A8A IB 80 DB 80 2A8B 1C 80 DB 80 2A8C ID 80 DB 80 2ABD IE 80 DB 80 2A8E IF 80 DB 80 2A8F 20 3F DB '*** SHIP DATA TO SPC 16'

XtON *=2A90

BUFFER LOU BYTE COUNT CHECK

2A90 0 D03510 DEC tix+10) DECREMENT BYTE COUNT 2A93 3 DD7E0D LD Af(IX+D) GET STATUS BYTE 2A96 6 E601 AND AtOl CHECK ~Q ENABLE FLAG 2A9B 8 C8 RET Z 2A99 9 DD7E10 LD Ai(IX+10) GET BYTE COUNT 2A9C C DDBEOE CP (IX+E) B.C. - L.B. 2A9F F CO RET NZ RETURN IF B.C. <> L.B 2AA0 10 DDCB0D86 RES Oi(IX+D) RESET "Q ENABLE BIT 2AA4 14 3E11 LD A.-Q OUTPUT "0 TO SPC 2AA6 16 D301 OUT A>(01) 2AA8 18 C9 RET

XJOFF *=2AA9

BUFFER HIGH BYTE COUNT CHECK

2AA9 0 DD7E08 LD A»(IX+8) CHECK FOR SPC INPUT 2AAC 3 FE01 CP 01 2AAE 5 CO RET NZ IF NOT SPC. RETURN 2AAF 6 DD3410 INC

NZ (IX+10) INCREMENT BYTE COUNT

2AB2 9 A7 AND A>A CLEAR CARRY FLAG 2AB3 A DD7E10 LD AF (IX+10)

195

2AB6 B BDBEOF CP (IX+F) B.C. - H.B. 2AB9 10 D8 RET C IF B.C.' < H.B. 2ABA 11 DDCB0DC6 SET 0>(IX+D) SET "Q ENABLE BIT 2ABE 15 3E13 LD Ar-S SEND "S TO SPC 16 2AC0 17 D301 OUT A.(01)

SEND "S TO SPC 16

2AC2 19 C9 RET

DtTIHR *=2AC3

DRIVER FOR TIMER INTERRUPT SERVICE

2AC3 0 DD4E00 LD Ci(IX+0> GET TIMER PORT 2AC6 3 DD7E01 LD At(IX+1) GET TIMER LOAD COUNT 2AC9 6 E079 OUT (C) i A RESTART TIMER 2ACB 8 DD7E02 LD Ai(IX+2) UPDATE INDEX 1 2ACE B 3D DEC A 2ACF C DD7702 LD (IX+2).A 2AB2 F CO RET NZ 2AD3 10 DD7E03 LD Ai(IX+3) RESET INDEX 1 2AD6 13 DD7702 LD (IX+2)rA 2AD9 16 DD7E04 LD Ai(IX+4) UPDATE INDEX 2 2ADC 19 3D DEC A

UPDATE INDEX 2

2ADD 1A DD7704 LD (IX+4)i A 2AE0 ID CO RET NZ 2AE1 IE DD7E05 LD Ai(IX+5) RESET INDEX 2 2AE4 21 DD7704 LD (IX+4)iA

RESET INDEX 2

2AE7 24 DDCB0646 BIT Of(IX+6) TEST FOR HANDLER SERV 2AEB 28 C8 RET Z

TEST FOR HANDLER SERV

2AEC 29 C3EF2A JP H$TIMR

H*TIMR *=2AEF

HANDLER FOR TIHER INTERRUPT SERVICE

2AEF 0 79 LD AiC 2AF0 1 FEA5 CP AS 2AF2 3 CA002B JP Z A1»TIH SERVICE DEV-A TIMER 1 2AF5 A FEA6 CP A6

SERVICE DEV-A TIMER 1

2AF7 8 CA232B JP Z A2STIH SERVICE DEV-A TIMER 2 2AFA B FEA7 CP A7


2AFC D CA6F2B JP Z A3ITIM SERVICE DEV-A TIMER 3 2AFF 10 C9 RET


A1ITIM *=2B00

HANDLER FOR 1 MINUTE BUFFER SERVICE

2B00 0 DD7E07 LD At(IX+7) 2B03 3 3D DEC A CHECK FOR FULL BUFFER 2B04 4 DD7707 LD (IX+7) »A

CHECK FOR FULL BUFFER 2B07 7 2009 JR NZ TIME1 2B09 9 CDBF2B CALL B*FULL 2B0C C DD7E08 LD Ai(IX+8) RESET BUFFER COUNTER 2B0F F DD7707 LD (IX+7).A 2B12 12 FD2A8026 TIHE1 LD IY»(TtPUT+12) MUX TIHER DCB 2B16 16 FB4E00 LD Cf(IY+O) GET TIMER PORT 2B19 19 FD7E01 LD Ai(IY+1) GET LOAD COUNT 2B1C 1C ED79 OUT (C)iA

GET LOAD COUNT

2B1E IE FDCB06C6 SET Oi(IY+6) ENABLE HUX HANDLER 2B22 22 C9 RET

ENABLE HUX HANDLER

A2*TIM *=2B23

196

HANDLER FOR HUX TIMER INTERRUPTS

2B23 0 DDCB0686 RES Oi (IX+6) DISABLE MUX SERVICE 2B27 4 FD2A8426 LD IYf(T*PUT+16) GET A/D TIHER DCB 2B2B 8 DD7E07 LD A»(IX+7) 2B2E B DDBE08 CP (IX+8) CHECK FOR END OF SET 2B31 E 201E JR NZ NEXT 2B33 10 FD6E0B LD L.(IY+B) RESET BUFFER POINTER 2B36 13 FD660C LD H»(IY+C) 2B39 16 FD7509 LD (IY+9) fL 2B3C 19 FD740A LD (IY+A)fH 2B3F 1C DD4E09 LD Cr <IX+9) GET MUX PORT 2B42 IF 21902C LD HLfT»MUX GET CONTROL BYTE 2B45 22 7E LD A.(HL) 2B46 23 ED79 OUT (C) > A OUTPUT MUX CONTROL BY 2B48 25 DD770B LD < IX-f-B> > A SAVE A/D CONTROL BYTE 2B4B 28 3E00 LD AfOO 2B4D 2A DD7707 LD (IX+7)»A INITIALIZE CONTROL CO 2B50 2D C9 RET 2B51 2E DD3407 NEXT INC (IX+7) UPDATE SET COUNTER 2B54 31 DD4E0A LD Cf(IX+A) GET A/D OUTPUT PORT 2B57 34 DD7E0B LD A.(IX+B) GET A/D CONVERT BYTE 2B5A 37 CBF7 SET 6.A A/D CONVERT SET 2B5C 39 ED79 OUT (C) iA PULSE A/D 2B5E 3B CBB7 RES 6» A A/D CONVERT RESET 2B60 3D ED79 OUT (C) >A PULSE A/D 2B62 3F FD4E00 LD CF(IY+0) A/D TIHER PORT 2B65 42 FD7E01 LD Af (IY+l) GET TIHER LOAD COUNT 2B68 45 ED79 OUT (C).A START TIMER 2B6A 47 FDCB06C6 SET Of (IY+6) ENABLE A/D SERVICE 2B6E 4B C9 RET

A3*TIH *=2B6F

HANDLER FOR A/D TIMER INTERRUPTS

2B6F 0 DDCB0686 RES 0»(IX+6) DISABLE A/D 2B73 4 DD6E09 LD L»(IX+9) GET BUFFER POINTER 2B76 7 DD660A LD Hf(IX+A) 2B79 A DD4E0F LD C»(IX+F) A/D INPUT PORT LOU 2B7C D ED78 IN A> (C) GET LOU BYTE 2B7E F BF CP A CLEAR CARRY FLAG 2B7F 10 8E ADC Ar(HL) SUH CURRENT VALUE 2B80 11 77 LD (HL)fA SAVE SUH LOU 2B81 12 DD4E10 LD Cf(IX+10) A/D INPUT PORT HIGH 2B84 15 23 INC HL HIGH BYTE OF SUM 2B85 16 3E00 LD AfOO 2B87 18 8E ADC Af (HL) ADD CARRY PRIOR TO HA 2B8B 19 77 LD (HL)fA 2B89 1A ED78 IN Af (C) GET HIGH BYTE 2B8B 1C E60F AND OF HASK OFF HIGH ORDER B 2B8D IE 8E ADC Af(HL) SUM CURRENT VALUE 2B8E IF 77 LD (HL)fA SAVE SUH HIGH 2B8F 20 23 INC HL UPDATE POINTER 2B90 21 DD7509 LD (IX+9)fL SAVE BUFFER POINTER 2B93 24 DD740A LD (IX+A)fH 2B96 27 FD2A8026 LD IY f(T*PUT+12) MUX TIMER DCB 2B9A 2B FD3407 INC (IY+7) BUMP BUFFER COUNTER 2B9D 2E FD7E07 LD At(IY+7) 2BA0 31 CB3F SRL A 2BA2 33 5F LD Et A COMPUTE INDEXED hUX-A 2BA3 34 1600 LD Df 00 CONTROL BYTE ADDRESS 2BA5 36 21902C LD HLfTtMUX 2BA8 39 19 ADD HLfDE

GET MUX OUTPUT PORT 2BA9 3A FD4E09 LD Cf (IY+9) GET MUX OUTPUT PORT 2BAC 3D 7E LD Af(HL) GET HUX CHANNEL 2BAD 3E ED79 OUT (C) f A SELECT HUX CHANNEL

198

2C2C 2C2E 2C2F 2C32 2C34 2C37 2C3A 2C3D 2C40 2C43 2C46 2C47 2C48 2C4B 2C4D 2C4E 2C51 2C53 2C56 2C59 2C5C 2C5F

6D 200C JR NZ Til 6F 7C LD AiH 70 DDBE12 CP (IX+12) 73 2006 JR NZ Til 75 DD6E0F LD Li(IX+F) 78 DD6610 LD Hi<IX+10) 7B DD7S0D Til LD (IX+D)iL 7E DD740E LD (IX+E)»H 81 DD6E09 LD Lr(IX+9) 84 DD660A LD Hi(IX+A) 87 09 ADD HLiBC 88 7D LD A.L 89 DDBE11 CP (iX+11) 8C 200C JR NZ TO 8E 7C LD AiH 8F DDBE12 CP UX+12) 92 2006 JR NZ TO 94 DD6E0F LD Li(IX+F) 97 DD6610 LD HI(IX+10) 9A DD7509 TO LD (IX+9) iL 9D DD740A LD (IX+A)iH AO C9 RET

(IX+A)iH

CHECK BUFFER ENDING H

RESET POINTER TO BEGI

SAVE CURRENT POINTER

UPDATE T-l POINTER

CHECK BUFFER ENDING L

CHECK BUFFER ENDING H

RESET POINTER TO BEGI

SAVE CURRENT POINTER

A1*DCB *=2C60

TUART TIHER-A1 DEVICE CONTROL BLOCK

2C60 0 AS DB A5 2C61 1 F1 DB F1 2C62 2 01 DB 01 2C63 3 F2 DB F2 2C64 4 01 DB 01 2C65 S 01 DB 01 2C66 6 01 DB 01 2C67 7 01 DB 01 2C68 8 10 DB 10 2C69 9 0031 DU 3100 2C6B B 2034 DU 3420 2C6D D 5031 DU 3150 2C6F F 0031 DU 3100 2C71 11 0036 DU 3600

TIHER PORT TIMER LOAD COUNT INDEX 1 INDEX 1 LOAD COUNT INDEX 2 INDEX 2 LOAD COUNT HANDLER STATUS INDEX 3 INDEX 3 LOAD COUNT BUFFER POINTER T-l BUFFER POINTER T-6 BUFFER POINTER T-15 BUFFER BEGINNING BUFFER ENDING

A2IDCB *=2C73

TUART TIHER-A2 DEVICE CONTROL BLOCK

2C73 0 A6 DB A6 2C74 1 80 DB 80 2C75 2 01 DB 01 2C76 3 01 DB 01 2C77 4 01 DB 01 2C78 5 01 DB 01 2C79 6 00 DB 00 2C7A 7 00 DB 00 2C7B 8 50 DB 50 2C7C 9 OA DB OA 2C7D A OA DB OA 2C7E B 00 DB 00

TIMER PORT TIMER LOAD COUNT INDEX 1 INDEX 1 LOAD COUNT INDEX 2 INDEX 2 LOAD COUNT HANDLER STATUS INDEX Z NUMBER OF CHANNELS MUX OUTPUT PORT A/D OUTPUT PORT A/D CONVERT BYTE

* 2

A3*DCB *=2C7F

2C7F

TUART TIMER-A3 DEVICE CONTROL BLOCK

0 A7 DB A7 TIMER PORT

197

2BAF 40 FD770B ID (IY+B)»A A/D CONVERT BYTE 2BB2 43 FD4E00 LD Cr(IY+O) MUX TIMER PORT 2BB5 46 FD7E01 LD Af(IY+1) MUX TIMER PORT LOAD 2BB8 49 ED79 OUT (C)»A START MUX TIMER 2BBA 4B FDCB06C6 SET 0» (IY+6) ENABLE HUX SERVICE 2BBE 4F C9 RET

B$FULL *=2BBF

UPDATES 16 HINUTE BUFFER AND INITIALIZES 1 MINUTE BUFFER

2BBF 0 FD2A8026 LD IY<(TIPUT+12) MUX TIHER BCB 2BC3 4 FD7E08 LD A.UY+8) GET NUMBER OF 2BC6 7 4F LD CrA CHANNELS*2 2BC7 B CB3F SRL A DIVIDE BY TUO 2BC9 A FD2A8426 LD IY.(T»PUT+16) A/D TIHER DCB 2BCD E FD6E0B LD Lf(IY+B) 2BD0 11 FD660C LD Hf(IY+C) 2BD3 14 5E DIV16 LD E.(HL) 2BH4 15 23 INC HL 2BD5 16 56 LD D>(HL) 2BD6 17 2B DEC HL 2BD7 18 CB3A SRL D 2BD9 1A CB1B RR E DIVIDE CONTENTS OF 2BDB 1C CB3A SRL D REGISTER PAIR DE 2BDD IE CB1B RR E BY SIXTEEN 2BDF 20 CB3A SRL D 2BE1 22 CB1B RR E 2BE3 24 CB3A SRL D 2BE5 26 CB1B RR E 2BE7 28 3001 JR NC RNDDUN 2BE9 2A 13 IMC DE ROUND UP QUOTIENT 2BEA 2B 73 RNDDUN LD (HL)fE SAVE RESULT IN BUFFER 2BEB 2C 23 INC HL 2BEC 2D 72 LD (HL)»D 2BED 2E 23 INC HL

CHECK FOR END OF SET 2BEE 2F 3D DEC A CHECK FOR END OF SET 2BEF 30 20E2 JR NZ DIV16 2BF1 . 32 41 UPDATE LD BrC 2BF2 33 DD5E0B LD Er(IX+B) BLOCK DESTINATION 2BF5 36 DD560C LD Dr(IX+C) 2BF8 39 FD6E0B LD L»(IY+B) BLOCK SOURCE 2BFB 3C FD660C LD H»(IY+C) 2BFE 3F 7E NEXT LD At(HL) BLOCK TRANSFER 2BFF 40 12 LD (DE)rA 2C00 41 3600 LB (HL)»00 INITIALIZE SUM TO ZER 2C02 43 23 INC HL 2C03 44 13 INC DE BUMP POINTERS 2C04 45 7B LD AtB INITIALIZE BLOCK COU 2C05 46 3D DEC A DECREMENT BLOCK 2C06 47 47 LD Br A SAVE A IN B 2C07 48 20F5 JR NZ NEXT 2C09 4A 7B LD A»E UPDATE T-6 POINTER 2C0A 4B DDBE11 CP (IX+11) CHECK BUFFER ENDING L 2C0D 4E 200C JR NZ T15 2C0F 50 7A LD AiD 2C10 51 DDBE12 CP (IX+12) CHECK BUFFER ENDING H 2C13 54 2006 JR NZ T15 2C15 56 DD5E0F LD E»(IX+F) RESET POINTER TO BEGI 2C18 59 DD5610 LD Df(IX+10) 2C1B 5C DD730B T15 LD (IX+B)»E SAVE CURRENT POINTER 2C1E 5F DD720C LD (IX+C)iD 2C21 62 DD6E0D LB L»(IX+D) UPDATE T-15 POINTER 2C24 65 DD660E LD H»(IX+E) 2C27 68 09 ADD HLrBC 2C2B 69 7D LD A>L 2C29 6A DDBE11 CP (IX+11) CHECK BUFFER ENDING L

2C80 1 80 DB 80 TIMER LOAD COUNT 2C81 2 01 DB 01 INDEX 1 2C82 3 01 DB 01 INDEX 1 LOAD COUNT 2C83 4 01 DB 01 INDEX 2 2C84 5 01 DB 01 INDEX 2 LOAD COUNT 2C85 6 00 DB 00 HANDLER STATUS 2C86 7 00 DB 00 INDEX 3 2C87 8 00 DB 00 INDEX 3 LOAD COUNT 2C88 9 B030 DU 30B0 BUFFER POINTER 2C8A B B030 DU 30B0 BUFFER BEGINNING 2C8C D 0031 DU 3100 BUFFER ENDING 2C8E F OA DB OA A/D INPUT PORT LOU 2C8F 10 OB DB OB A/D INPUT PORT HIGH

TIMUX *=2C90

TABLE OF MULTIPLEXOR CONTROL BYTES

2C90 0 00 DB 00 2C91 1 01 DB 01 2C92 2 02 DB 02 2C93 3 03 DB 03 2C94 4 04 DB 04 2C95 5 05 DB 05 2C96 6 06 DB 06 2C97 7 07 DB 07 TRACE CHANNEL 2C98 8 08 DB 08 2C99 9 09 DB 09 2C9A A OA DB OA 2C9B B OB DB OB 2C9C C OC DB OC 2C9D D OD DB OD 2C9E E OE DB OE 2C9F . F OF DB OF TRACE CHANNEL 2CA0 10 10 DB 10 2CA1 U 11 DB 11 2CA2 12 12 DB 12 2CA3 13 13 DB 13 2CA4 14 14 DB 14 2CA5 15 15 DB 15 2CA6 16 16 DB 16

TRACE CHANNEL 2CA7 17 17 DB 17 TRACE CHANNEL 2CA8 18 18 DB 18 TRANSPORT AIR 2CA9 19 19 DB 19 SECONDARY AIR 2CAA 1A 1A DB 1A STAGED AIR 2CAB IB IB DB IB C02 ANALYZER 2CAC 1C 1C DB 1C CO ANALYZER 2CAD ID ID DB ID 02 ANALYZER 2CAE IE IE DB IE NO ANALYZER 2CAF IF IF DB IF TRACE CHANNEL 2CB0 20 20 DB 20 2CB1 21 21 DB 21 2CB2 22 22 DB 22 2CB3 23 23 DB 23 2CB4 24 24 DB 24 2CB5 25 25 DB 25 2CB6 26 26 DB 26 2CB7 27 27 DB 27 TRACE CHANNEL

ENTRY* *=2CB8

DISABLE CHARACTER SERVICE f ENABLE TIMERS

2CB8 0 F5 PUSH AF SAVE AF 2CB9 1 3EOO LD A>00 2CBB 3 D303 OUT (03>rA MASK OUT SCC UART

200

2CBD 5 3E0B LD AiOB 2CBF 7 D3A3 OUT (A3)rA MASK OUT DEV-A UART 2CC1 9 F1 POP AF 2CC2 A FB EI ENABLE INTERRUPTS 2CC3 B C9 RET

EXIT* *=2CC4

ENABLE CHARACTER SERVICE t ENABLE TIMERS

2CC4 0 F3 DI DISABLE INTERRUPTS 2CCS 1 F5 PUSH AF 2CC6 2 3E30 LD A >30

MASK FOR SCC UART 2CC8 4 D303 OUT (03)>A MASK FOR SCC UART 2CCA 6 3E3B LD A»3B 2CCC 8 D3A3 OUT <A3)fA MASK FOR DEV-A UART 2CCE A F1 POP AF 2CCF B C9 RET

DUMP* *=2CD0

SEND T-l i T-6 AND T-15 BUFFERS TO REQUESTING PORT

2CD0 0 DD7E08 LD A.QX+8) GET REQUESTING PORT N 2CD3 3 FEB1 CP B1 2CD5 S C8 RET Z IGNORE IF CHROKATOGRA 2CD6 6 FD2A7E26 LD IYf(T*PUT+10) GET MINUTE TIMER DCB 2CBA A FDCB0686 RES 0»(IY+6) DISABLE MINUTE BUFFER 2CDE E CDB82C CALL ENTRY* ENABLE TIMERS/DISABLE 2CE1 11 DD4E08 LD C»(IX+8> GET REQUESTING PORT N 2CE4 14 DD2A9626 LD IXi (T*PUT+28) GET CHROMATOGRAPH DCB 2CE8 18 FD6E09 LD LrtIY+9) 2CEB IB FD660A LD H»(IY+A) 2CEE IE CD0B2D CALL WRITE* SEND T-l BUFFER 2CF1 21 DD6E0D LD Li<IY+D) 2CF4 24 DD660E LD Hr(IY+E) 2CF7 27 CD0B2D CALL WRITE* SEND T-6 BUFFER 2CFA 2A DD6E0F LD Li(IY+F) 2CFD 2D DD6610 LD Hi(IY+10) 2D00 30 CD0B2D CALL WRITE* SEND T-15 BUFFER 2D03 33 CDC42C CALL EXIT* ENABLE CHARACTER SERV 2D06 36 FDCB06C6 SET Or(IY+6) ENABLE MINUTE BUFFER 2B0A 3ft C9 RET

WRITE* *=2D0B

ROUTINE TO TRANSMIT 2 HALF RECORDS

2D0B 0 1E02 LD Ei02 NUMBER OF RECORDS TO 2D0D 2 1614 NXTREC LD Di 14 NUHBER OF WORDS PER R 2D0F 4 CD2229 CALL SHAKE* 2IU2 7 46 NXTBYT LD Bi(HL) GET LOW BYTE 2IU3 8 23 INC HL 2D14 9 7E LD Af(HL) GET HIGH BYTE 2D IS A 23 INC HL 2D16 B CD2B2D CALL P2*HEX PRINT HIGH BYTE 2B19 E 78 LD ArB 2D1A F CD2B2D CALL P2*HEX PRINT LOU BYTE 2D1D 12 7A LD Af D 2D1E 13 3D DEC A UPDATE UORD COUNTER 2D1F 14 57 LD Df A 2D20 15 2OF0 JR NZ NXTBYT 2D22 17 CD2A29 CALL CR* 2D25 1A 7B LD Af E

201

2D26 IB 3D DEC A UPDATE RECORD COUNTER 2D27 1C 5F LD ErA 2D28- ID 20E3 JR NZ NXTREC END OF TRANSMISSION 2D2A IF C9 RET

P2*HEX »=2D2B

PRINTS CONTENTS OF A-REGISTER AS TUO HEX DIGITS

2D2B 0 CD2F2D CALL P1HEX PRINT HIGH NIBBLE 2D2E 3 IF RRA PRINT LOU NIBBLE 2D2F 4 IF P1HEX RRA 2D30 5 IF RRA SUAP NIBBLES 2Ii 31 6 IF RRA 2D32 7 IF RRA 2D33 8 F5 PUSH AF SAVE AF 2D34 9 E60F AND OF MASK OFF DIGIT 2036 B FEOA CP OA 2D38 D 3802 JR C PHI 2D3A F C607 ADD 07 A THROUGH F 2D3C 11 C630 PHI ADD 30 ASCII BIAS 2D3E 13 CDDF28 CALL OUTS PRINT CHARACTER 2D41 16 F1 POP AF 2042 17 C9 RET

REFERENCE MAP

CHKSUH 42 2500 SETUP 65 252A HtlSR 128 25CC SARS* 17 264C LARSt 17 265D T$PUT 48 266E TtlSR 97 256B DtRDA 63 269E D$TBE 64 26DD H*RDA 196 2764 H*TBE 71 271D HSDPLX 20 2828 HIINPT 25 296E OtCHK 33 294D ITIMAP 14 2R.1C SHAKE* 8 2922 CRt 6 292A CIDUHP 149 284A OUT* 9 28DF C*DEL 47 28E8 ••DONE: 11 2917 P«HSG 29 2930 GOSSCC 25 2987 T $MSG 40 29AD GETCH* 13 29A0 CNTLSO 88 29D5 SSDCB 33 2A2D AtDCB 33 2A4E BtDCB 33 2A6F XtON 25 2A90 XIOFF 26 2AA9 DITIMR 44 2AC3 HITIMR 17 2AEF A1*TIM 35 2B00 A2»TIM 76 2B23 A3*TIM 80 2B6F B$FULL 161 2BBF AltDCB 19 2C60

202

A2*BCB A3*DCB TSMUX ENTRYi EXIT* DUMP* URITE* P2*HEX

12 2C73 17 2C7F 40 2C90 12 2CB8 12 2CC4 59 2CD0 32 2D0B 24 2D2B

203

REFERENCES

1. Anscombe, F. J., "Rejection of Outliers,11 Technometrics, Vol. 2, No. 2, pp. 123-147, May, 1960 .

2. Carnahan, B., H. A. Luther and J. 0. Wilkes, Applied Numerical Methods, John Wiley and Sons, Inc., New York, 1969.

3. Davidson, E. R. and G. P. Christian, "Quantitative Analysis of Multicomponent Fluorescence Using the Methods of Least Squares and Non-Negative Sum of Errors," Analytical Chemistry, Vol. 49, No. 14, Dec., 1977.

4. Glass, J. W., Private Conversation, Dept. of Chemical Engineering, University of Arizona, 1980.

5. Glass, J. W. and J. 0. L. Wendt, Combustion Research and Air Pollution Colloquia, Chem. Eng., University of Arizona, Fall, 1980.

6. Glass, J. W., "Influence of Coal Combustion on the Fate of Coal Nitrogen During Staged Combustion," M. S. Thesis, University of Arizona, 1978.

7. Himmelblau, D. M., Process Analysis by Statistical Methods, John Wiley and Sons, Inc. , New York, l"969.

8. Hockings, W. A. and R. W. Cullen, "Computer Program for Calculating Mass Flow Balances of Continuous Process Streams," SME/AIME Preprint 77-B-372, Oct., 1977.

9. Kuester, J. L. and J. H. Mize, Optimization Techniques with FORTRAN, McGraw Hill, New York, 1973.

10. Pearson, E. S. and H. 0. Hartley, Biometrika Tables for Statisticians, Vol. 1, pp. 32-33, Cambridge, 1954.

11. Smith, H. W. and N. M. Ichiyen, "Computer Adjustment of Metallurgical Balances," Can. Mln. and Met. Bull., pp. 97-100, Sep., 1973.

12. "Student", "Errors of Routine Analysis," Biometrika, Vol. 19, pp. 151-164, 1927.

204

13. Takacs, L. , "Improving the Efficiency of Industrial Boilers by Microprocessor Control," Power Eng., pp. 80-83, Nov., 1977.

14. Wendt, J. 0. L., Private Conversation, Dept. of Chemical Engineering, University of Arizona, 1981.

15. Wendt, J. 0. L. and J. W. Glass, Topical Report No. 1, "Pollutant Control Through Staged Combustion of Pulverized Coal," U.S. Dept. of Energy, Contract DE-AC01-79ET-15184, May, 1979-

16. Wendt, J. 0. L., "Advanced Staged Combustion Configurations for Pulverized Coal," Proposal for Research Renewal of Contract DE-AC01-79ET-15184, Dept. of Chem. Eng., University of Arizona, Aug., 1977.

17. White, J. W. and R. L. Winslow, "Flowsheet Analysis for Mass Balance Calculations in Overdefined Metallurgical Systems with Recycle," SME/AIME Preprint No. 79-80, Feb., 1979.

18. White, J. W., R. L. Winslow and G. J. Rossiter, "A Useful Technique for Metallurgical Mass Balances -Applications in Grinding," Int'l J. Min'l Proc., Vol. 4, pp. 39-49, 1977.

19. Whiten, W. J., "Model Building Techniques for Mineral-Treatment Process," Symp. on Auto. Control Sys. in Min'l Proc. Plants, Tech. Papers, Brisbane, pp. 129-148, May, 1971.

20. Wiegel, R. L., "Advances in Mineral Processing Material Balances," Can. Met. Quart., Vol. 71, No. 2, pp. 412-424, 1972.

21. Winslow, R. L., "A Systems Approach to Analysis of Industrial Wet Grinding Circuit Data," M. S. Thesis, University of Arizona, 1980.

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