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UnderSea Solutions, Inc.
Arctic AUV Proposal
OCE 4542
12/8/00
Team Members:
Ryan Roberts Nicky Samuelson
Chris Duer Adam Kay
Instructor:
Dr. Stephen Wood
1
Introduction
This project entails the conceptual design and analysis of an AUV, Autonomous
Underwater Vehicle, for Arctic under-ice water sampling. As such, the primary goals of the
project are twofold: to apply engineering principles to real world design, and to work
cooperatively in a team that approximates the organization by which design is carried out in real
world situations.
In order to properly organize the design project, a company was created called UnderSea
Solutions, Inc. A complete company hierarchy was created to differentiate different systems in
the project and thus maintain clarity throughout the project. The company hierarchy is shown
below.
Chief Executive Officer
Ryan Roberts
Mechanical Engineer Electrical Engineer Computer Engineer
Nicky Samuelson Chris Duer Adam Kay
The three main company divisions are each tasked with several components of the overall
AUV design. These are as follows:
Mechanical Design:
? Hull Design
? Materials Standards & Testing
? Maneuverability/Control
? Layout & Arrangement
? Deployment & Retrieval Mechanisms
Electrical Design:
? Power Consumption
? Battery Requirements & Selection
? Thrust Motor Requirements & Selection
? Control Plane Motor Selection
2
Computer Design and Instrumentation:
? Command & Control Systems
? Navigation Sonar & Collision Avoidance
? Instrumentation & Sensing
? Data Acquisition, Storage & Retrieval
Design Parameters & Requirements
The basic design criteria are imposed by the environment in which the AUV will be used,
the requirements of the operators and the overall ease with which the AUV may be operated.
Mission Statement:
The Arctic AUV will be used for under-ice water sampling in Alaska’s coastal waters.
Turbidity measurements will be made at known relative and absolute points along the
AUV’s survey track. The AUV must be functional in a harsh marine environment, user
friendly with respect to data collection and retrieval and easily stowed, deployed and
retrieved.
Environmental Characteristics
? 0o to –40o C Air Temperature
? 5o to –5o C Water Temperature
? Low to Moderate Currents (0.5 knot maximum)
? 40 ft. maximum water depth
? 6 ft. ice cap
3
AUV Requirements
? Light Weight
? Deployable through a 15 inch diameter hole
? Variable Speed Capability
? Capable of navigating under ice field and returning to deployment point
? Collect water quality data with corresponding locations
? Distinguish sonar signals (Collision Avoidance)
? Cruising Speed: 2 kts.
? Maximum Speed: 20 kts.
? 5 hours endurance at cruise speed
Required Instrumentation
? Nephelometer
? CTD
? Camera
? Turbidity instrument
Main Design Points
? Design for Assembly and Disassembly
? Design for serviceability and multiple reuse
? Design for Interchangeability and modularity
? Commonality between computer components
Mechanical Design
We are focused on producing an innovative product, which is simple, reliable and
manufactured to the highest standards.
The Artic water sampler is a small, compact, extremely capable, high performance
professional AUV system, which can be used for a variety of underwater tasks such as water
sampling, survey and observation, etc.
4
Performance/Dimension
Depth Rating: 33 meters standard 100 feet
Dimensions:
Length 1.12 m 7 feet
Outer radius 15.5 mm 6"
Thickness 6.3 mm 0.25"
Maximum Velocity/Operational Current:
Maximum velocity 20 Kt
Standard cruise 2 Kt
Housing
The Artic water sampler housing is constructed of Aluminum incorporating the following
features:
Aluminum housing with low temperature resistant O-ring seals
Acrylic dome for nose cone
Lift points
Hull Form
The hydrodynamic form of the AUV determines the propulsion energy required, as well
as the stability and maneuverability at various operating speeds. A hull form may also impose
limitations on vehicle access, launch and recovery, and maintenance.
5
The speed for the AUV is between ½ and 20 knots. In most applications, the vehicle will
maintain a steady cruising speed of 2 knots throughout the mission. The following considerations
drive the selection of the hull form:
? Minimization of overall vehicle drag
? Minimization of flow separation, especially for efficient propulsion near the tail
? Stability as a sensor platform at 2 knots
? Stability and maneuverability at speeds as low as ½ knots
Longer, more slender shapes tend to be better. We have chosen the torpedo hull form
because of its many advantages
? Streamline shape for low resistance and high ability to store lots of equipment
? Maneuverability
? Small diameter (needed to launch and recover the vehicle through the ice)
Equipment layout and arrangement
Front Bulb Collision Avoidance Sonar Array
Industry Standard Camera with RCA video output
2 Lights (20 Watt halogens)
Mid-compartment 1 Data Storage
Command and Controls
Mid-compartment 2 Batteries
Aft compartment Watertight Fin Servos
Aft External Thrust Motor
6
Figure 1: Equipment layout and arrangement
Maneuverability and Control:
The Artic water sampler has six fins for stability maneuverability:
? Two forward fixed fins for stability
? Four controllable fixed fins for maneuverability:
o Two rudder
o Two driving planes
The aft fins are controlled by watertight heavy duty professional Series Tone Servos
SSPS-105.
PVC Flexural Tests
The flexural test on PVC, Polyvinyl Chloride, measures the deflection of a 6” inside
diameter Schedule 40 pipe length. An idea of the elasticity of this material and its applicability
as a pressure vessel may partially be obtained from this test. The maximum loading before
rupture may also be determined.
The apparatus for testing the PVC pipe is as follows:
7
? Digital Extensiometer
? End supports
? Duct tape
? Loads: batteries and dive weights
? Scale
PVC Pipe
Pipe Support
Figure 2: PVC End Support
Load
Dial GageSupport
PVC Pipe
Figure 3: PVC Flexural Test Apparatus
Procedure
The following steps outline the procedure for the flexural testing of PVC pipe.
8
1. Place two tables approximately 5 feet apart.
2. Fix supports on each inside edge of table.
3. Place PVC pipe on supports ensuring that both ends have the same contact surface area.
4. Using bookshelves and books as sheaves, place extensiometer at mid-span, with plunger
depressed approximately halfway.
5. Reset the readout to zero and ensure that the reading will give a positive answer as the
plunger is allowed to come out.
6. Weigh and record the masses of the batteries and dive weights.
7. Place each load as close to the center as possible, one at a time.
8. Record the deflection of the pipe.
9. Repeat procedure until failure occurs or until all weights have been used.
Results
Weight
(lb)
4 8 12 16 20 26 32 40.9 49.9 58.8 67.7 76.7
Deflecti
on (in)
0.002
4
0.008
7
0.01
5
0.022
2
0.028
5
0.03
8
0.048
7
0.066
2
0.08
2
0.095
7
0.106
2
0.115
4
Table 1: 1st Trial Results
Weight
(lb)
9 17.9 26.8 35.7 44.7 58.7 72.7
Deflection
(in)
0.015 0.0306 0.0441 0.0589 0.073 0.087 0.1055
Table 2: 2nd Trial Results
Battery # 1 2 3 4 5
Weight (lb) 8.9 9.0 8.9 8.9 9.0
Table 3: Battery Weights
9
Deflection Vs. Load
0102030405060708090
0 0.02 0.04 0.06 0.08 0.1 0.12 0.14
Deflection (in)
Load
(lb)
1st Trial2nd Trial
Figure 4: Results Plot
PVC Destructive Impact Tests
For the impact test on PVC we will be performing a destructive impact test (or simple
beam test). This test will be performed on a 1 foot long, 6” inside diameter Schedule 40 pipe at
room temperature and at -70?C.
Results:
PVC Failure
Room temperature Never
-70?C 110 ft/lb
-50?C Never
-70?C 75 ft/lb
-60?C 110 ft/lb
Table 4. Impact Test Results
The variation in the results from the five tests were a function of the time that the PVC
was allowed to cool. The PVC that failed with the lowest applied force was the specimen that
was allowed to cool the shortest amount of time. In the third trial, the specimen did not fail.
This was because the specimen cooled for too long, almost to room temperature.
10
We ultimately decided not to use the PVC because of the possibility of brittle fracture
and because of the great deflection when the specimen did not fracture. The PVC specimens
deformed enough that the seals of the AUV would leak.
Electrical Design
The electrical design for the AUV is composed of 5 individual systems. These systems
are the thrust motor, control plane motors control systems, navigation system and
instrumentation.
Thrust Motor
The thrust motor is manufactured by Minn Kota. The Riptide Saltwater Bow-Mount
Motor RT65/AP was chosen for its thrust to amp draw to voltage ratio of 65 lb:38 Amp/hr:12 V,
which was the best of all motors surveyed.
Control Plane Motor
The control plane motor used is a CK Design Technology Heavy Duty Professional
Series Tone Servo SSPS-105. This motor requires an average of 1 amp/hr.
Control system, Navigation System and Instrumentation
The computer systems, described in the Computer Design section require only a minimal
amount of amp draw. The total draw is 5280 mA, or approximately 5 Amp/hr. The following
table is a breakdown of the draw for each individual computer component.
Computer Component Controls
Amp Draw
(mA)
2 PC/104 Boards brain/navigation/instrumentation/collision 1400
Relay Board on/off 250
11
ADC & DCA 480
Video Capture camera 350
Motor Controller x3 thrusters & fin servos 1050
Signal Processor transducers (navigation & collision) 150
Matrix Keypad & LCD command entry & display 100
Hard Drive video & data storage 1500
Total 5280
~5Amp/hr
Total Amp Draw
The total Amp/hour draw of the AUV is laid out in the following table.
Item Amp Draw
Computer Equipment 5 Amp/hr
Thruster Motor 38 Amp/hr
Control Plane Motor x2 1 Amp/hr
Total 45 Amp/hr
Battery Requirement
The AUV will house four 12V batteries and have four more on reserve to be changed out
between each run. This decreases turnaround time between each run. The batteries are each 12
volt 30 Amp batteries.
Computer Design and Instrumentation
System Requirements
In order for the Arctic AUV to perform its mission of transporting scientific
instrumentation from one point to another under the ice, it must be able to control its thrust motor
and fins, find its way from the start to finish and back, and avoid obstacles along the way. All of
these, along with storage of the scientific data are handled by the computer systems on board the
12
vehicle. The Arctic AUV contains two separate computer systems. The first is the main control
system, which is responsible for getting the payload from start to finish and back. The second
system is the data logger for the scientific instrumentation, including the storage of pictures
taken with the onboard camera.
Main Control System
The main control system handles the navigation (getting the vehicle from start to finish
and back), collision avoidance (avoiding obstacles along the way), and motor control (changing
and storing thruster speed and fin position). This system is centered around a high-power
PC/104 form-factor single board computer that will simultaneously run 4 mission programs in a
real-time OS. These programs are:
? Central Command
? Navigation
? Collision Avoidance
? Thruster and Fin Control
Central Command
The central command program ties together input and output from the other three
programs. If the navigation system determines that the AUV is off the desired course, the central
command program will check with the collision avoidance program to insure that the path is
clear, before telling the thruster and fin control system to make any adjustments.
Navigation
The navigation program is only a part of the complete navigation system, which begins
with hydrophones recessed in the front fixed fins of the AUV. These hydrophones are tuned to
hear the frequency that the navigation buoys will continuously transmit. The signal from these
hydrophones is amplified and then sent to a PC/104 signal processor board which “listens” for a
certain shift in the pings received form the navigation buoys. When this part of the ping is
detected, the board will immediately notify the navigation program on the single board computer
13
via the PC/104 main bus of the occurrence and on which hydrophone the shift was heard. The
navigation program will wait until the signal processor has reported for both hydrophones and
will determine what course change (if any) is necessary based on the time difference between the
receptions of the ping shift. If the ping shift is heard by one hydrophone before the other than at
turn needs to be made towards the first reporting hydrophone to get back on course. The
navigation program will report to the central command program towards which direction, if any
the course needs to be adjusted.
Collision Avoidance
In order to avoid obstacles encountered along the way, the Arctic AUV will have a 5-
transducer sonar array mounted in the front dome in order to actively ping in many different
direction to detect objects that the AUV may be approaching. The collision avoidance program
will send a signal to begin an active ping of all the transducers through a PC/104 digital IO board
and store the exact time of this order in memory. After sending the ping, the transducers will
then be used for listening for the reflected signal. The transducers in this array will have their
reception signals amplified in much the same way as the navigation hydrophones. These
amplified signals will be sent to the same PC/104 signal processor, which will report to the
collision avoidance program reception of the reflected signal from each transducer. By recording
the time of each reception into memory and comparing with the send time, the collision
avoidance program can determine the distance to the nearest obstacle in every direction and then
use a logic program to determine if any of the obstacles warrant a course change and, if so,
which direction to take to avoid the obstacle. The basics of this logic program are shown in
Figure 5 in flow-chart format. In the flowchart the directions (front, bottom, top, left, and right,
are the time differences between send and reception of the signal and their corresponding
variables (F, B, T, L, & R) are a pre-determined distance at which the obstacle is a threat to the
vehicle and is based on the speed of the vehicle and the rate at which it can turn at that speed.
All action blocks are outputs to the central command program. Action blocks with bold boarders
cause the program to return to the top left decision block with a double line border.
14
Slow Front > F
Bottom > B & Top > T
Left > L & Right > R
Up
No
Speed >
½ kn
Speed =
½ kn Bottom > B
Yes Down
Yes
Yes
No
Top > T Yes
Up Only Bottom < B
Yes
Down
No
Only Top < T
Yes
No
No
Slow Speed =
½ kn Left > Right
Speed >
½ kn
Left
Right
Yes
No
Right Only Left < L
Yes
Left
No
Only Right < R
Yes
No
No
Slow Ui = 2kn
Top > T Ui > 2kn
Up
Down
Yes
No
Bottom > B
Yes No
Reverse Figure 5: Collision Avoidance Flow Chart
15
Thruster and Fin Control
The thruster and fin control program simply stores the speed of the thruster and the
position of the fins and makes necessary adjustments as directed by the central command
program. The control of the fin servos and thrust motors is done by PC/104 motor controller
boards with communication via the PC/104 main bus.
Miscellaneous
The main control system will also include a keypad and LCD interface board (also
PC/104) that will allow the user to input mission data via a small keypad with the options
displayed on a small LCD display. The LCD display will be viewable though an acrylic window
in the pressure housing and the keypad will be accessible by opening as small hatch in the
housing.
Data Logging System
The data logging system stores data from the scientific instruments and camera to a
laptop hard drive. The system is composed of a low power, Ethernet capable PC/104 single
board computer, PC/104 video capture board, laptop hard drive, RS232 compatible scientific
instruments, and video camera with an RCA output. The single board computer will capture data
from the scientific instruments via RS232 COM ports and record this data to a file on the hard
drive. The video capture board will periodically capture frames from the video camera, which
the single board computer will store as picture files on the hard drive. These time intervals for
data capture can be set by placing a mission data file on the hard drive via an Ethernet link
between the single board computer and a laptop computer. Also, data will be able to be retrieved
through the same link after mission completion. The Ethernet plug will be accessible through the
same hatch used to access the keypad.
The following pages contain pictures and basic information about the computer boards
mentioned in this section. They are all manufactured by Arcom Control System and are taken
from their PC/104 Product Guide.
16
The SBC-386 provides the performance and reliability of previous generation boards, with the addition of on-board Ethernet at a reduced cost. The SBC features the low power, high performance 25MHz 386EX CPU from Intel surrounded by a host of functionality including: (3) serial ports, debug port, 10baseT Ethernet, 2MB DRAM, 1MB Flash, up to 512K battery backed SRAM, and an on-board 8-18VDC (or 10-16VAC) power supply.
The SBC-386 is rated at an operating temperature of –20 to +70C, and has been designed to meet European CE standards. The board is supplied as standard with Treck’s Real-Time TCP/IP stack and Supertask Multitasking Operating System pre-installed, and has the backing of a full suite of software development tools offered by Arcom.
17
18
Conclusion
UndeSea Solutions, Inc. has created an under-ice sampling AUV that will function
effortlessly in less than desirable conditions in North Alaska. This AUV is the culmination of an
entire semester worth of research, design, and testing in the areas of mechanical, electrical, and
computer engineering. This AUV was engineered to the highest degree to be both structurally
sound as well as operate to the fullest efficiency.