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8/11/2019 Aviation Systems
1/13
AVIATION WEATHER
SURVEILLLANCE SYSTEMSAdvanced radar and surface sensors
for flight safety and air traffic management
PRAVAS MAHAPATRA
with contributions from
Richard J. Doviak
Vladislav Mazur
Dusan S. Zrnic
of the US National Severe Storms Laboratory
The Institution of Electrical Engineers
The American Institute of Aeronautics and Astronautics
8/11/2019 Aviation Systems
2/13
Copublished by:
The Institution of Electrical Engineers,
Michael Faraday House,
Six Hills Way, Stevenage,
Herts. SG1 2AY, United Kingdom
and
The American Institute of Aeronautics and Astronautics
1801 Alexander Bell Drive
Suite 5
Reston
VA 20191-4344
USA
1999: The Institution of Electrical Engineers
This publication is copyright under the Berne Convention and the
Universal Copyright Convention. All rights reserved. Apart from any fair
dealing for the purposes of research or private study, or criticism or
review, as permitted under the Copyright, Designs and Patents Act, 1988
r
this publication may be reproduced, stored or transmitted, in any forms
or by any means, only with the prior permission in writing of the Institution
of Electrical Engineers IEE) or in the case of reprographic reproduction in
accordance with the terms of licences issued by the Copyright Licensing
Agency. Inquiries concerning reproduction outside those terms should be
sent to the IEE at the address above.
While the author and the publishers believe that the information and
guidance given in this work are correct, all parties must rely upon their
own skill and judgment when making use of them. Neither the author nor
the publishers assume any liability to anyone for any loss or damage
caused by any error or omission in the work, whether such error or
omission is the result of negligence or any other cause. Any and all such
liability is disclaimed.
The moral right of the author to be identified as author of this work has
been asserted by him/her in accordance with the Copyright, Designs and
Patents Act 1988.
ritish Library Cataloguing in Publication Data
A CIP catalogue record for this book
is available from the British Library
ISBN 85296 937 6
Printed in England by Short Run Press Ltd., Exeter
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to my p rents
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Preface
While writing this book I had the feeling of chasing and trying to catch the pieces
of an exploding bombshell. So rapid and diversified has been the growth of the
subject of this book in the recent past, that there was a distinct fear of the book
becoming obsolete even before it was completed. I have therefore taken the
approach of focusing more on the fundamental aspects of the aviation weather
problem and generic solutions to them. Specific equipment and systems are
referred to essentially to illustrate the capabilities and potential of modern
aviation weather surveillance systems, as well as the problems encountered in
performing the surveillance function. The specific systems also serve to provide a
realistic flavour to the description. One casualty of such an essentially generic
approach has been the relative lack of reference to specific software and
algorithms th at perform many of the intelligent tasks described in this book . But
given the fluidity of the software scene which undergoes rapid and continual
upgrading, substantial coverage of specific software would be impractical for a
book of this natu re.
The boo k is written with scientists, engineer s, airline techno logy m anage rs, civil
aviation planners and other interested meteorological and aviation personnel in
mind. Most of the material presented here should be of value in the training
programmes of aviation operators including pilots and air traffic controllers.
The literature in the area of aviation weather surveillance is vast but scattered
am on g a wide variety of sources. This highly interd isciplinary area of activity draws
personnel and information from diverse scientific and technological fields which
are fundamentally different from one another, each with its own distinct
methodology, focus and even jar go n. T his book is the first attem pt to mak e a
synthesis of such scattered inform ation an d to presen t it to pe rso nn el with diverse
backgrounds in a coherent manner for independent and self-contained reading.
The information contained here is graduated in such a way that the serious
technically minded reader can apprise himself or herself of many details of
modern aviation weather surveillance, while the lay reader can still get a fair
appreciation of the intricacies of the interplay of various apparently unrelated
factors in the common task of aviation quality improvement.
Pravas R. Mahapatra
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Acknowledgments
I am indebted to many in bringing this book to the present form. First and
foremost, I wish to express my deepest gratitude to Drs Dusan Z rnic and Dick
Doviak of the US National Severe Storms Laboratory (NSSL), who have long
been my friends, philosophers and guides in this area of inquiry, and who,
along with their colleague and my friend Dr Vlad Mazur, have contributed the
last three guest chapters of the book, and also othe r graphical material tha t
has greatly enriched this work. I have also been fortunate in receiving
inspiration, both philosophical and practical, from my special friend and
former director of NSSL, Dr Ed Kessler. A large number of professional
colleagues and manufacturers representatives from around the world have
generously contributed and permitted their material to be included in
this book, for which I am indebted to them. Input from my colleague
Prof. S. P. Govindaraju on aeroplane flight parameters appearing in
Chapter 2 is gratefully acknowledged. Also greatly appreciated is the he lp on
multiple occasions rendered by my long-time friend and colleague Dr M.
Sachidananda in obtaining hard-to-get reference material. Special thanks are
due to the editorial team at the IEE, especially Jo hn St Aubyn, Jo na than
Simpson and Fiona MacDonald who have provided superlative support on all
aspects connected with the processing of the manuscript. I am grateful to the
reviewers of the manuscript who have read the book with meticulous care and
made corrections and useful suggestions which have improved the quality of
the work. Finally, but importantly, I must express words of sentimental
gratitude to my wife Purn ima and children Satya and Pooja who have no t only
cheerfully borne the deprivation of my attention during the thick of this
project, bu t even cheered me u p during my long nocturnal writing sessions.
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Abbreviations
ACARS ARINC co m m un icatio n an d retrieval system
ACAS air bo rn e collision avo idanc e system
A / D analogue-to-digital (conv erter)
ADAS AWOS da ta acqu isition system
ADF auto m atic direction finder
AGC autom atic gain con trol
AGFS aviation gr idd ed forecast system
AJV aviation im pa ct variable
ARINC Aero naut ical Radio, Inc.
ARSR air rou te surveil lance rad ar
ART CC air ro u te traffic co ntro l ce nt re
ARTS auto m ated rada r term inal system
ASD aircraft situa tion display
ASDE airpo rt surface detect ion eq uip m en t
ASOS au tom ate d surface observ ing system
ASR airp ort surveil lance rad ar
ATC air traffic co nt ro l
ATCRBS air traffic co ntr ol ra da r be ac on system
ATM air traffic m an ag em en t
ATMS advan ced traffic m an ag em en t system
AV a irp o rt visibility
AWOS au tom ate d w eather observa tion system
AWPG aviation we ather pro duc ts ge ner ator
CAA Civil Aviation A uth ority (UK)
DME distance measu r ing equ ipm ent
EFAS en ro u te flight advisory service
FAA Fe der al Aviation A dm inistra tion (USA)
FAR Fe der al Aviation R egu lation (USA)
FAST fore/af t scanning techn ique
FDP flight da ta proc essing (or proc esso r)
FFT fast-Fourier transfo rm
GOES geostat ionary ope rat ional env ironm ental satell ite
GPS global po sition ing system
HF high frequency
ICAO In tern atio na l Civil Aviation Org anisation
IFR ins tru m en t f light rules
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ILS in str um en t land ing system
INMARSAT inte rna tion al m ari t im e satel li te organ isat ion
ITWR inter im termin al do pp ler rada r
ITWS integ rated term inal w eathe r system
JAWS jo in t airp ort we ather s tudies
K-H Kelvin-Helmhol tz
LAPS local analysis an d pr ed ic tio n system
LDR linear depo larisat ion rat io
LLWAS low level w ind sh ea r ale rt system
LLWAS-NE low level w ind sh ea r ale rt system with ne tw ork e xp an sio n
LOR AN long -rang e navigation system
LST local sta nd ard time
MAP meso scale analysis an d pre dic tio n (system)
MKS metre-kilogram-second
MLS microwave lan din g system
MO PA m aster oscillator pow er amp lifier
MST m esosph eric-stratospheric-tropo spheric (radar)
MVD m ed ian volum e dia m eter (of a po pu lat io n of drop lets)
NACA Na tional Advisory Co m m ittee on Ae ronau tics (USA)
NASA Na tional Ae ronau tics an d Space Ad m inistrat ion (USA)
NAWPG nation al aviation w eathe r pro du cts ge ne rato r
NCAR Na tional C ent er for Atm osph eric Research
NDB nondi rec t iona l beacon
NEXRAD nex t-gene rat ion rad ar (fo reru nn er of WSR-88D)
NIM ROD N or the rn I ll inois Meteorological Research on Dow nburs ts
PAR precision ap pro ac h rad ar
Pirep pi lo t rep or t
PO SH proba bility of severe hail
PPI plan-posit ion indic ator
PRF pulse repe ti t ion frequency
PRI pulse rep etitio n interva l (same as PRT)
PRT pulse rep etitio n time (same as PRI)
PU P principa l user processo r
RAMS regiona l atm osp heric m ode ll ing system
RASS radio-acoustic so un di ng system
RAWPG region al aviat ion we ather pro du cts ge ne rato r
RDA ra da r da ta acqu isition (un it or subsystem)
RDASC rad ar da ta acquisition status co ntro l
RDP rad ar data processo r (or processing)
RHI range-height indicator
RPG radar p rod uc t gene ra tor
RVR runwav visual ran ge
RWP real- t ime we ather processo r
SAV state-of-th e-atm osph ere variab le
SSR seco nda ry surveil lance rad ar
ST s t ra tospher ic- t ropospher ic ( rada r /prof i le r )
STC sensitivity-time co nt ro l
STO L sho rt takeoff an d land ing
TACAN tactical air nav igation (system)
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TASS ter m in al are a surv eillance system
TCA S traffic ale rt collision avo ida nce system
TDWR terminal dop pler weather radar
TO A time of arrival
TRACO N terminal radar cont ro l
TRSB t ime reference scanning beam
TVAD tan ge ntia l velocity azim uth display
TVS tor na do vortex s ignature
U H F ul t ra-high frequency
USAF U nite d States Air Force
V /ST O L ver t ica l / sho r t takeoff and landing
VAD velocity az im uth display
VFR visual flight ru les
VH F very high frequency
VLF very low frequ ency
VOR very-high-frequency om nira ng e
VORTAC coloc ated VO R an d TACAN systems
WISP win ter icing an d storm s projec t
WS R-88D wea ther surveil lance rada r - 1988 D opp ler
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ym ols
a, b constan ts used tospecify Z-R r e l a t ionship
c s peedofl ight
d
d i a m e t e r (ofhai lsto nes ); distanc e from sensor; thicknes sof
sheared layer
d
m ax
maximum distanceofradarforobserving weatherat a
minimum height
h
min
e
base
of
natural logarithm
e
m a x
h ig hes t e levat ion ang leofther a d a r a n t e n n a d u r i n gthe
scan cycle
f
c
c a r r i e r f requency
f
d
D o p p l e r f r eq u ency
f
dm
m ea n D o p p l e r f r eq u ency
(of an
e n s e m b l eofsca t terers)
f
r
pu l se repe t i t ion f requency
^v Nyquis t f requ ency
/
4
( 0 , ) no rm al is ed two-way pow er pa t te rnofa n t e n n a
g
a cce le ra t ionduetogravity
h
he ig ht (c l earance)
of
r ada r beam above g ro un d
(for
st raight - l ine propagat ion)
h height (c learance)ofr ada r bea m above g ro un d
(considering atmospheric refract ion)
h
m i n
minimum heightofobservationofweather phenomena
V T
k /?'/R(~4/3)
k
m
s a m p le n u m b e r (inf requency dom ai n ) co r res pon d i ngto
the mean Doppler f requency
l
c
referen ce length ( leng thofw ing cho rdatdes igna ted cross-
sect ion)
m refractive in de xofwater
n refractive in de xofair
n
r
t ot al nu m be rofresolut ion volum esorpixelsin afull circ le
of scan
r ran ge (dis tance)
to a
g iven resolut ion volum e
r pos i t ion vector
r
a a
radiusofairport area
r
b
maximum radiusofblind zone
r
m
maximum range (e.g.ofradar)
8/11/2019 Aviation Systems
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r
m a x { a a
maximum permitted distance of radar from centre of
airport area (while providing resolution p
aa
over the
entire airport area)
r
m a x t a maximum permitted distance of radar from centre of
terminal area (while providing resolution p
ta
over the
entire terminal area)
r
m a x
P
maximum permitted distance of radar from the common
centre of airport and terminal areas while meeting the
resolution requirement everywhere within terminal area
r
ta
radius of terminal area
r
u
(maximum) unambiguous range
s
h h
complex scattering coefficient of a hydrometeor
considering the horizontally polarised component of
scattered radiation caused by a horizontally polarised
incident radiation
s
h v
complex scattering coefficient of a hydrometeor
considering the horizontally polarised component of
scattered radiation caused by a vertially polarised
incident radiation
s
v v
complex scattering coefficient of a hydrometeor
considering the vertically polarised component of
scattered radiation caused by a vertically polarised
incident radiation
t
two-way propagation delay corresponding to-a given radar
target or resolution volume
t
m
electromagnetic propagation time delay (two-way)
corresponding to maximum range
r
m
t
s
sampling instant
u, v, w orthogonal wind components wbeing vertical)
v wind vector
v horizontal wind speed
\
h
horizontal wind velocity vector
V
1
longitudinal velocity component
v
t
transverse velocity component
v
r
radial component of scatterer velocity relative to radar
V
77n
mean radial velocity (of an ensemble of scatterers) (used as
fin Chap. 11)
v
u
( m a x i m u m ) u n a m b i g u o u s v elo ci ty
w w e i g h t
of
a i r c ra f t
W
1
terminal velocity (of raindrops)
X
1
samples of (complex) receiver voltage output
B
receiver bandwidth
C radar constant
C
D
drag coefficient
C
L
lift coefficient
^ L m a x
maximum lift coefficient
C
M p
pitching moment coefficient
C\ turbulent structure parameter of refractive index
D drag force; diameter of raindrop
8/11/2019 Aviation Systems
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F
F-factor (related
to
wind shear)
F
equivalent average F-factor
/'(K) Fourier transform
of
weighting function
I
n
G
antenna gain
H
m ax
m a x i m u m a l t it u d eofw e a t h e r s u r v e i ll a n c e
H
D R
ha i l de tec t io n s ignal
/
i n- ph a se c o m p o n e n t
of
r a da r s ignal
I
n
a
n o r m a l i s e d w e i g h t i n g f u n c t i o n
K a t t en ua t ion coef fi c ien t
in
d B / k m ; m a g n i tu d e
of K
K w a v e n u m b e r
K
g
gus t al leviat ion factor
K
5
a t t e n u a t i o n c o e ff i ci e nt due
to
s now
K
1 0
c o n s t a n t r e l a t e dtor e f rac t ive in de xofw a t e r
K
D
p
specific differe ntial ph as e shif t
L lif t force; lo ga ri th mofr a t ioofe c h o p o w e rands ingle- lag
au t oco r re l a t i on es t imate ; l en g th (d i s t ance) in te rva l
L
a
a m p li tu d e loss factor (one-way)
Lf
rece iver f i l ter ing loss
(or
f ini te ba nd w id th loss) factor
L
5
system loss fac tor
M
n u m b e r
of
r ad a r pu l ses used
for
s igna l p roce s s ing (D op p le r
m o m e n t e s t i m a t i o n )
M p p i tc h in g m o m e n t
N n u m b e rofr a i n d r o p sperun i t spa tia l vo lum eperu n i t
d iame te r in te rva l ; no i se power
N
d
n u m b e r
of
ha i l s tones
per
cub ic m e t re
of
spa tia l volu m e
per
mill imetre s ize interval
P ins tan tan eo us pow er leve lofmic rowave rad ia t ion th ro ug h
air
P
0
initial po w er level
of
mic rowave rad ia t ion th ro ug h
air
P
a
ave rage t r ansm i t ted pow er
P
1
po we r associated withtheiths ignal sa m ple
P
r
r ece ived pow er (byr a da r )
P
ro
r e c e i v er o u t p u t p o w e r
P
t
t r ansm i t ted pow er (peak)
P e s t ima ted rad a r ech o pow er
Q q u a d r a tu r e c o m p o n e n tofr ad ar s ignal
R
r a d iusof theea r th; ra infa l l ra te ; auto co rre l a t io nof the
s igna l sample sequence
R' f ictit ious rad iu s
of the
e a r t h
to
a c c o u n t
for
a t m o s p h e r i c
refract ion
of
r a da r be a m
R
g
R i c h a rd s o n n u m b e r
R
s
rate
of
snowfall
S
r e f e re nce a re a (w ing p la t fo rm a rea )
S
k
th s a m p l e
of
thep e r i o d o g r a m
S
m
receiver sensitivity (minimum detectable signal)
S
xx
etc.
wind shear components
T a i rc raft en gi ne thr us t
T
x
pu l se r epe t i t ion t ime(orpulse repe t i t io n inte rva l )
T
1
temperature
of the
layer
in
which
a
wave evolves
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U
de
derived gust velocity
V
9
V
6
radar resolution volume (the subscropt 6 explicitly denotes
6-dB thresholding)
V
a
airspeed of aircraft
Y
n
airspeed vector of aircraft
V
00
speed of aircraft relative to undisturbed air
W magnitude of the range weighting function (of processing
filter)
W absolute (inertial) wind vector
W
w
w i n d s p e e d p e r t u r b a t i o n due towe a th e r f ac to r s
W
x
h o r i z o n t a l w i n d c o m p o n e n t ( us ua ll y a l o n g a e r o p l a n e
g r o u n d t r a c k )
W
y
h o r i z o n t a l w i n d c o m p o n e n t p e r p e n d i c u l a r
to W
x
W
z
v er ti ca l c o m p o n e n tofw i nd (pos it ive d ow nw ards )
Z reflectivity fact or
Z
D P
reflectivity difference (between two different polarisations)
Z
D R
dif fere ntia l reflectivity
Z
e
eq uiv ale nt ref lect ivi ty facto r
Z
h
reflectivity fac toratho r izon ta l po la r i s a t ion
Z
v
reflectivity fac toratver t ica l pola r isa t i on
a angle of attack; constant inK-Rrelationship
a
s t a U
s tal l an gl e
of
a t tack
/3
p rof i ler be am t il t ang le ; co ns tan tinK-R r e l a t i o n s h i p
Sy Kronecker delta function (S =O,tef, S^=I, i=j)
s
extinction coefficient (or specific attenuation); normalised
turbulent energy dissipation rate
ref lect ivi ty
6
b
beam width
6 antenna scan rate
6
potential temperature
A wavelength (of radar signal)
p vector separation between two points (in the atmosphere)
P
0 0
dens i tyofu n d i s t u r b e dair
p
a
dens i ty
of
a m b i e n t
air
p
a a
l inear resolut ion req uir em en t over a i rpo r t area
p
d
duty ratio
p
hv
(0)
co r r e la t i on coeff i c ien t ofpo la r ised s ignalatz e r olag
p
s n
s ignal- to-noise rat i o
p
ta
l inear resolut ion req uir em en t overthe t e rminal area
(outsidethea i rpo r t area)
a
b
bac ksc atterin g cross section
of
ra in d ro p
T J
spectrum width component due to fall speed differences
among hydrometeors
J
0
s pec t rum width com pon en tdue too scillation (s)of
hydrome teo r s
av spec t rum width com po nen t
due to
ro ta t ion (scanning)
of
radar beam
c r
s
spectrum width component due to wind shear
T
1
spectrum width component due to turbulence
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a
v
spectrum width of radial (Doppler) velocity (for an
ensemble of scatterers)
I
2
Q
second central moment of two-way antenna power pattern
a
2
r
second central moment of two-way range weighting function
c r
2
p
variance of the velocity at a point
T
radar pulse width
c f
h h
two-way phase shift with horizontally polarised transmission
and reception
(f)^ two-way phase shift with vertically polarised transmission
and reception
< f i
D P
differential phase (between two different polarisations)
kh
change in aircraft altitude
An turbulence-induced incremental vertical acceleration of
aircraft; perturbation in refractive index of air due to
turbulence
Ar range resolution
AiV number
of
r a indrops
per
un it spatial volum e having
diam eter be tweenD
and
D
+ AZ)
Ay difference
in
wind spe ed
(e.g.
across g ust fronts
and
microbursts)
A Fo urier wavelength
(i.e.
scale
of the
velocity pe r turb at io n)
I spectral density (tensor)