Aviation Systems

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    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

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    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)

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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

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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)