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\ I ..I , .. . . U' c L. rL 50 i ! ml12 781UiSi20 21.36:m UTC 3 63.4" 275" 0.73 -WO 0.3" I. I WO 0.0e +tu one . 2656I.'d9 km - Time (Hours) m124 78106120 21:36:0 UTC 4 63.4. 65 " 0.73 -90" o.oo One 0.oc +oo ale 42164 km Fig. 1. Elevation angle voriotion for different orbits. ! I n U Valats rw Tundra Orhit tundr 78/05/20 21:36:00 UTC 5 63.4" 20" 0.374 -90" 0.0" One O.&+OO One 42164 km
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ADVISORY GROUP FOR AEROSPACE RESEAR
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Acccorclinp tto 11s C”liirlcr. th
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0 Im oyi.rationr rcccntc\ *Tcm+tc d
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Theme 'fieme 0 - 0 Avionics Pencl a
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-- Printed in Clawificcl puhlicatio
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1'. 2 c From tplc four pafcn. thcrc
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Talcs. Thc lcchnology emphasis wnr
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These arc three spccific fecornmen&
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when WO Rave gone from one'modsl sa
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3-4 mggd and easily operated. This
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3-6 interim capability should one o
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OI~UI'IS MISSIONS I PAYLOAD TYPE -.
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1 Int raduction The iiotcntial cxpl
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indicated hat an IR vcrsion of the
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a 0 Annex A Radar system A. I Backg
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Annex C ESM system C.1 Background A
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e communications, point to point, p
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(i-4 TACSAT Operations Phase The TA
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6-6 w J > a 3 v, [E ' 0 LL U3 I- Q
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(1-2 rcliabiliry pcrfornianccs, bot
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0 8-4 specific tools for each main
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0 0
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affichent un coot au kilo de 2 a 3
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I 1 - CONSTELLATION LAIJNCHES COST
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ls FIGURE 3 6-11
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a a
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SYmME DE NAVIGATION PAR SATELLIT'ES
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du sntcllitc fixCe. Aucunc controin
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0 0 ' ml 3200. 2800. 2400. 2000. 16
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A cct instant. ct si IC PDOP cat in
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giostationnaire (RS mlslnn contrc 5
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0 This pqxr is dividcd in lhrcc pat
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0 Grouad-air-ground communication T
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0 a .. . . .I AIR COMMAND AND CQNTR
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ENNEAAV ORDER OF BATLE ASSESSMENT D
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0 0 (CO") -COMMUNlCATlONTACSATSARE
Page 140: 0 0 . 14-2 xiv)physical attack and
Page 144: 14-4 There has been a minimum of jo
Page 148: Architecture TABLE -1 Number of Sat
Page 152: 14-8 Table - 3 : The EHF Ground Seg
Page 156: 0. 16-2 combincd analog and digital
Page 160: flgurm 2. Frequency Synlhmrlur Aduc
Page 164 and 165: L n , JA. " Flguro 5. LlghtwolgM LD
Page 167: GEOSYNCHRONOUSALTITUDEORBlT VARIABL
Page 170: I SYNCHRONIZATION TECHNIQUES FOR ME
Page 174: -U I 1 b I l l . . . . , Figure 2:
Page 178: @ & a time acquisition. Due to thc
Page 182: 6 SYSIXM SYNCHRONIZATION ALGORITHM
Page 186: TACSAT payload. Sptinl and time syn
Page 192: 4fi 2345 hm 0830 hrs' 2245 hrs 270.
Page 195: Flg. 4. Mmpd 8 d Rock, WA. -17-16-$
Page 199: C. c 1-- 24 U < L c 0 - c i C - ,9
Page 203 and 204: 6x1 Cammm To mqienasclz: 1 P 4 lln
Page 205: 0 0 18-1 1 (91 Mayes. d&ri D.. Dycr
Page 211: mum (3 ~qnrlra;Og~m.or~~~n.olR6r?Qi
Page 215: - .d: 5.1.2 EMlOP Eump is Pcpn:scnt
Page 221: 1 6.1 Cumt ud NcwTcm, r*n.ri and Pr
Page 224 and 225: 0 0
Page 227: 6.2.2 UniEcd Kin~domlNonvay I-ii~lc
Page 231: 7.9 Fmmp 1.9.1 Unitrd Kingdom (U0 M
Page 235: Many of thnw splcms and platforms w
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25.. NFQ %&myr* Spcrcc Clipper. Cam
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Figvn 1. Pegorus kjligh. 1
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Wilbpflamed pailbnin6ofrrbkk1mdfril
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payload upruiun syucm is availnhle.
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APEX 1993 247 kg 375w 3 Axis, 0.5'
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countries for several years. Couple
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21-2 2 POSI'6"ION DU PROBLEME 2.1 M
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214 Dens le cas ."un aanslen bi-imp
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21-6 ,...-. ".._ . + . I.. 0 8 IO I
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21-8 Cea finurea montrant qul le co
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21-10 d'iugrnmter nu cours des itdr
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I - - AI with Ihr cue of LOSAT-X. O
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Thc ADACS provido *ti!dc &lamhh ud
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.- I
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12-11 Spacecraft Family Carrying Ty
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23-2 . - missile wnrninq, e.g. agai
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234 L -'*. f . . 23 AOCS Opntioncrl
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i3-6 yuratiori. Whcel desaturatioo
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23-8 tional and storzge capacity aa
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contains thc H/w systcm configurati
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Figs. 2.1- la-2.1- IC: Parmeters fo
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Fig. 4.1-1 a/h: SIC orientation U2
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4 2 0 -2 -4 t . . . I "W Fig. 4.4-1
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Control Accuracy 1 Control oncep pi
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0.75 - 0.2 2 - 0.6 6 - 1.85 IO - 3
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abic 4.2-2: Corrcspadaucc bcwccn to
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lpnpQR rOYi0WS the QdVOUItQ~OQ and
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3.2 P A tuimira ~ ok c~,~~a~aellona
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Thoro are sovoral additlonal positi
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- it is possible to use 8 low level
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I . Ihfcmc Advanced RcJcuch hojccts
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- physical and mvirnnmmtal rrquirem
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IMPACT rill work cbuly wilh thr MIL
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! --- ----FE- UICLIEASWO SAIEI Ill
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i 0
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I 0 I I I @. I 1 @uc?otion: You men
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aLRaqy1 rsmnto ,.verviaw An incrooa
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264 giving tho nunbor of oaeollitnn
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0 I
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280 65.0 63:6 40.1 360 84.6 81.8 56
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I I I
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I I I
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The small size aaad low mts of the
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The dediated nature of the sumeiUUa
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274 The outhe cdmcept of a SAR moun
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In order to erform a useful recoanw
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I I
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-.- I I I I I !
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27-10 Currcunaly available ground a
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I ! I I I I I
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Figure 1 Figure 2 \ '. 0 # --e- I i
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SliMMARY Cost and ycrformancc techn
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. FIQURE 2. REPRESENTATIVE OPERATIO
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mr a n problem. The pal was to Jcwg
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w 4 I Discussion Question: May you
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- SURVEILLANCE - ENVIRONMENTAL FLEX
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31-4 spciri dtilrdo * beMsa 450 rd
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*APERTURE *FOCALLENmn OAS U STARINO
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Tb lSB in &a "heat" of ha TacSet sp
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: 0' 31-10 plovadm mglc apecity int
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31-12 _. ’ Discussion Question: W
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33-2 commander. Parameters sP iwter
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, I I I : I I 33-4 . I. psitiom am
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Figure1 World Met roroloKy -h Visib
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, Comment: TACSATS, 1 only as "truc
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. 1.
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