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L n , JA. " Flguro 5. LlghtwolgM LDR Slgrvl Procwaor Impiomentatlon . : !"""" .................................................... ~ im : : -CE CHlr i wemocEswn j i j CnP .. :: .. .. . I .. :: .. - E U : ! i i TOUR iwotxsson MAGNITUDE , MmEmEn j i : .. I .. : :: co(ysM i :: .. .. .. non . i i ........ j DEUODUUTION FOR BOTH COUUUNICATIONS AND ACQUISITION LIG"WE!GHT IYPLEMEMATION ALLOWS UP TO 256.B.pOINl TRANSFORM flgun 6. Dlg11.1 FFl Drmndulrlor . .. !
0- PREPROC PREPROC i 16 COMMUI(ICATI0N CHANNELS ROM DOWNLINK PROCESSOR RESOURCE CONTROLLER FQun 8. Dunoduhtor and Upllnk Procouor ulllcchlp yodula Conflguatlon
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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
Page 112: A cct instant. ct si IC PDOP cat in
Page 116: giostationnaire (RS mlslnn contrc 5
Page 120: 0 This pqxr is dividcd in lhrcc pat
Page 124: 0 Grouad-air-ground communication T
Page 128: 0 a .. . . .I AIR COMMAND AND CQNTR
Page 132: ENNEAAV ORDER OF BATLE ASSESSMENT D
Page 136: 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 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 190: \ I ..I , .. . . U' c L. rL 50 i !
Page 194 and 195: It is IqmmtQlive of the ,wc.sa Cmst
Page 197: I' !'.
Page 201: v / I ,p ,
Page 204 and 205: f I
Page 209: 3. IAUWCUU SVSTEM SELECTION CRUQTXO
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19-41 5.8.1.8 A/Im faniity of whicl
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CURRLHT PRowcTKm N DEVELOPMENT " P
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.clrc;lih w m iua thc orhilot planc
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19-10 OcazO midm ~ r nof mp htb~rm
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19-12 0 'I% whicles must PW: lnunch
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8.3 Uniad KingdodWussia Inrtn'm HOT
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1P.16 'II-tcx chen@ngcnvimnmcntal c
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SPACECRAIT AND I.AIJNCII SIISlT.MS
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c Firvn 4. Horimld vrhiclr andpaylo
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H 8p~nwmd by DARPA ud will dcliwr8
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'ThcTauNt prylodckcoicwl inlnlactt
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20-10 (hcntercoaunnndma have ben di
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RESUME Puisque ks futun lanceun per
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. 232 CdcJ du IIIOIWYHI?~ Mmoeuvm m
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En rcvnnchc, m ce qui concemc la pe
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Lea masses d'ergoh pour les trois o
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- Figure 13 - Les orbiteo intermedi
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SVMMARy - rution inonly I5 monh. Qu
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I f igun 5-1 QulrUfar spcun@ syslrm
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?- I
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* Snull ground conlrol VMS 1s.a.a F
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.. 1. INTRODUCTION Attitude- and Or
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m, = f*U*d Whcn liquid bipropellant
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sensors, gyros) intorporated in the
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th: burn-our (or dry) mm and subsys
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23-10 between the modulator output
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23-12 . pcnsatc for thc imbact of l
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23-14 e I w 11 n IS n n a 41 U 9s M
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23-16 / Fig. 4.3.1: ICDS principle
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23-18 Communication Weat her - Oper
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23-20 r - .-_ -- - -. --_.._ I U i
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23-22 I .a * .o.s 8.2 am3 c 0.012 a
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PRW mrms lottrfrsa : UDir Bnterfscc
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24.2 CJ6Qh ion pl'b;pPelaion tho ap
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48 iao 4.b 11 8.2 19.3 26.5 88.6 C
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I I ! I i ~ I I I I I I I ! I I I I
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[ Z ] C. Purrotta, M.Bieconi, A. Bi
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I 23-2 2. ):SADLISG TF.CIISOLOGY PR
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124.1 PhwdAwmy Mimv.~tnhbkL.u#eApn(
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Lulrhd durimilr NASA md Navy p*bd o
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2s-a The paylord concept is distinc
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2s-10 \ I i I f
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~Y!!?w!L Tho fnasibllity of install
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c_- XZiiK matelT. mloy ka>r*can h.i
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, i'or a typical 708 operating duty
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Tho ]Lo~ton boU& Of the Dfb-UFfliTf
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I I 0 I I I I I , For tn ainglo pla
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NovorthdanfS high frograonq CIQBfi~
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008e~Ensrr witfa ~ bde~ec~ion s of
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! I I I
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I I I I I ! I I I I I I ~ I I I I I
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274 from soia may. For this mission
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=mitrioa~ ~ ~ h i frown ~ ~ e allei
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e The SAW must possess a raa)is$wet
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I I I ! 27-9 Different data rate: c
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In resent ears, industry made gr0fp
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I I I I I I , I .: I I I 27- 12 7.0
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27-14 , I I
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, ._ .'< . , '\ '
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LOW.oIlN ANTENNA b ClsLEWRIP 4 SOWR
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NOI-1-0' MZ-1-90 NO 3- I I 57 NO1-1
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Cost Efl'ectivc TacSats for Militar
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' Figure 3. Usa Driven Dwign Future
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L Figure 6. Tu&oprrpliom Rovi Usus
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Vlrtbl~ D~tect~n b Rows of 18um qua
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I I I . . / 0 - 0 0 0 0 0 0 0 0 0 0
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covering a variety of scenes, asses
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AbsltmsU 'E'AC.WT MEmOROWflCU PAYLO
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I I I I Trtarasiaiaand Pnogramme (M
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several chys. If S~CDPO term foreca
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e: l , / I Discussion Question: You
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7 t!lETTl?3T iDOCWMEWAmOT'd PAGE AG
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