APOLLO TRAININO GUIDANCE AND CONTROL SYSTEMS - BLOCK II s/c lO_ 15SEPTEMBER 1967 FOR TRAINING PURPOSES ONLY OOI6"l'le2_ APOLLOTRANI ING GUIDANCE AND CONTROL SYSTEMS- BLOCK II s/c _o_ 15SEPTEMBER1967 FOR TRAINING PURPOSESONLY OGIS, _'_¢Q QUESTIONS RELATIVETO THECONTENTS OF THIS DOCUMENT SHOULD BEDIRECTEDTO: D.P. BENNETT A.R. PAYNE W.O. RUFFIN A.H. SOHLER NAA, SD DOWNEY, CALlFORNIA Extension 4325,6, or 7 TABLE OF CONTENTS Section Page I INTRODUCTION .......... 1 II COMPUTER AND COUPUNG DATA UNITS ...... 9 HI OPTICAL AND INERTIAL SUBSYSTEMS . . . Z9 IV ATTITUDE CONTROL SUBSYSTEMS . . 48 V ATTITUDE REFERENCE SUBSYSTEMS .... 70 VI NAVIGATION . 87 VII THRUST VECTOR CONTROL SUBSYSTEMS AND SIVB TAKEOVER 94 VIII ENTRY CONTROL AND DISPLAY (EMS) . . . 1I0 IX POWER DISTRIBUTION, ABBREVIATIONS AND ACRONYMS . . . IZ6 ii CSMGUIDANC,:. & CONTROL VEHICLEDYNAMCI S I'-......... "3 ROTATION TRANSLATION [[ TRANS- LATION SERV0 ii AND _ i PGNCS SCS SPS _ A_P v ASSY L REACTION A ENGINE Y ON-OFF r ASSY RCS SCS I s _! CONTROL i _,rRONAUT BORTEAATIKOoNuTCRONTswITCHEStl T [ - DIRECT RCS ROTATION I_. ....... _,1 VEHICLE DYNAMI CS scs-_oo_c(_._ 1 PROPULSION TORQUE AND FORCEINPUTS TO THE S/C CW +P +PITCH +Y +X -P -Z 12 ROTATIONv_,TRANSLATION +y/ RCSMOTOR(4 SETS) TRANSLATION 3 A16 31 +X + 13 2 ,, ROTATOIN _- PITCH MBALING -Y / 6 _2 DEFLECOTIN -y x cT_ +YAW 11 +Z ROTATION 14C +Z TRANSLATION GIMBALING DEFLECIOTN scs-oo, A 2 PGNCS DATA FLOW STEERINGSIGNALS (S-IVB) ATTITUDEERROR& ATTITUDE_I SCSDLSPLAYS& I..,SCWOINTCFHIGINUGRATION, (: !1 vm ,,,_,,u_,-m l m ..,-,.BI TM m m CONTROLS i , .iGIUIDANCE I I B_AG II ' SYSTEM p . IU I LZV' ALIGNMENTAND 'NuTsll SEQUENCECONTROLI i m_ CONTROCLOMMANDS I I I M,aI,N STEERINI G I / NERTIAL STATUSOFINERTIALSUBSYSI I I I DISPLAY SIGNALSI I IIII I I I SUBSYSTEM ACCELERATION CONTROL coIuA.m,.Oo PAN . CONF-- \ RUST \y"_ I ICMDS_, T ___ I i I COMPUTER IATTITUDE'ISCS _ {A_TPn-_ ICMDS .J _'_I_AUT_' .... "1_I SUBSYSTEM INTERFACkE I / ANGLAENSD ++ + ---_ h I I / MACROKMMAmNI /D ÷÷++ • , I STATUSOFOPTICALSUBSYSI / , , SPS,RCS& SIVB SUOBPSYTSITCEAMLI MINIMUIMMPULCSOENTR/OL I PROPULS'ION I_ (OPTICS& CONTRO&L POSITIONCOMMANDS I SYSTEMS I CDU'S) I SICSTEERINGSIGNALS(SPS) I I fT_o GNC-5D(4,') PGNCS EQUIPMENT OPTICS ASSEMBLY PIPAELECTRONICS SIGNACLONDITIONER IMU ASSEMBLY_ INDICATORCONTROPLANEL _'q_l I POWER NEDLSKY ASSEMBLY • ) COUPLINGDATAUNIT _" COMMANDMODULE COMPUTER _""_'" 4 GUIDANCE NAVIGATION, s,,_o,o,,,,, AND COI_TROLSYSTEM STOWA(_ rOPTICS ASSEMBLY _ __ SIGNAL CONDITIONER ASSEMBLY SPACE _11 _ STECLAENSNCINOGPE SEXTANT INERTIAL MEASUREMENT CONTROL UNIT PANELS I )WER j SERVO ASSEMBLY COUPLING DATA -4- AND NAVIGATION MODULE BASE ' SIDEVIEW 5 SCS FLIGHT HARDWARE BLOCK II . ATT PANEL _._ O.R ELECTRONICDISPLAY ASSEMBLY GYRO DISPLAYCOUPLER SCS-eO'LOC_,_) (EDA) (GDC) 6
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