A

EARTH ORBIT GEOMETRY FIGURE 1 VIEW ON SURFACE FIGURE 3 SIMPLIFIED ORBITAL NAVIGATION FUNCTIONAL DIAGRAM TRACKING MEASUREMENT INCORPORATION ROUTINE J SIMPLIFIED CMC RENDEZOUS NAVIGATIONAL ESTIMATE OF REND. SENSOR MEASUREMENT TRACKING MEASUREMENT INCORPORATION ROUTINE REACTION JET ENGINE ON-OfF CONTROL ASSEMBLY REACTION JET ENGINE ON-OfF CONTROL ASSEMBLY MANUAL SWITCHING INPUTS FOR CONFIGURATION LOGIC AND ENABLING FUNCTIONS TO ALL ASSEMBLIES REACTION JET ENGINE ON-OFF CONTROL ASSY HIVE CDU S...

Tvc

i m o IMU GIMBAL ANGLES INNER, Ml DDLE AND OUTER. ic *mc OC IMU GIMBAL-ANGLE COMMANDS INNER, Ml DDLE AND OUTER. ei em eo GIMBAL-ANGLE ERRORS INNER, Ml DDLE AND OUTER. ep ey eR SPACECRAFT ATTITUDE ERRORS PITCH, YAW AND ROLL. ap 4Y PITCH-AND YAW-CHANNEL SPS GIMBAL-ANGLE COMMANDS. 4R ROLL-CHANNEL SM RCS ENGINE ON-OFF' COMMANDS. FUEL PRESSURE GIMBAL POSITION INDICATOR CMC CMD'S ARE DISABLED IN CMC IF TC IS CW OR SC CONT SWITCH IN SCS POSITION CMC CMD'S ARE DISABLED IN CMC IF TC IS CW OR SC CONT...

Indicator Control Panel

gt 1 w ki n I It A H6US 1 11 A IM. 'tO O U LC I WC L U Cll kk, I COT C T I H.LLCI II I k C IT A, L K I I LI L CG3I70V - SCT TRUNNION TACHOMETER OUTPUT CG3160V - SCT SHAFT TACHOMETER OUTPUT CG315W - SXT TRUNNION TACHOMETER OUTPUT CG3140V - SXT SHAFT TACHOMETER OUTPUT CG3721V - SHAFT CDU DAC OUTPUT GNC-129C gt SPACECRAFT amp GUIDANCE SYSTEM AXES NAVIGATION GIMBALED PLATFORM MG TORQUE MOTOR CG2112V - IG IX RESOLVER OUTPUT SIN CG3113V - IG IX RESOLVER OUTPUT COS CG2142V - MG IX RESOLVER OUTPUT SIN...

Block Ii Stabilization Loops

CG2117V - IGA SERVO ERROR IN PHASE CG2147V - MGA SERVO ERROR IN PHASE CG2177V - OGA SERVO ERROR IN PHASE CG2117V - IGA SERVO ERROR IN PHASE CG2147V - MGA SERVO ERROR IN PHASE CG2177V - OGA SERVO ERROR IN PHASE PI PA SG OUTPUT IN PHASE PI PA SG OUTPUT IN PHASE PI PA SG OUTPUT IN PHASE PI PA SG OUTPUT IN PHASE PI PA SG OUTPUT IN PHASE PI PA SG OUTPUT IN PHASE TEMP LIMIT T WARNING TO COMPUTER

Rotation Control

TRAVEL PRIOR TO SWITCH ACTUATION TRAVEL TO HARDSTOP MAXIMUM TORQUE 8.0 MIN 25.0 MAX 1.0 POUND INCHES BREAKOUT SWITCH ACTUATION CONTROLLER LOCK TO ARM DISPLACEMENT 1L 5 0.50 IL 0 10 1 1.5 0.5 5tt 0 DIRECT RCS SOLENOIDS amp RJ EC AUTO RCS LOGIC HARD STOP, DETENT amp SWITCH CLOSURE FORCE INTO DETENT OUT OF DETENT TRANSLATION CONTROL MOTION LIMITS OR - COMMANDS MECHANICAL STOP - a 5 0.075 ARC INCHES SWITCH CLOSURE - a375 ARC INCHES v - r ' 17 scs ENABLE 3K1 - RATE I IGN 2 J SCS AUTO CW SCS RATE CMD...

Scs Control Panel Switching Tm

Functional Flow Block Diagram

CH3635X - BMAG MODE SW ROLL AH I RATE 2 CH3636X - BMAG MODE SW - ROLL RATE 2 CH3638X - BMAG MODE SW - PITCH ATTI RATE 2 CH3639X - BMAG MODE SW - PITCH RATE 2 CH3641X - BMAG MODE SW - YAW ATT 1 RATE 2 CH3642X - BMAG MODE SW - YAW RATE 2 FLIGHT DIRECTOR ATTITUDE INDICATOR NO. 2 FLIGHT DIRECTOR ATTITUDE INDICATOR NO. 2 FLIGHT DIRECTOR ATTITUDE INDICATOR NO. 1 FLIGHT DIRECTOR ATTITUDE INDICATOR NO. 1 EULER ATTITUDE ON BALL PITCH - 9 014 YAW - 034 ROLL - lt P 330 ALL POLARITIES INDICATE VEHICLE...

Imu Alignment Measurement

Apollo Imu

IBSfSflHllBHWHllBSSiBllB iBI lEnaiiitfaailEzniliBM EXTD REl -RETRACT-II-LIGHTS-, LM PWR DOCKING - PRIM 1 SEC EXTERIOR TUNNEL CSM TARGET I t_ 11_ I _ gt _ I_ _ J _ I I I NORMAL CSM POWER I LAMP TIST START NORMAL CSM POWER I LAMP TIST START TRANS CMO CHANNEL DISABU -SCS AUTO MAN ATT MODE SW-SPS ENC ICN 1-DIRECT ROT- r H I-, CHANNEL PHA OF 1 'E' I I SWITCH J 1-1 r H I-, CHANNEL PHA OF 1 'E' I I SWITCH J 1-1 2. DAP DATA 1 Specify A P configuration FLV04 N46 Request data load Load data EXTENDED VERB...

Cdu

Block Diagram Cdu

DRIVE PULSES ' FROM CMC 160 S PULSE FDAI ATTITUDE ERROR SIG. IMU GIMBAL MOTOR DRIVE SIG. OPTICS ERROR COUNTER ENABLE 12-2 OPTICS ERROR COUNTER ENABLE 12-2 40 SEC PULSE SHAFT 10 SEC PULSE TRUNNION DRIVE PULSES FROM CMC 160 SEE PULSE SHAFT 40 SEC PULSE TRUNNION 851E5 PULSE SPS GIMBALS READ COUNTER RELATIONSHIP TO COARSE FINE SWITCHING COARSE SWITCH LOGIC EQUATIONS DC 1 - 2l5214213 2I52-Ii2Ty DC 2 . SZUP PPP DC 3 215 214213 15 2ii2i5 DC 4 - 2T52T3213 213 z14 1 2N - N REFERS TO BIT IN THE READ...

Main Display Console

Apollo Guidance Computer

It all NUC TON MNCL TUMUTHM, DOTATION . TWIN L.t. X VB.OOTY L.B. Y VtlOOTY t,r z vtioanr AT 51.2 KC BIT RATE TELEMETRY SYSTEM F03 Optical Verification of Azimuth Pll Earth Orbit Insertion Monitor Coast P23 Cislunar Midcourse Navigation P34 Transfer Phase Initiation TPI P35 Transfer Phase Initiation Midcourse P51 IMU Orientation Determination P53 Backup IMU Orientation Determination P6l Entry Maneuver to CM SM Separation Attitude P62 CH SM Separation amp Pre entry maneuver P74 LM Transfer Phase...

Pgncs Equipment

Space Sextant

GUIDANCE, NAVIGATION, AND CONTROL SYSTEM REACTION JET AND ENGINE ON-OFF CONTROL RJ EC GIMBAL POSITION FUEL PRESSURE INDICATOR GP FPI THRUST VECTOR POSITION SERVO AMPLIFIER TVSA FLIGHT DIRECTOR ATTITUDE INDICATOR FDA11, FDAI 2 FLIGHT DIRECTOR ATTITUDE INDICATOR FDA11, FDAI 2