Csm Guidance Control
PROPULSION TORQUE AND FORCE INPUTS TO THE S C -CCW p TCH Y W ROTATION TRANSLATION
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
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
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 1
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
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
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
Reference Coordinate Systems
Ot RIGHT ASCENSION ANGLE 8 m DECLINATION ANGLE r POSITION VECTOR GEODETIC POLAR ROTATING L - LONGITUDE X LATITUDE GEODETIC POLAR ROTATING L - LONGITUDE X LATITUDE Ot RIGHT ASCENSION ANGLE 8 m DECLINATION ANGLE r POSITION VECTOR