diff --git a/Comanche055/ASSEMBLY_AND_OPERATION_INFORMATION.agc b/Comanche055/ASSEMBLY_AND_OPERATION_INFORMATION.agc index ff67f5d..1314883 100644 --- a/Comanche055/ASSEMBLY_AND_OPERATION_INFORMATION.agc +++ b/Comanche055/ASSEMBLY_AND_OPERATION_INFORMATION.agc @@ -46,7 +46,7 @@ # PINBALL NOUN TABLES # CSM GEOMETRY # IMU COMPENSATION PACKAGE -# PINBALL GAME BUTTONS AND LIGHTS +# PINBALL GAME BUTTONS AND LIGHTS # R60,R62 # ANGLFIND # GIMBAL LOCK AVOIDANCE @@ -62,7 +62,7 @@ # STABLE ORBIT - P38-P39 # TROUBLE # P11 -# TP1 SEARCH +# TPI SEARCH # P20-P25 # P30,P37 # P32-P33, P72-P73 @@ -77,14 +77,14 @@ # P37,P70 # S-BAND ANTENNA FOR CM # TVCDAPS -# TVC INITIALIZE +# TVCINITIALIZE # Page 3 -# TVC EXECUTIVE -# TVC MASSPROP -# TVC RESTARTS -# TVC DAPS -# TVC STROKE TEST -# TVC ROLLDAP +# TVCEXECUTIVE +# TVCMASSPROP +# TVCRESTARTS +# TVCDAPS +# TVCSTROKETEST +# TVCROLLDAP # MYSUBS # RCS-CSM DIGITAL AUTOPILOT # AUTOMATIC MANEUVERS @@ -139,44 +139,44 @@ # REGULAR VERBS -# 00 NOT IN USE -# 01 DISPLAY OCTAL COMP 1 IN R1 -# 02 DISPLAY OCTAL COMP 2 IN R1 -# 03 DISPLAY OCTAL COMP 3 IN R1 -# 04 DISPLAY OCTAL COMP 1,2 IN R1,R2 -# 05 DISPLAY OCTAL COMP 1,2,3 IN R1,R2,R3 -# 06 DISPLAY DECIMAL IN R1 OR R1,R2 OR R1,R2,R3 -# 07 DISPLAY DP DECIMAL IN R1,R2 (TEST ONLY) +# 00 NOT IN USE +# 01 DISPLAY OCTAL COMP 1 IN R1 +# 02 DISPLAY OCTAL COMP 2 IN R1 +# 03 DISPLAY OCTAL COMP 3 IN R1 +# 04 DISPLAY OCTAL COMP 1,2 IN R1,R2 +# 05 DISPLAY OCTAL COMP 1,2,3 IN R1,R2,R3 +# 06 DISPLAY DECIMAL IN R1 OR R1,R2 OR R1,R2,R3 +# 07 DISPLAY DP DECIMAL IN R1,R2 (TEST ONLY) # 08 # 09 # 10 -# 11 MONITOR OCTAL COMP 1 IN R1 -# 12 MONITOR OCTAL COMP 2 IN R1 -# 13 MONITOR OCTAL COMP 3 IN R1 -# 14 MONITOR OCTAL COMP 1,2, IN R1,R2 -# 15 MONITOR OCTAL COMP 1,2,3 IN R1,R2,R3 -# 16 MONITOR DECIMAL IN R1 OR R1,R2 OR R1,R2,R3 -# 17 MONITOR DP DECIMAL IN R1,R2 (TEST ONLY) +# 11 MONITOR OCTAL COMP 1 IN R1 +# 12 MONITOR OCTAL COMP 2 IN R1 +# 13 MONITOR OCTAL COMP 3 IN R1 +# 14 MONITOR OCTAL COMP 1,2, IN R1,R2 +# 15 MONITOR OCTAL COMP 1,2,3 IN R1,R2,R3 +# 16 MONITOR DECIMAL IN R1 OR R1,R2 OR R1,R2,R3 +# 17 MONITOR DP DECIMAL IN R1,R2 (TEST ONLY) # 18 # 19 # 20 -# 21 LOAD COMPONENT 1 INTO R1 -# 22 LOAD COMPONENT 2 INTO R2 -# 23 LOAD COMPONENT 3 INTO R3 -# 24 LOAD COMPONENT 1,2 INTO R1,R2 -# 25 LOAD COMPONENT 1,2,3 INTO R1,R2,R3 +# 21 LOAD COMPONENT 1 INTO R1 +# 22 LOAD COMPONENT 2 INTO R2 +# 23 LOAD COMPONENT 3 INTO R3 +# 24 LOAD COMPONENT 1,2 INTO R1,R2 +# 25 LOAD COMPONENT 1,2,3 INTO R1,R2,R3 # 26 -# 27 DISPLAY FIXED MEMORY +# 27 DISPLAY FIXED MEMORY # 28 # 29 -# 30 REQUEST EXECUTIVE -# 31 REQUEST WAITLIST -# 32 RECYCLE PROGRAM -# 33 PROCEED WITHOUT DSKY INPUTS -# 34 TERMINATE FUNCTION -# 35 TEST LIGHTS -# 36 REQUEST FRESH START -# 37 CHANGE PROGRAM (MAJOR MODE) +# 30 REQUEST EXECUTIVE +# 31 REQUEST WAITLIST +# 32 RECYCLE PROGRAM +# 33 PROCEED WITHOUT DSKY INPUTS +# 34 TERMINATE FUNCTION +# 35 TEST LIGHTS +# 36 REQUEST FRESH START +# 37 CHANGE PROGRAM (MAJOR MODE) # 38 # 39 @@ -184,80 +184,80 @@ # EXTENDED VERBS -# 40 ZERO CDU-S -# 41 COARSE ALIGN CDU-S -# 42 FINE ALIGN IMU-S -# 43 LOAD IMU ATT ERROR METERS -# 44 SET SURFACE FLAG -# 45 RESET SURFACE FLAG -# 46 ESTABLISH G&C CONTROL -# 47 MOVE LM STATE VECTOR INTO CM STATE VECTOR. -# 48 REQUEST DAP DATA LOAD ROUTINE (R03) -# 49 REQUEST CREW DEFINED MANEUVER ROUTINE (R62) -# 50 PLEASE PERFORM -# 51 PLEASE MARK -# 52 MARK ON OFFSET LANDING SITE -# 53 PLEASE PERFORM ALTERNATE LOS MARK -# 54 REQUEST RENDEZVOUS BACKUP SIGHTING MARK ROUTINE (R23) -# 55 INCREMENT AGC TIME (DECIMAL) -# 56 TERMINATE TRACKING (P20 + P25) -# 57 REQUEST RENDEZVOUS SIGHTING MARK ROUTINE (R21) -# 58 RESET STICK FLAG -# 59 PLEASE CALIBRATE -# 60 SET ASTRONAUT TOTAL ATTITUDE (N17) TO PRESENT ATTITUDE -# 61 DISPLAY DAP ATTITUDE ERROR -# 62 DISPLAY TOTAL ATTITUDE ERROR (WRT N22 (THETAD)) -# 63 DISPLAY TOTAL ASTRONAUT ATTITUDE ERROR (WRT N17 (CPHIX)) -# 64 REQUEST S-BAND ANTENNA ROUTINE -# 65 OPTICAL VERIFICATION OF PRELAUNCH ALIGNMENT -# 66 VEHICLES ARE ATTACHED. MOVE THIS VEHICLE STATE TO OTHER VEHICLE. +# 40 ZERO CDU-S +# 41 COARSE ALIGN CDU-S +# 42 FINE ALIGN IMU-S +# 43 LOAD IMU ATT ERROR METERS +# 44 SET SURFACE FLAG +# 45 RESET SURFACE FLAG +# 46 ESTABLISH G+C CONTROL +# 47 MOVE LM STATE VECTOR INTO CM STATE VECTOR. +# 48 REQUEST DAP DATA LOAD ROUTINE (R03) +# 49 REQUEST CREW DEFINED MANEUVER ROUTINE (R62) +# 50 PLEASE PERFORM +# 51 PLEASE MARK +# 52 MARK ON OFFSET LANDING SITE +# 53 PLEASE PERFORM ALTERNATE LOS MARK +# 54 REQUEST RENDEZVOUS BACKUP SIGHTING MARK ROUTINE (R23) +# 55 INCREMENT AGC TIME (DECIMAL) +# 56 TERMINATE TRACKING (P20 + P25) +# 57 REQUEST RENDEZVOUS SIGHTING MARK ROUTINE (R21) +# 58 RESET STICK FLAG +# 59 PLEASE CALIBRATE +# 60 SET ASTRONAUT TOTAL ATTITUDE (N17) TO PRESENT ATTITUDE +# 61 DISPLAY DAP ATTITUDE ERROR +# 62 DISPLAY TOTAL ATTITUDE ERROR (WRT N22 (THETAD)) +# 63 DISPLAY TOTAL ASTRONAUT ATTITUDE ERROR (WRT N17 (CPHIX)) +# 64 REQUEST S-BAND ANTENNA ROUTINE +# 65 OPTICAL VERIFICATION OF PRELAUNCH ALIGNMENT +# 66 VEHICLES ARE ATTACHED. MOVE THIS VEHICLE STATE TO OTHER VEHICLE. # 67 -# 68 CSM STROKE TEST ON -# 69 CAUSE RESTART -# 70 UPDATE LIFTOFF TIME -# 71 UNIVERSAL UPDATE-BLOCK ADR -# 72 UNIVERSAL UPDATE-SINGLE ADR -# 73 UPDATE AGC TIME (OCTAL) -# 74 INITIALIZE ERASABLE DUMP VIA DOWNLINK -# 75 BACKUP LIFTOFF -# 76 SET PREFERRED ATTITUDE FLAG -# 77 RESET PREFERRED ATTITUDE FLAG -# 78 UPDATE PRELAUNCH AZIMUTH -# 79 REQUEST LUNAR LANDMARK SELECTION ROUTINE (R35) -# 80 UPDATE LEM STATE VECTOR -# 81 UPDATE CSM STATE VECTOR -# 82 REQUEST ORBIT PARAM DISPLAY (R30) -# 83 REQUEST REND PARAM DISPLAY (R31) -# 84 START TARGET DELTA V (R32) -# 85 REQUEST RENDEZVOUS PARAMETER DISPLAY NO. 2 (R34) -# 86 REJECT RENDEZVOUS BACKUP SIGHTING MARK -# 87 SET VHF RANGE FLAG +# 68 CSM STROKE TEST ON +# 69 CAUSE RESTART +# 70 UPDATE LIFTOFF TIME +# 71 UNIVERSAL UPDATE-BLOCK ADR +# 72 UNIVERSAL UPDATE-SINGLE ADR +# 73 UPDATE AGC TIME (OCTAL) +# 74 INITIALIZE ERASABLE DUMP VIA DOWNLINK +# 75 BACKUP LIFTOFF +# 76 SET PREFERRED ATTITUDE FLAG +# 77 RESET PREFERRED ATTITUDE FLAG +# 78 UPDATE PRELAUNCH AZIMUTH +# 79 REQUEST LUNAR LANDMARK SELECTION ROUTINE (R35) +# 80 UPDATE LEM STATE VECTOR +# 81 UPDATE CSM STATE VECTOR +# 82 REQUEST ORBIT PARAM DISPLAY (R30) +# 83 REQUEST REND PARAM DISPLAY (R31) +# 84 START TARGET DELTA V (R32) +# 85 REQUEST RENDEZVOUS PARAMETER DISPLAY NO. 2 (R34) +# 86 REJECT RENDEZVOUS BACKUP SIGHTING MARK +# 87 SET VHF RANGE FLAG # Page 7 -# 88 RESET VHF RANGE FLAG -# 89 REQUEST RENDEZVOUS FINAL ATTITUDE ROUTINE (R63) -# 90 REQUEST RENDEZVOUS OUT OF PLANE DISPLAY ROUTINE (R36) -# 91 DISPLAY BANK SUM -# 92 OPERATE IMU PERFORMANCE TEST (P07) -# 93 ENABLE W MATRIX INITIALIZATION -# 94 PERFORM CYSLUNAR ATTITUDE MANEUVER (P23) -# 95 NO UPDATE OF EITHER STATE VECTOR (P20 OR P22) -# 96 TERMINATE INTEGRATION AND GO TO P00 -# 97 PERFORM ENGINE FAIL PROCEDURE -# 98 ENABLE TRANSLUNAR INJECT -# 99 PLEASE ENABLE ENGINE +# 88 RESET VHF RANGE FLAG +# 89 REQUEST RENDEZVOUS FINAL ATTITUDE ROUTINE (R63) +# 90 REQUEST RENDEZVOUS OUT OF PLANE DISPLAY ROUTINE (R36) +# 91 DISPLAY BANK SUM +# 92 OPERATE IMU PERFORMANCE TEST (P07) +# 93 ENABLE W MATRIX INITIALIZATION +# 94 PERFORM CYSLUNAR ATTITUDE MANEUVER (P23) +# 95 NO UPDATE OF EITHER STATE VECTOR (P20 OR P22) +# 96 TERMINATE INTEGRATION AND GO TO P00 +# 97 PERFORM ENGINE FAIL PROCEDURE +# 98 ENABLE TRANSLUNAR INJECT +# 99 PLEASE ENABLE ENGINE # Page 8 # IN THE FOLLOWING NOUN LIST THE :NO LOAD: RESTRICTION MEANS THE NOUN # CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF # SCALE TYPE L (MIN/SEC) OR PP (2 INTEGERS). -# IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22, OR 23 +# IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22 OR 23 # MAY BE USED TO LOAD ANY OF THE NOUN:S COMPONENTS WHICH ARE NOT OF THE # ABOVE SCALE TYPES. # THE :DEC ONLY: RESTRICTION MEANS ONLY DECIMAL OPERATION IS ALLOWED ON # EVERY COMPONENT IN THE NOUN. (NOTE THAT :NO LOAD: IMPLIES :DEC ONLY:.) -# NORMAL NOUNS COMPONENTS SCALE & DECIMAL POINT RESTRICTIONS -# +# NORMAL NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS + # 00 NOT IN USE # 01 SPECIFY MACHINE ADDRESS (FRACTIONAL) 3COMP .XXXXX FOR EACH # 02 SPECIFY MACHINE ADDRESS (WHOLE) 3COMP XXXXX. FOR EACH @@ -276,7 +276,7 @@ # 000XX. MIN MUST LOAD 3 COMPS # 0XX.XX SEC # 12 OPTION CODE 2COMP OCTAL ONLY FOR EACH -# (USED BY EXTENDED VERBS ONLY) +# (USED BY EXTENDED VERBS ONLY) # 13 TIG OF CDH 3COMP 00XXX. HRS DEC ONLY # 000XX. MIN MUST LOAD 3 COMPS # 0XX.XX SEC @@ -297,16 +297,12 @@ # 0XX.XX SEC # 25 CHECKLIST 3COMP XXXXX. FOR EACH # (USED WITH PLEASE PERFORM ONLY) - # Page 9 - # 26 PRIORITY/DELAY, ADRES, BBCON 3COMP OCTAL ONLY FOR EACH # 27 SELF TEST ON/OFF SWITCH 1COMP XXXXX. # 28 SPARE # 29 XSM LAUNCH AZIMUTH 1COMP XXX.XX DEG DEC ONLY - # Page 10 - # 30 TARGET CODES 3COMP XXXXX. FOR EACH # 31 TIME OF LANDING SITE 3COMP 00XXX. HRS DEC ONLY # 000XX. MIN MUST LOAD 3 COMPS @@ -338,7 +334,7 @@ # Page 11 -# MIXED NOUNS COMPONENTS SCALE & DECIMAL POINT RESTRICTIONS +# MIXED NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS # # 40 TIME FROM IGNITION/CUTOFF 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY # VG, XXXX.X FT/SEC @@ -361,7 +357,7 @@ # 47 THIS VEHICLE WEIGHT 2COMP XXXXX. LBS DEC ONLY # OTHER VEHICLE WEIGHT XXXXX. LBS # 48 PITCH TRIM 2COMP XXX.XX DEG DEC ONLY -# YAW TRIM, XXX.XX DEG +# YAW TRIM, XXX.XX DEG # 49 DELTA R 3COMP XXXX.X NAUT MI DEC ONLY # DELTA V XXXX.X FT/SEC # VHF OR OPTICS CODE XXXXX. @@ -373,7 +369,7 @@ # 52 CENTRAL ANGLE OF ACTIVE VEHICLE 1COMP XXX.XX DEG # 53 RANGE, 3COMP XXX.XX NAUT MI DEC ONLY # RANGE RATE, XXXX.X FT/SEC -# PHI XXX.X DEG +# PHI XXX.XX DEG # 54 RANGE, 3COMP XXX.XX NAUT MI DEC ONLY # RANGE RATE, XXXX.X FT/SEC # THETA XXX.XX DEG @@ -388,9 +384,7 @@ # DELTA V TPF XXXX.X FT/SEC # 59 DELTA VELOCITY LOS 3COMP XXXX.X FT/SEC FOR EA. DEC ONLY # 60 GMAX, 3COMP XXX.XX G DEC ONLY - # Page 12 - # VPRED, XXXXX. FT/SEC # GAMMA EI XXX.XX DEG # 61 IMPACT LATITUDE, 3COMP XXX.XX DEG DEC ONLY @@ -399,7 +393,7 @@ # 62 INERTIAL VEL MAG (VI), 3COMP XXXXX. FT/SEC DEC ONLY # ALT RATE CHANGE (HDOT), XXXXX. FT/SEC # ALT ABOVE PAD RADIUS (H) XXXX.X NAUT MI -# 63 RANGE 297,431 TO SPLASH (RTGO), 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY +# 63 RANGE 297,431 TO SPLASH (RTGO), 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY # PREDICTED INERT VEL (VIO), XXXXX. FT/SEC # TIME FROM 297,431 (TFE), XXBXX MIN/SEC # 64 DRAG ACCELERATION, 3COMP XXX.XX G DEC ONLY @@ -417,7 +411,7 @@ # 68 COMMAND BANK ANGLE (BETA), 3COMP XXX.XX DEG DEC ONLY # INERTIAL VELOCITY (VI), XXXXX. FT/SEC # ALT RATE CHANGE (RDOT) XXXXX. FT/SEC -# 69 BETA 3COMP XXX.XX DEG +# 69 BETA 3COMP XXX.XX DEG DEC ONLY # DL XXX.XX G # VL XXXXX. FT/SEC # 70 STAR CODE, 3COMP OCTAL ONLY @@ -441,9 +435,7 @@ # 78 SPARE # 79 SPARE # 80 TIME FROM IGNITION/CUTOFF 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY - # Page 13 - # VG XXXXX. FT/SEC # DELTA V (ACCUMULATED) XXXXX. FT/SEC # 81 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY @@ -451,7 +443,7 @@ # 83 DELTA V (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY # 84 DELTA V (OTHER VEHICLE) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY # 85 VG (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY -# 86 DELTA V (LV) 3COMP XXXXX. FT/SEC FOR EACH DEC ONLY +# 86 DELTA V(LV) 3COMP XXXXX. FT/SEC FOR EACH DEC ONLY # 87 MARK DATA SHAFT, 2COMP XXX.XX DEG # TRUNION XX.XXX DEG # 88 HALF UNIT SUN OR PLANET VECTOR 3COMP .XXXXX FOR EACH DEC ONLY @@ -468,7 +460,7 @@ # 93 DELTA GYRO ANGLES 3COMP XX.XXX DEG FOR EACH # 94 NEW OPTICS ANGLES SHAFT 2COMP XXX.XX DEG # TRUNNION XX.XXX DEG -# 95 PREFERRED ATTITUDE ICDU ANGLES 3COMP XXX.XX FOR EACH +# 95 PREFERRED ATTITUDE ICDU ANGLES 3COMP XXX.XX FOR FOR EACH # 96 +X-AXIS ATTITUDE ICDU ANGLES 3COMP XXX.XX DEG FOR EACH # 97 SYSTEM TEST INPUTS 3COMP XXXXX. FOR EACH # 98 SYSTEM TEST RESULTS AND INPUTS 3COMP XXXXX. @@ -521,7 +513,7 @@ # 34 DSPTEM1 K # 35 TTOGO K # 36 TIME2 K -# 37 TTP1 K +# 37 TTPI K # 38 TET K # 39 T3TOT4 K @@ -577,9 +569,7 @@ # 57 1 DELTAR Q # 58 1 POSTTPI Q # 2 DELVTPI S - # Page 16 - # 3 DELVTPF S # 59 1 DVLOS S # 2 DVLOS +2 S @@ -630,9 +620,7 @@ # 75 1 DIFFALT Q # 2 T1TOT2 L # 3 T2TOT3 L - # Page 17 - # 76 SPARE # 77 SPARE # 78 SPARE @@ -660,9 +648,9 @@ # 3 DELVLVC +4 P # 87 1 MRKBUF1 +3 D # 2 MRKBUF1 +5 J -# 88 1 STARSAV ZZ -# 2 STARSAV +2 ZZ -# 3 STARSAV +4 ZZ +# 88 1 STARSAV3 ZZ +# 2 STARSAV3 +2 ZZ +# 3 STARSAV3 +4 ZZ # 89 1 LANDLAT G # 2 LANDLONG G # 3 LANDALT JJ @@ -683,9 +671,7 @@ # 3 PRAXIS +2 D # 96 1 CPHIX D # 2 CPHIX +1 D - # Page 18 - # 3 CPHIX +2 D # 97 1 DSPTEM1 C # 2 DSPTEM1 +1 C @@ -750,9 +736,7 @@ # LOADED. # # -K- - # Page 20 - # TIME (HR, MIN, SEC) 00XXX. HR DP BIT 1 OF LOW REGISTER = # 000XX. MIN -2 # 0XX.XX SEC 10 SEC @@ -795,16 +779,14 @@ # 2 METERS/CENTI-SEC # # -Q- -# POSITION 4 XXXX.XX NAUTICAL MILES DP BIT 1 OF LOW REGISTER = +# POSITION 4 XXXX.X NAUTICAL MILES DP BIT 1 OF LOW REGISTER = # 2 METERS # # -S- # VELOCITY 3 XXXX.X FT/SEC DP BIT 1 OF HIGH REGISTER = # -7 # 2 METERS/CENTI-SEC - # Page 21 - # -T- -2 # G XXX.XX G SP BIT 1 = 10 G # (MAX 163.83) @@ -846,7 +828,7 @@ # 2 INTEGERS +XXBYY DP BIT 1 OF HIGH REGISTER = # (B IS A BLANK 1 UNIT OF XX # POSITION. DECIMAL BIT 1 OF LOW REGISTER = -# ONLY, DISPLAY, OR 1 UNIT OF YY +# ONLY, DISPLAY OR 1 UNIT OF YY # MONITOR ONLY. CANNOT (EACH REGISTER MUST # BE LOADED.) CONTAIN A POSITIVE INTEGER # (MAX 99B99) LESS THAN 100) @@ -855,9 +837,7 @@ # VELOCITY/2VS XXXXX. FEET/SEC DP FRACTIONAL PART OF # (MAX 51532.) 2VS FEET/SEC # (VS = 25766.1973) - # Page 22 - # -VV- # POSITION8 XXXX.X NAUT MI DP BIT 1 OF LOW REGISTER = # -28 @@ -884,9 +864,9 @@ # Page 23 -# ALARM CODES FOR 504 +# ALARM CODES FOR 504 -# REPORT DEFICIENCIES TO JOHN SUTHERLAND @ MIT 617-864-6900 X1458 +# REPORT DEFICIENCIES TO JOHN SUTHERLAND @ MIT 617-864-6900 X1458 # *9 *18 *60 *25 COLUMN # @@ -913,7 +893,7 @@ # 00207 ISS TURNON REQUEST NOT PRESENT FOR 90 SEC T4RUPT ALARM # 00210 IMU NOT OPERATING IMU MODE SWITCH, IMU-2, R02, P51 ALARM,VARALARM # 00211 COARSE ALIGN ERROR - DRIVE > 2 DEGREES IMU MODE SWITCH ALARM -# 00212 PIPA FAIL BUT PIPA IS NOT BEING USED IMU MODE SWITCH,T4RUPT ALARM +# 00212 PIPA FAIL BUT PIPA IS NOT BEING USED IMU MODE SWITCH,T4RPT ALARM # 00213 IMU NOT OPERATING WITH TURN-ON REQUEST T4RUPT ALARM # 00214 PROGRAM USING IMU WHEN TURNED OFF T4RUPT ALARM # 00215 PREFERRED ORIENTATION NOT SPECIFIED P52,P54 ALARM @@ -922,9 +902,9 @@ # 00401 DESIRED GIMBAL ANGLES YIELD GIMBAL LOCK IMF ALIGN, IMU-2 ALARM # 00404 TARGET OUT OF VIEW - TRUN ANGLE > 90 DEG R52 PRIOLARM # 00405 TWO STARS NOT AVAILABLE P52,P54 ALARM -# 00406 REND NAVIGATION NOT OPERATING P21,R23 ALARM +# 00406 REND NAVIGATION NOT OPERATING R21,R23 ALARM # 00407 AUTO OPTICS REQUEST TRUN ANGLE > 50 DEG. R52 ALARM -# 00421 W-MATRIX OVERFLOW INTEGRV ALARM +# 00421 W-MATRIX OVERFLOW INTEGRV VARALARM # 00430 * INTEG. ABORT DUE TO SUBSURFACE S. V. ALL CALLS TO INTEG POODOO # 00600 IMAGINARY ROOTS ON FIRST ITERATION P32, P72 VARALARM # 00601 PERIGEE ALTITUDE LT PMIN1 P32,P72, VARALARM @@ -934,16 +914,14 @@ # 00605 NUMBER OF ITERATIONS EXCEEDS LOOP MAXIMUM P32,P72,P37 VARALARM # 00606 DV EXCEEDS MAXIMUM P32,P72 VARALARM # 00607 * NO SOLN FROM TIME-THETA OR TIME-RADIUS TIMETHET,TIMERAD POODOO - # Page 24 - # 00610 * LAMBDA LESS THAN UNITY P37 POODOO # 00611 NO TIG FOR GIVEN ELEV ANGLE P34,P74 VARALARM # 00612 STATE VECTOR IN WRONG SPHERE OF INFLUENCE P37 VARALARM # 00613 REENTRY ANGLE OUT OF LIMITS P37 VARALARM # 00777 PIPA FAIL CAUSED ISS WARNING. T4RUPT VARALARM # 01102 CMC SELF TEST ERROR ALARM2 -# 01103 * UNUSED CCS BRANCH EXECUTED ABORT ALARM2 +# 01103 * UNUSED CCS BRANCH EXECUTED ABORT POODOO # 01104 * DELAY ROUTINE BUSY EXEC BAILOUT # 01105 DOWNLINK TOO FAST T4RUPT ALARM # 01106 UPLINK TOO FAST T4RUPT ALARM @@ -1000,7 +978,7 @@ # 00204 PERFORM SPS GIMBAL TRIM # 00403 SWITCH OPTICS TO MANUAL OR ZERO # SWITCH DENOTES CHANGE POSITION OF A CONSOLE SWITCH -# PERFORM DENOTES START OF END OF A TASK +# PERFORM DENOTES START OR END OF A TASK # KEY IN DENOTES KEY IN OF DATA THRU THE DSKY # Page 26 @@ -1013,20 +991,20 @@ # CONJUNCTION WITH VERB04NOUN06 TO REQUEST THE ASTRONAUT TO LOAD INTO # COMPONENT R2 THE OPTION HE DESIRES. -# *9 *17 #52 #11 #25 COLUMN +# *9 *17 #52 #11 #25 COLUMN # # OPTION -# CODE PURPOSE INPUT FOR COMPONENT 2 PROGRAM(S) APPLICABILITY +# CODE PURPOSE INPUT FOR COMPONENT 2 PROGRAM(S) APPLICABILITY # -# 00001 SPECIFY IMU ORIENTATION 1=PREF 2=NOM 3=REFSMMAT P50'S ALL -# 00002 SPECIFY VEHICLE 1=THIS 2=OTHER P21,R30 ALL -# 00003 SPECIFY TRACKING ATTITUDE 1=PREFERRED 2=OTHER R63 ALL -# 00004 SPECIFY RADAR 1=RR 2=LR R04 SUNDANCE + LUMINARY -# 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY -# 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY -# 00007 SPECIFY PROPULSION SYSTEM 1=SPS 2=RCS P37 COLOSSUS -# 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT +G P57 LUMINARY -# 2=TWO BODIES 3=ONE BODY + G -# 00011 SPEC. SEPARATION MONITOR PHASE 1=DELTAV 2=STATE VECTOR UPDATE P46 LUMINARY -# 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY -# ORBIT TO PASS OVER LM +# 00001 SPECIFY IMU ORIENTATION 1=PREF 2=NOM 3=REFSMMAT P50'S ALL +# 00002 SPECIFY VEHICLE 1=THIS 2=OTHER P21,R30 ALL +# 00003 SPECIFY TRACKING ATTITUDE 1=PREFERRED 2=OTHER R63 ALL +# 00004 SPECIFY RADAR 1=RR 2=LR R04 SUNDANCE + LUMINARY +# 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY +# 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY +# 00007 SPECIFY PROPULSION SYSTEM 1=SPS 2=RCS P37 COLOSSUS +# 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT +G P57 LUMINARY +# 2=TWO BODIES 3=ONE BODY + G +# 00011 SPECIFY SEPARATION MONITOR PHASE 1=DELTAV 2=STATE VECTOR UPDATE P46 LUMINARY +# 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY +# ORBIT TO PASS OVER LM