Proof ASSEMBLY_AND_OPERATION_INFORMATION (#337)
This commit is contained in:
cai
James Harris
parent
27e2acf88a
commit
3a9b000cb4
@ -46,7 +46,7 @@
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# PINBALL NOUN TABLES
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# CSM GEOMETRY
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# IMU COMPENSATION PACKAGE
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# PINBALL GAME BUTTONS AND LIGHTS
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# PINBALL GAME BUTTONS AND LIGHTS
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# R60,R62
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# ANGLFIND
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# GIMBAL LOCK AVOIDANCE
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@ -62,7 +62,7 @@
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# STABLE ORBIT - P38-P39
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# TROUBLE
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# P11
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# TP1 SEARCH
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# TPI SEARCH
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# P20-P25
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# P30,P37
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# P32-P33, P72-P73
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@ -77,14 +77,14 @@
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# P37,P70
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# S-BAND ANTENNA FOR CM
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# TVCDAPS
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# TVC INITIALIZE
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# TVCINITIALIZE
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# Page 3
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# TVC EXECUTIVE
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# TVC MASSPROP
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# TVC RESTARTS
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# TVC DAPS
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# TVC STROKE TEST
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# TVC ROLLDAP
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# TVCEXECUTIVE
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# TVCMASSPROP
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# TVCRESTARTS
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# TVCDAPS
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# TVCSTROKETEST
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# TVCROLLDAP
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# MYSUBS
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# RCS-CSM DIGITAL AUTOPILOT
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# AUTOMATIC MANEUVERS
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@ -139,44 +139,44 @@
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# REGULAR VERBS
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# 00 NOT IN USE
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# 01 DISPLAY OCTAL COMP 1 IN R1
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# 02 DISPLAY OCTAL COMP 2 IN R1
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# 03 DISPLAY OCTAL COMP 3 IN R1
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# 04 DISPLAY OCTAL COMP 1,2 IN R1,R2
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# 05 DISPLAY OCTAL COMP 1,2,3 IN R1,R2,R3
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# 06 DISPLAY DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
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# 07 DISPLAY DP DECIMAL IN R1,R2 (TEST ONLY)
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# 00 NOT IN USE
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# 01 DISPLAY OCTAL COMP 1 IN R1
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# 02 DISPLAY OCTAL COMP 2 IN R1
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# 03 DISPLAY OCTAL COMP 3 IN R1
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# 04 DISPLAY OCTAL COMP 1,2 IN R1,R2
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# 05 DISPLAY OCTAL COMP 1,2,3 IN R1,R2,R3
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# 06 DISPLAY DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
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# 07 DISPLAY DP DECIMAL IN R1,R2 (TEST ONLY)
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# 08
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# 09
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# 10
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# 11 MONITOR OCTAL COMP 1 IN R1
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# 12 MONITOR OCTAL COMP 2 IN R1
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# 13 MONITOR OCTAL COMP 3 IN R1
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# 14 MONITOR OCTAL COMP 1,2, IN R1,R2
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# 15 MONITOR OCTAL COMP 1,2,3 IN R1,R2,R3
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# 16 MONITOR DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
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# 17 MONITOR DP DECIMAL IN R1,R2 (TEST ONLY)
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# 11 MONITOR OCTAL COMP 1 IN R1
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# 12 MONITOR OCTAL COMP 2 IN R1
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# 13 MONITOR OCTAL COMP 3 IN R1
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# 14 MONITOR OCTAL COMP 1,2, IN R1,R2
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# 15 MONITOR OCTAL COMP 1,2,3 IN R1,R2,R3
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# 16 MONITOR DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
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# 17 MONITOR DP DECIMAL IN R1,R2 (TEST ONLY)
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# 18
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# 19
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# 20
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# 21 LOAD COMPONENT 1 INTO R1
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# 22 LOAD COMPONENT 2 INTO R2
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# 23 LOAD COMPONENT 3 INTO R3
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# 24 LOAD COMPONENT 1,2 INTO R1,R2
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# 25 LOAD COMPONENT 1,2,3 INTO R1,R2,R3
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# 21 LOAD COMPONENT 1 INTO R1
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# 22 LOAD COMPONENT 2 INTO R2
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# 23 LOAD COMPONENT 3 INTO R3
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# 24 LOAD COMPONENT 1,2 INTO R1,R2
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# 25 LOAD COMPONENT 1,2,3 INTO R1,R2,R3
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# 26
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# 27 DISPLAY FIXED MEMORY
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# 27 DISPLAY FIXED MEMORY
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# 28
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# 29
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# 30 REQUEST EXECUTIVE
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# 31 REQUEST WAITLIST
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# 32 RECYCLE PROGRAM
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# 33 PROCEED WITHOUT DSKY INPUTS
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# 34 TERMINATE FUNCTION
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# 35 TEST LIGHTS
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# 36 REQUEST FRESH START
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# 37 CHANGE PROGRAM (MAJOR MODE)
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# 30 REQUEST EXECUTIVE
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# 31 REQUEST WAITLIST
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# 32 RECYCLE PROGRAM
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# 33 PROCEED WITHOUT DSKY INPUTS
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# 34 TERMINATE FUNCTION
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# 35 TEST LIGHTS
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# 36 REQUEST FRESH START
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# 37 CHANGE PROGRAM (MAJOR MODE)
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# 38
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# 39
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@ -184,80 +184,80 @@
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# EXTENDED VERBS
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# 40 ZERO CDU-S
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# 41 COARSE ALIGN CDU-S
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# 42 FINE ALIGN IMU-S
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# 43 LOAD IMU ATT ERROR METERS
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# 44 SET SURFACE FLAG
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# 45 RESET SURFACE FLAG
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# 46 ESTABLISH G&C CONTROL
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# 47 MOVE LM STATE VECTOR INTO CM STATE VECTOR.
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# 48 REQUEST DAP DATA LOAD ROUTINE (R03)
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# 49 REQUEST CREW DEFINED MANEUVER ROUTINE (R62)
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# 50 PLEASE PERFORM
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# 51 PLEASE MARK
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# 52 MARK ON OFFSET LANDING SITE
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# 53 PLEASE PERFORM ALTERNATE LOS MARK
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# 54 REQUEST RENDEZVOUS BACKUP SIGHTING MARK ROUTINE (R23)
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# 55 INCREMENT AGC TIME (DECIMAL)
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# 56 TERMINATE TRACKING (P20 + P25)
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# 57 REQUEST RENDEZVOUS SIGHTING MARK ROUTINE (R21)
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# 58 RESET STICK FLAG
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# 59 PLEASE CALIBRATE
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# 60 SET ASTRONAUT TOTAL ATTITUDE (N17) TO PRESENT ATTITUDE
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# 61 DISPLAY DAP ATTITUDE ERROR
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# 62 DISPLAY TOTAL ATTITUDE ERROR (WRT N22 (THETAD))
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# 63 DISPLAY TOTAL ASTRONAUT ATTITUDE ERROR (WRT N17 (CPHIX))
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# 64 REQUEST S-BAND ANTENNA ROUTINE
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# 65 OPTICAL VERIFICATION OF PRELAUNCH ALIGNMENT
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# 66 VEHICLES ARE ATTACHED. MOVE THIS VEHICLE STATE TO OTHER VEHICLE.
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# 40 ZERO CDU-S
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# 41 COARSE ALIGN CDU-S
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# 42 FINE ALIGN IMU-S
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# 43 LOAD IMU ATT ERROR METERS
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# 44 SET SURFACE FLAG
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# 45 RESET SURFACE FLAG
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# 46 ESTABLISH G+C CONTROL
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# 47 MOVE LM STATE VECTOR INTO CM STATE VECTOR.
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# 48 REQUEST DAP DATA LOAD ROUTINE (R03)
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# 49 REQUEST CREW DEFINED MANEUVER ROUTINE (R62)
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# 50 PLEASE PERFORM
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# 51 PLEASE MARK
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# 52 MARK ON OFFSET LANDING SITE
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# 53 PLEASE PERFORM ALTERNATE LOS MARK
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# 54 REQUEST RENDEZVOUS BACKUP SIGHTING MARK ROUTINE (R23)
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# 55 INCREMENT AGC TIME (DECIMAL)
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# 56 TERMINATE TRACKING (P20 + P25)
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# 57 REQUEST RENDEZVOUS SIGHTING MARK ROUTINE (R21)
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# 58 RESET STICK FLAG
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# 59 PLEASE CALIBRATE
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# 60 SET ASTRONAUT TOTAL ATTITUDE (N17) TO PRESENT ATTITUDE
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# 61 DISPLAY DAP ATTITUDE ERROR
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# 62 DISPLAY TOTAL ATTITUDE ERROR (WRT N22 (THETAD))
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# 63 DISPLAY TOTAL ASTRONAUT ATTITUDE ERROR (WRT N17 (CPHIX))
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# 64 REQUEST S-BAND ANTENNA ROUTINE
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# 65 OPTICAL VERIFICATION OF PRELAUNCH ALIGNMENT
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# 66 VEHICLES ARE ATTACHED. MOVE THIS VEHICLE STATE TO OTHER VEHICLE.
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# 67
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# 68 CSM STROKE TEST ON
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# 69 CAUSE RESTART
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# 70 UPDATE LIFTOFF TIME
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# 71 UNIVERSAL UPDATE-BLOCK ADR
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# 72 UNIVERSAL UPDATE-SINGLE ADR
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# 73 UPDATE AGC TIME (OCTAL)
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# 74 INITIALIZE ERASABLE DUMP VIA DOWNLINK
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# 75 BACKUP LIFTOFF
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# 76 SET PREFERRED ATTITUDE FLAG
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# 77 RESET PREFERRED ATTITUDE FLAG
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# 78 UPDATE PRELAUNCH AZIMUTH
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# 79 REQUEST LUNAR LANDMARK SELECTION ROUTINE (R35)
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# 80 UPDATE LEM STATE VECTOR
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# 81 UPDATE CSM STATE VECTOR
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# 82 REQUEST ORBIT PARAM DISPLAY (R30)
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# 83 REQUEST REND PARAM DISPLAY (R31)
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# 84 START TARGET DELTA V (R32)
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# 85 REQUEST RENDEZVOUS PARAMETER DISPLAY NO. 2 (R34)
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# 86 REJECT RENDEZVOUS BACKUP SIGHTING MARK
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# 87 SET VHF RANGE FLAG
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# 68 CSM STROKE TEST ON
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# 69 CAUSE RESTART
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# 70 UPDATE LIFTOFF TIME
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# 71 UNIVERSAL UPDATE-BLOCK ADR
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# 72 UNIVERSAL UPDATE-SINGLE ADR
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# 73 UPDATE AGC TIME (OCTAL)
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# 74 INITIALIZE ERASABLE DUMP VIA DOWNLINK
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# 75 BACKUP LIFTOFF
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# 76 SET PREFERRED ATTITUDE FLAG
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# 77 RESET PREFERRED ATTITUDE FLAG
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# 78 UPDATE PRELAUNCH AZIMUTH
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# 79 REQUEST LUNAR LANDMARK SELECTION ROUTINE (R35)
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# 80 UPDATE LEM STATE VECTOR
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# 81 UPDATE CSM STATE VECTOR
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# 82 REQUEST ORBIT PARAM DISPLAY (R30)
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# 83 REQUEST REND PARAM DISPLAY (R31)
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# 84 START TARGET DELTA V (R32)
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# 85 REQUEST RENDEZVOUS PARAMETER DISPLAY NO. 2 (R34)
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# 86 REJECT RENDEZVOUS BACKUP SIGHTING MARK
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# 87 SET VHF RANGE FLAG
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# Page 7
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# 88 RESET VHF RANGE FLAG
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# 89 REQUEST RENDEZVOUS FINAL ATTITUDE ROUTINE (R63)
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# 90 REQUEST RENDEZVOUS OUT OF PLANE DISPLAY ROUTINE (R36)
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# 91 DISPLAY BANK SUM
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# 92 OPERATE IMU PERFORMANCE TEST (P07)
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# 93 ENABLE W MATRIX INITIALIZATION
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# 94 PERFORM CYSLUNAR ATTITUDE MANEUVER (P23)
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# 95 NO UPDATE OF EITHER STATE VECTOR (P20 OR P22)
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# 96 TERMINATE INTEGRATION AND GO TO P00
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# 97 PERFORM ENGINE FAIL PROCEDURE
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# 98 ENABLE TRANSLUNAR INJECT
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# 99 PLEASE ENABLE ENGINE
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# 88 RESET VHF RANGE FLAG
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# 89 REQUEST RENDEZVOUS FINAL ATTITUDE ROUTINE (R63)
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# 90 REQUEST RENDEZVOUS OUT OF PLANE DISPLAY ROUTINE (R36)
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# 91 DISPLAY BANK SUM
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# 92 OPERATE IMU PERFORMANCE TEST (P07)
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# 93 ENABLE W MATRIX INITIALIZATION
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# 94 PERFORM CYSLUNAR ATTITUDE MANEUVER (P23)
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# 95 NO UPDATE OF EITHER STATE VECTOR (P20 OR P22)
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# 96 TERMINATE INTEGRATION AND GO TO P00
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# 97 PERFORM ENGINE FAIL PROCEDURE
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# 98 ENABLE TRANSLUNAR INJECT
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# 99 PLEASE ENABLE ENGINE
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# Page 8
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# IN THE FOLLOWING NOUN LIST THE :NO LOAD: RESTRICTION MEANS THE NOUN
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# CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF
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# SCALE TYPE L (MIN/SEC) OR PP (2 INTEGERS).
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# IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22, OR 23
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# IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22 OR 23
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# MAY BE USED TO LOAD ANY OF THE NOUN:S COMPONENTS WHICH ARE NOT OF THE
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# ABOVE SCALE TYPES.
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# THE :DEC ONLY: RESTRICTION MEANS ONLY DECIMAL OPERATION IS ALLOWED ON
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# EVERY COMPONENT IN THE NOUN. (NOTE THAT :NO LOAD: IMPLIES :DEC ONLY:.)
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# NORMAL NOUNS COMPONENTS SCALE & DECIMAL POINT RESTRICTIONS
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#
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# NORMAL NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
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# 00 NOT IN USE
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# 01 SPECIFY MACHINE ADDRESS (FRACTIONAL) 3COMP .XXXXX FOR EACH
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# 02 SPECIFY MACHINE ADDRESS (WHOLE) 3COMP XXXXX. FOR EACH
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@ -276,7 +276,7 @@
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# 000XX. MIN MUST LOAD 3 COMPS
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# 0XX.XX SEC
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# 12 OPTION CODE 2COMP OCTAL ONLY FOR EACH
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# (USED BY EXTENDED VERBS ONLY)
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# (USED BY EXTENDED VERBS ONLY)
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# 13 TIG OF CDH 3COMP 00XXX. HRS DEC ONLY
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# 000XX. MIN MUST LOAD 3 COMPS
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# 0XX.XX SEC
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@ -297,16 +297,12 @@
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# 0XX.XX SEC
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# 25 CHECKLIST 3COMP XXXXX. FOR EACH
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# (USED WITH PLEASE PERFORM ONLY)
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# Page 9
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# 26 PRIORITY/DELAY, ADRES, BBCON 3COMP OCTAL ONLY FOR EACH
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# 27 SELF TEST ON/OFF SWITCH 1COMP XXXXX.
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# 28 SPARE
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# 29 XSM LAUNCH AZIMUTH 1COMP XXX.XX DEG DEC ONLY
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# Page 10
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# 30 TARGET CODES 3COMP XXXXX. FOR EACH
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# 31 TIME OF LANDING SITE 3COMP 00XXX. HRS DEC ONLY
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# 000XX. MIN MUST LOAD 3 COMPS
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@ -338,7 +334,7 @@
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# Page 11
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# MIXED NOUNS COMPONENTS SCALE & DECIMAL POINT RESTRICTIONS
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# MIXED NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
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#
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# 40 TIME FROM IGNITION/CUTOFF 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
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# VG, XXXX.X FT/SEC
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@ -361,7 +357,7 @@
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# 47 THIS VEHICLE WEIGHT 2COMP XXXXX. LBS DEC ONLY
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# OTHER VEHICLE WEIGHT XXXXX. LBS
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# 48 PITCH TRIM 2COMP XXX.XX DEG DEC ONLY
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# YAW TRIM, XXX.XX DEG
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# YAW TRIM, XXX.XX DEG
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# 49 DELTA R 3COMP XXXX.X NAUT MI DEC ONLY
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# DELTA V XXXX.X FT/SEC
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# VHF OR OPTICS CODE XXXXX.
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@ -373,7 +369,7 @@
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# 52 CENTRAL ANGLE OF ACTIVE VEHICLE 1COMP XXX.XX DEG
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# 53 RANGE, 3COMP XXX.XX NAUT MI DEC ONLY
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# RANGE RATE, XXXX.X FT/SEC
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# PHI XXX.X DEG
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# PHI XXX.XX DEG
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# 54 RANGE, 3COMP XXX.XX NAUT MI DEC ONLY
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# RANGE RATE, XXXX.X FT/SEC
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# THETA XXX.XX DEG
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@ -388,9 +384,7 @@
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# DELTA V TPF XXXX.X FT/SEC
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# 59 DELTA VELOCITY LOS 3COMP XXXX.X FT/SEC FOR EA. DEC ONLY
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# 60 GMAX, 3COMP XXX.XX G DEC ONLY
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# Page 12
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# VPRED, XXXXX. FT/SEC
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# GAMMA EI XXX.XX DEG
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# 61 IMPACT LATITUDE, 3COMP XXX.XX DEG DEC ONLY
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@ -399,7 +393,7 @@
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# 62 INERTIAL VEL MAG (VI), 3COMP XXXXX. FT/SEC DEC ONLY
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# ALT RATE CHANGE (HDOT), XXXXX. FT/SEC
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# ALT ABOVE PAD RADIUS (H) XXXX.X NAUT MI
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# 63 RANGE 297,431 TO SPLASH (RTGO), 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
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# 63 RANGE 297,431 TO SPLASH (RTGO), 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
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# PREDICTED INERT VEL (VIO), XXXXX. FT/SEC
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# TIME FROM 297,431 (TFE), XXBXX MIN/SEC
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# 64 DRAG ACCELERATION, 3COMP XXX.XX G DEC ONLY
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@ -417,7 +411,7 @@
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# 68 COMMAND BANK ANGLE (BETA), 3COMP XXX.XX DEG DEC ONLY
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# INERTIAL VELOCITY (VI), XXXXX. FT/SEC
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# ALT RATE CHANGE (RDOT) XXXXX. FT/SEC
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# 69 BETA 3COMP XXX.XX DEG
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# 69 BETA 3COMP XXX.XX DEG DEC ONLY
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# DL XXX.XX G
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# VL XXXXX. FT/SEC
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# 70 STAR CODE, 3COMP OCTAL ONLY
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@ -441,9 +435,7 @@
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# 78 SPARE
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# 79 SPARE
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# 80 TIME FROM IGNITION/CUTOFF 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
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# Page 13
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# VG XXXXX. FT/SEC
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# DELTA V (ACCUMULATED) XXXXX. FT/SEC
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# 81 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
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@ -451,7 +443,7 @@
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# 83 DELTA V (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
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# 84 DELTA V (OTHER VEHICLE) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
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# 85 VG (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
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# 86 DELTA V (LV) 3COMP XXXXX. FT/SEC FOR EACH DEC ONLY
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# 86 DELTA V(LV) 3COMP XXXXX. FT/SEC FOR EACH DEC ONLY
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# 87 MARK DATA SHAFT, 2COMP XXX.XX DEG
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# TRUNION XX.XXX DEG
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# 88 HALF UNIT SUN OR PLANET VECTOR 3COMP .XXXXX FOR EACH DEC ONLY
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@ -468,7 +460,7 @@
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# 93 DELTA GYRO ANGLES 3COMP XX.XXX DEG FOR EACH
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# 94 NEW OPTICS ANGLES SHAFT 2COMP XXX.XX DEG
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# TRUNNION XX.XXX DEG
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# 95 PREFERRED ATTITUDE ICDU ANGLES 3COMP XXX.XX FOR EACH
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# 95 PREFERRED ATTITUDE ICDU ANGLES 3COMP XXX.XX FOR FOR EACH
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# 96 +X-AXIS ATTITUDE ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
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# 97 SYSTEM TEST INPUTS 3COMP XXXXX. FOR EACH
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# 98 SYSTEM TEST RESULTS AND INPUTS 3COMP XXXXX.
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@ -521,7 +513,7 @@
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# 34 DSPTEM1 K
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# 35 TTOGO K
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# 36 TIME2 K
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# 37 TTP1 K
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# 37 TTPI K
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# 38 TET K
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# 39 T3TOT4 K
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@ -577,9 +569,7 @@
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# 57 1 DELTAR Q
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# 58 1 POSTTPI Q
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# 2 DELVTPI S
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# Page 16
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# 3 DELVTPF S
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# 59 1 DVLOS S
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# 2 DVLOS +2 S
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@ -630,9 +620,7 @@
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# 75 1 DIFFALT Q
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# 2 T1TOT2 L
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# 3 T2TOT3 L
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# Page 17
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# 76 SPARE
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# 77 SPARE
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# 78 SPARE
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@ -660,9 +648,9 @@
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# 3 DELVLVC +4 P
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# 87 1 MRKBUF1 +3 D
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# 2 MRKBUF1 +5 J
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# 88 1 STARSAV ZZ
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||||
# 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
|
||||
|
||||
Loading…
Reference in New Issue
Block a user