2016-07-07 08:47:26 +00:00
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# Copyright: Public domain.
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# Filename: ASSEMBLY_AND_OPERATION_INFORMATION.agc
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# Purpose: Part of the source code for Colossus 2A, AKA Comanche 055.
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# It is part of the source code for the Command Module's (CM)
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# Apollo Guidance Computer (AGC), for Apollo 11.
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# Assembler: yaYUL
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# Contact: Ron Burkey <info@sandroid.org>.
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# Website: www.ibiblio.org/apollo.
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# Mod history: 2009-05-05 RSB Adapted from the Colossus249/ file of the
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# same name, using Comanche055 page images.
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#
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# This source code has been transcribed or otherwise adapted from digitized
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# images of a hardcopy from the MIT Museum. The digitization was performed
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# by Paul Fjeld, and arranged for by Deborah Douglas of the Museum. Many
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# thanks to both. The images (with suitable reduction in storage size and
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# consequent reduction in image quality as well) are available online at
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# www.ibiblio.org/apollo. If for some reason you find that the images are
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# illegible, contact me at info@sandroid.org about getting access to the
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# (much) higher-quality images which Paul actually created.
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#
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# Notations on the hardcopy document read, in part:
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#
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# Assemble revision 055 of AGC program Comanche by NASA
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# 2021113-051. 10:28 APR. 1, 1969
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#
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# This AGC program shall also be referred to as
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# Colossus 2A
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# Page 2
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# ASSEMBLY AND OPERATIONS INFORMATION
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# TAGS FOR RELATIVE SETLOC AND BLANK BANK CARDS
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# SUBROUTINE CALLS
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# COMERASE
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# ERASABLE ASSIGNMENTS
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# COMAID
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# INTERRUPT LEAD INS
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# T4RUPT PROGRAM
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# DOWNLINK LISTS
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# FRESH START AND RESTART
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# RESTART TABLES
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# SXTMARK
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# EXTENDED VERBS
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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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# R60,R62
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# ANGLFIND
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# GIMBAL LOCK AVOIDANCE
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# KALCMANU STEERING
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# SYSTEM TEST STANDARD LEAD INS
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# IMU CALIBRATION AND ALIGNMENT
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# COMEKISS
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# GROUND TRACKING DETERMINATION PROGRAM -- P21
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# P34-P35, P74-P75
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# R31
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# P76
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# R30
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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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# P20-P25
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# P30,P37
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# P40-P47
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# P51-P53
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# LUNAR AND SOLAR EPHEMERIDES SUBROUTINES
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# P61-P67
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# SERVICER207
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# ENTRY LEXICON
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# REENTRY CONTROL
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# CM BODY ATTITUDE
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# P37,P70
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# S-BAND ANTENNA FOR CM
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# LUNAR LANDMARK SELECTION FOR CM
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# TVCDAPS
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# TVC INITIALIZE
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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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# MYSUBS
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# RCS-CSM DIGITAL AUTOPILOT
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# AUTOMATIC MANEUVERS
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# RCS-CSM DAP EXECUTIVE PROGRAMS
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# JET SELECTION LOGIC
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# CM ENTRY DIGITAL AUTOPILOT
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# CHIEFTAN
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# DOWN-TELEMETRY PROGRAM
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# INTER-BANK COMMUNICATION
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# INTERPRETER
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# FIXED-FIXED CONSTANT POOL
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# INTERPRETIVE CONSTANTS
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# SINGLE PRECISION SUBROUTINES
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# EXECUTIVE
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# WAITLIST
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# LATITUDE LONGITUDE SUBROUTINES
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# PLANETARY INERTIAL ORIENTATION
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# MEASUREMENT INCORPORATION
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# CONIC SUBROUTINES
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# INTEGRATION INITIALIZATION
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# ORBITAL INTEGRATION
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# INFLIGHT ALIGNMENT ROUTINES
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# POWERED FLIGHT SUBROUTINES
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# TIME OF FREE FALL
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# STAR TABLES
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# AGC BLOCK TWO SELF-CHECK
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# PHASE TABLE MAINTENANCE
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# RESTARTS ROUTINE
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# IMU MODE SWITCHING ROUTINES
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# KEYRUPT, UPRUPT
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# DISPLAY INTERFACE ROUTINES
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# SERVICE ROUTINES
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# ALARM AND ABORT
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# UPDATE PROGRAM
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# RTB OP CODES
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# SYMBOL TABLE LISTING
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2016-07-11 12:35:15 +00:00
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# UNREFERENCED SYMBOL LISTING
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2016-07-07 08:47:26 +00:00
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# ERASABLE & EQUALS CROSS-REFERENCE TABLE
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# SUMMARY OF SYMBOL TABLE LISTINGS
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# MEMORY TYPE & AVAILABILITY DISPLAY
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# COUNT TABLE
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# PARAGRAPHS GENERATED FOR THIS DISPLAY
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# Page 4
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# OCTAL LISTING
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# OCCUPIED LOCATIONS TABLE
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# SUBROS CALLED & PROGRAM STATUS
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# Page 5
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# VERB LIST FOR CSM
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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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# 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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# 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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# 26
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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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# 38
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# 39
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# Page 6
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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 REQUES 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 ROUTIEN (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 (W.R.T. N22 (THETAD))
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# 63 DISPLAY TOTAL ASTRONAUT ATTITUDE ERROR (W.R.T. 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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# 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 SYSLUNAR 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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# 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. (NOT THAT 'NO LOAD' IMLIES 'DEC ONLY'.)
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# NORMAL NOUNS COMPONENTS SCALE & DECIMAL POINT RESTRICTION
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#
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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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# 03 SPECIFY MACHINE ADDRESS (DEGREES) 3COMP XXX.XX DEG FOR EACH
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# 04 SPARE
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# 05 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
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# 06 OPTION CODE 2COMP OCTAL ONLY FOR EACH
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# LOADING NOUN 07 WILL SET OR RESET SELECTED BITS IN ANY ERASABLE REGISTER.
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# 07 ECADR OF WORD TO BE MODIFIED 3COMP OCTAL ONLY FOR EACH
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# ONES FOR BITS TO BE MODIFIED
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# 1 TO SET OR 0 TO RESET SELECTED BITS
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# 08 ALARM DATA 3COMP OCTAL ONLY FOR EACH
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# 09 ALARM CODES 3COMP OCTAL ONLY FOR EACH
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# 10 CHANNEL TO BE SPECIFIED 1COMP OCTAL ONLY
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# 11 TIG OF CSI 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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# 12 OPTION CODE 2COMP OCTAL ONLY FOR EACH
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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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# 14 SPARE
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# 15 INCREMENT MACHINE ADDRESS 1COMP OCTAL ONLY
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# 16 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
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# (USED BY EXTENDED VERBS ONLY) 000XX. MIN MUST LOAD 3 COMPS
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# 0XX.XX SEC
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# 17 ASTRONAUT TOTAL ATTITUDE 3COMP XXX.XX DEG FOR EACH
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# 18 AUTO MANEUVER BALL ANGLES 3COMP XXX.XX DEG FOR EACH
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# 19 BYPASS ATTITUDE TRIM MANEUVER 3COMP XXX.XX DEG FOR EACH
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# 20 ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
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# 21 PIPAS 3COMP XXXXX. PULSES FOR EACH
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# 22 NEW ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
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# 23 SPARE
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# 24 DELTA TIME FOR AGC CLOCK 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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# 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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# 0XX.XX SEC
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# 32 TIME FROM PERIGEE 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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# 33 TIME OF IGNITION 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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# 34 TIME OF EVENT 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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# 35 TIME FROM EVENT 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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# 36 TIME OF AGC CLOCK 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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# 37 TIG OF TPI 3COMP 00XXX. HRS DEC ONLY
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# 000XX. MIN MUST LOAD 3 COMPS
|
|
|
|
# 0XX.XX SEC
|
|
|
|
# 38 TIME OF STATE VECTOR 3COMP 00XXX. HRS DEC ONLY
|
|
|
|
# 000XX. MIN MUST LOAD 3 COMPS
|
|
|
|
# 0XX.XX SEC
|
|
|
|
# 39 DELTA TIME FOR TRANSFER 3COMP 00XXX. HRS DEC ONLY
|
|
|
|
# 000XX. MIN MUST LOAD 3 COMPS
|
|
|
|
# 0XX.XX SEC
|
|
|
|
|
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|
# Page 11
|
|
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|
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|
|
|
# MIXED NOUNS COMPONENTS SCALE & DECIMAL POINT RESTRICTION
|
|
|
|
#
|
|
|
|
# 40 TIME FROM IGNITION/CUTOFF 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
|
|
|
|
# VG XXXX.X FT/SEC
|
|
|
|
# DELTA V (ACCUMULATED) XXXX.X FT/SEC
|
|
|
|
# 41 TARGET AZIMUTH 2COMP XXX.XX DEG
|
|
|
|
# ELEVATION XX.XXX DEG
|
|
|
|
# 42 APOGEE 3COMP XXXX.X NAUT MI DEC ONLY
|
|
|
|
# PERIGEE XXXX.X NAUT MI
|
|
|
|
# DELTA V (REQUIRED) XXXX.X FT/SEC
|
|
|
|
# 43 LATITUDE 3COMP XXX.XX DEG DEC ONLY
|
|
|
|
# LONGITUDE XXX.XX DEG
|
|
|
|
# ALTITUDE XXXX.X NAUT MI
|
|
|
|
# 44 APOGEE 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
|
|
|
|
# PERIGEE XXXX.X NAUT MI
|
|
|
|
# TFF XXBXX MIN/SEC
|
|
|
|
# 45 MARKS (VHF - OPTICS) 3COMP +XXBXX NO LOAD, DEC ONLY
|
|
|
|
# TFI OF NEXT BURN XXBXX MIN/SEC
|
|
|
|
# MGA XXX.XX DEG
|
|
|
|
# 46 AUTOPILOT CONFIGURATION 2COMP OCTAL ONLY FOR EACH
|
|
|
|
# 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
|
|
|
|
# 49 DELTA R 3COMP XXXX.X NAUT MI DEC ONLY
|
|
|
|
# DELTA V XXXX.X FT/SEC
|
|
|
|
# VHF OR OPTICS CODE XXXXX.
|
|
|
|
# 50 SPLASH ERROR 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
|
|
|
|
# PERIGEE XXXX.X NAUT MI
|
|
|
|
# TFF XXBXX MIN/SEC
|
|
|
|
# 51 S-BAND ANTENNA ANGLES PITCH 2COMP XXX.XX DEG DEC ONLY
|
|
|
|
# YAW XXX.XX DEG
|
|
|
|
# 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
|
|
|
|
# 54 RANGE 3COMP XXX.XX NAUT MI DEC ONLY
|
|
|
|
# RANGE RATE XXXX.X FT/SEC
|
|
|
|
# THETA XXX.XX DEG
|
|
|
|
# 55 PERIGEE CODE 3COMP XXXXX. DEC ONLY
|
|
|
|
# ELEVATION ANGLE XXX.XX DEG
|
|
|
|
# CENTRAL ANGLE OF PASSIVE VEHICLE XXX.XX DEG
|
|
|
|
# 56 REENTRY ANGLE 2COMP XXX.XX DEG DEC ONLY
|
|
|
|
# DELTA V XXXXX. FT/SEC
|
|
|
|
# 57 DELTA R 1COMP XXXX.X NAUT MI DEC ONLY
|
|
|
|
# 58 PERIGEE ALT (POST TPI) 3COMP XXXX.X NAUT MI DEC ONLY
|
|
|
|
# DELTA V TPI XXXX.X FT/SEC
|
|
|
|
# DELTA V TPF XXXX.X FT/SEC
|
|
|
|
# 59 DELTA VELOCITY LOS 3COMP XXXX.X FT/SEC FOR EACH 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
|
|
|
|
# IMPACT LONGITUDE XXX.XX DEG
|
|
|
|
# HEADS UP/DOWN +/- 00001
|
|
|
|
# 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
|
|
|
|
# PREDICTED INERT VEL (VIO) XXXXX. FT/SEC
|
|
|
|
# TIME FROM 297,431 (TFE) XXBXX MIN/SEC
|
|
|
|
# 64 DRAG ACCELERATION 3COMP XXX.XX G DEC ONLY
|
|
|
|
# INERTIAL VELOCITY (VI) XXXXX. FT/SEC
|
|
|
|
# RANGE TO SPLASH XXXX.X NAUT MI
|
|
|
|
# 65 SAMPLED AGC TIME 3COMP 00XXX. HRS DEC ONLY
|
|
|
|
# (FETCHED IN INTERRUPT) 000XX. MIN
|
|
|
|
# 0XX.XX SEC
|
|
|
|
# 66 COMMAND BANK ANGLE (BETA) 3COMP XXX.XX DEG DEC ONLY
|
|
|
|
# CROSS RANGE ERROR XXXX.X NAUT MI
|
|
|
|
# DOWN RANGE ERROR XXXX.X NAUT MI
|
|
|
|
# 67 RANGE TO TARGET 3COMP XXXX.X NAUT MI DEC ONLY
|
|
|
|
# PRESENT LATITUDE XXX.XX DEG
|
|
|
|
# PRESENT LONGITUDE XXX.XX DEG
|
|
|
|
# 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
|
|
|
|
# DL XXX.XX G
|
|
|
|
# VL XXXXX. FT/SEC
|
|
|
|
# 70 STAR CODE 3COMP OCTAL ONLY
|
|
|
|
# LANDMARK DATA OCTAL ONLY
|
|
|
|
# HORIZON DATA OCTAL ONLY
|
|
|
|
# 71 STAR CODE 3COMP OCTAL ONLY
|
|
|
|
# LANDMARK DATA OCTAL ONLY
|
|
|
|
# HORIZON DATA OCTAL ONLY
|
|
|
|
# 72 DELT ANG 3COMP XXX.XX DEG DEC ONLY
|
|
|
|
# 73 ALTITUDE 3COMP XXXXXB. NAUT MI
|
|
|
|
# VELOCITY XXXXX. FT/SEC
|
|
|
|
# FLIGHT PATH ANGLE XXX.XX DEG
|
|
|
|
# 74 COMMAND BANK ANGLE (BETA) 3COMP XXX.XX DEG
|
|
|
|
# INERTIAL VELOCITY (VI) XXXXX. FT/SEC
|
|
|
|
# DRAG ACCELERATION XXX.XX G
|
|
|
|
# 75 DELTA ALTITUDE CDH 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
|
|
|
|
# DELTA TIME (CDH-CSI OR TPI-CDH) XXBXX MIN/SEC
|
|
|
|
# DELTA TIME (TPI-CDH OR TPI-NOMTPI) XXBXX MIN/SEC
|
|
|
|
# 76 SPARE
|
|
|
|
# 77 SPARE
|
|
|
|
# 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
|
|
|
|
# 82 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
|
|
|
|
# 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
|
|
|
|
# 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
|
|
|
|
# 89 LANDMARK LATITUDE 3COMP XX.XXX DEG DEC ONLY
|
|
|
|
# LONGITUDE/2 XX.XXX DEG
|
|
|
|
# ALTITUDE XXX.XX NAUT MI
|
|
|
|
# 90 Y 3COMP XXX.XX NM DEC ONLY
|
|
|
|
# Y DOT XXXX.X FPS
|
|
|
|
# PSI XXX.XX DEG
|
|
|
|
# 91 OCDU ANGLES SHAFT 2COMP XXX.XX DEG
|
|
|
|
# TRUNION XX.XXX DEG
|
|
|
|
# 92 NEW OPTICS ANGLES SHAFT 2COMP XXX.XX DEG
|
|
|
|
# TRUNON XX.XXX DEG
|
|
|
|
# 93 DELTA GYRO ANGLES 3COMP XX.XXX DEG FOR EACH
|
|
|
|
# 94 NEW OPTICS ANGLES SHAFT 2COMP XXX.XX DEG
|
|
|
|
# TRUNION XX.XXX DEG
|
|
|
|
# 95 PREFERRED ATTITUDE ICDU ANGLES 3COMP XXX.XX 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.
|
|
|
|
# .XXXXX
|
|
|
|
# XXXXX.
|
|
|
|
# 99 RMS IN POSITION 3COMP XXX.XX NAUT MI DEC ONLY
|
|
|
|
# RMS IN VELOCITY XXXX.X FT/SEC
|
|
|
|
# RMS OPTION XXXXX.
|
|
|
|
|
|
|
|
# Page 14
|
|
|
|
|
|
|
|
# REGISTERS AND SCALING FOR NORMAL NOUNS
|
|
|
|
#
|
|
|
|
# NOUN REGISTER SCALE TYPE
|
|
|
|
#
|
|
|
|
# 00 NOT IN USE
|
|
|
|
# 01 SPECIFY ADDRESS H
|
|
|
|
# 02 SPECIFY ADDRESS C
|
|
|
|
# 03 SPECIFY ADDRESS D
|
|
|
|
# 04 SPARE
|
|
|
|
# 05 DSPTEM1 H
|
|
|
|
# 06 OPTION1 A
|
|
|
|
# 07 XREG A
|
|
|
|
# 08 ALMCADR A
|
|
|
|
# 09 FAILREG A
|
|
|
|
# 10 SPECIFY CHANNEL A
|
|
|
|
# 11 TCSI K
|
|
|
|
# 12 OPTIONX A
|
|
|
|
# 13 TCDH K
|
|
|
|
# 14 SPARE
|
|
|
|
# 15 INCREMENT ADDRESS A
|
|
|
|
# 16 DSPTEMX C
|
|
|
|
# 17 CPHIX D
|
|
|
|
# 18 THETAD D
|
|
|
|
# 19 THETAD D
|
|
|
|
# 20 CDUX D
|
|
|
|
# 21 PIPAX C
|
|
|
|
# 22 THETAD D
|
|
|
|
# 23 SPARE
|
|
|
|
# 24 DSPTEM2 +1 K
|
|
|
|
# 25 DSPTEM1 C
|
|
|
|
# 26 DSPTEM1 A
|
|
|
|
# 27 SMODE C
|
|
|
|
# 28 SPARE
|
|
|
|
# 29 DSPTEM1 D
|
|
|
|
# 30 DSPTEM1 C
|
|
|
|
# 31 DSPTEM1 K
|
|
|
|
# 32 -TPER K
|
|
|
|
# 33 TIG K
|
|
|
|
# 34 DSPTEM1 K
|
|
|
|
# 35 TTOGO K
|
|
|
|
# 36 TIME2 K
|
|
|
|
# 37 TTP1 K
|
|
|
|
# 38 TET K
|
|
|
|
# 39 T3TOT4 K
|
|
|
|
|
|
|
|
# Page 15
|
|
|
|
|
|
|
|
# REGISTERS AND SCALING FOR MIXED NOUNS
|
|
|
|
#
|
|
|
|
# NOUN COMP REGISTER SCALE TYPE
|
|
|
|
#
|
|
|
|
# 40 1 TTOGO L
|
|
|
|
# 2 VGDISP S
|
|
|
|
# 3 DVTOTAL S
|
|
|
|
# 41 1 DSPTEM1 D
|
|
|
|
# 2 DSPTEM1 +1 E
|
|
|
|
# 42 1 HAPO Q
|
|
|
|
# 2 HPER Q
|
|
|
|
# 3 VGDISP S
|
|
|
|
# 43 1 LAT H
|
|
|
|
# 2 LONG H
|
|
|
|
# 3 ALT Q
|
|
|
|
# 44 1 HAPOX Q
|
|
|
|
# 2 HPERX Q
|
|
|
|
# 3 TFF L
|
|
|
|
# 45 1 VHFCNT PP
|
|
|
|
# 2 TTOGO L
|
|
|
|
# 3 +MGA H
|
|
|
|
# 46 1 DAPDATR1 A
|
|
|
|
# 2 DAPDATR2 A
|
|
|
|
# 47 1 CSMMASS KK
|
|
|
|
# 2 LEMMASS KK
|
|
|
|
# 48 1 PACTOFF FF
|
|
|
|
# 2 YACTOFF FF
|
|
|
|
# 49 1 N49DISP Q
|
|
|
|
# 2 N49DISP +2 S
|
|
|
|
# 3 N49DISP +4 C
|
|
|
|
# 50 1 RSP-RREC LL
|
|
|
|
# 2 HPERX Q
|
|
|
|
# 3 TFF L
|
|
|
|
# 51 1 RHOSB H
|
|
|
|
# 2 GAMMASB H
|
|
|
|
# 52 1 ACTCENT H
|
|
|
|
# 53 1 RANGE JJ
|
|
|
|
# 2 RRATE S
|
|
|
|
# 3 RTHETA H
|
|
|
|
# 54 1 RANGE JJ
|
|
|
|
# 2 RRATE S
|
|
|
|
# 3 RTHETA H
|
|
|
|
# 55 1 NN1 C
|
|
|
|
# 2 ELEV H
|
|
|
|
# 3 CENTANG H
|
|
|
|
# 56 1 RTEGAM2D H
|
|
|
|
# 2 RTEDVD P
|
|
|
|
# 57 1 DELTAR Q
|
|
|
|
# 58 1 POSTTPI Q
|
|
|
|
# 2 DELVTPI S
|
|
|
|
|
|
|
|
# Page 16
|
|
|
|
|
|
|
|
# 3 DELVTPF S
|
|
|
|
# 59 1 DVLOS S
|
|
|
|
# 2 DVLOS +2 S
|
|
|
|
# 3 DVLOS +4 S
|
|
|
|
# 60 1 GMAX T
|
|
|
|
# 2 VPRED P
|
|
|
|
# 3 GAMMAEI H
|
|
|
|
# 61 1 LAT (SPL) H
|
|
|
|
# 2 LNG (SPL) H
|
|
|
|
# 3 HEADSUP C
|
|
|
|
# 62 1 VMAGI P
|
|
|
|
# 2 HDOT P
|
|
|
|
# 3 ALTI Q
|
|
|
|
# 63 1 RTGO LL
|
|
|
|
# 2 VIO P
|
|
|
|
# 3 TTE L
|
|
|
|
# 64 1 D MM
|
|
|
|
# 2 VMAGI P
|
|
|
|
# 3 RTGON64 LL
|
|
|
|
# 65 1 SAMPTIME K
|
|
|
|
# 2 SAMPTIME K
|
|
|
|
# 3 SAMPTIME K
|
|
|
|
# 66 1 ROLLC H
|
|
|
|
# 2 XRNGERR VV
|
|
|
|
# 3 DNRNGERR LL
|
|
|
|
# 67 1 RTGON67 LL
|
|
|
|
# 2 LAT H
|
|
|
|
# 3 LONG H
|
|
|
|
# 68 1 ROLLC H
|
|
|
|
# 2 VMAGI P
|
|
|
|
# 3 RDOT UU
|
|
|
|
# 69 1 ROLLC H
|
|
|
|
# 2 Q7 MM
|
|
|
|
# 3 VL UU
|
|
|
|
# 70 1 STARCODE A
|
|
|
|
# 2 LANDMARK A
|
|
|
|
# 3 HORIZON A
|
|
|
|
# 71 1 STARCODE A
|
|
|
|
# 2 LANDMARK A
|
|
|
|
# 3 HORIZON A
|
|
|
|
# 72 1 THETZERO H
|
|
|
|
# 73 1 P21ALT Q (MEMORY/100 TO DISPLAY TENS N.M.)
|
|
|
|
# 2 P21VEL P
|
|
|
|
# 3 P21GAM H
|
|
|
|
# 74 1 ROLLC H
|
|
|
|
# 2 VMAGI P
|
|
|
|
# 3 D MM
|
|
|
|
# 75 1 DIFFALT Q
|
|
|
|
# 2 T1TOT2 L
|
|
|
|
# 3 T2TOT3 L
|
|
|
|
|
|
|
|
# Page 17
|
|
|
|
|
|
|
|
# 76 SPARE
|
|
|
|
# 77 SPARE
|
|
|
|
# 78 SPARE
|
|
|
|
# 79 SPARE
|
|
|
|
# 80 1 TTOGO L
|
|
|
|
# 2 VGDISP P
|
|
|
|
# 3 DVTOTAL P
|
|
|
|
# 81 1 DELVLVC S
|
|
|
|
# 2 DELVLVC +2 S
|
|
|
|
# 3 DELVLVC +4 S
|
|
|
|
# 82 1 DELVLVC S
|
|
|
|
# 2 DELVLVC +2 S
|
|
|
|
# 3 DELVLVC +4 S
|
|
|
|
# 83 1 DELVIMU S
|
|
|
|
# 2 DELVIMU +2 S
|
|
|
|
# 3 DELVIMU +4 S
|
|
|
|
# 84 1 DELVOV S
|
|
|
|
# 2 DELVOV +2 S
|
|
|
|
# 3 DELVOV +4 S
|
|
|
|
# 85 1 VGBODY S
|
|
|
|
# 2 VGBODY +2 S
|
|
|
|
# 3 VGBODY +4 S
|
|
|
|
# 86 1 DELVLVC P
|
|
|
|
# 2 DELVLVC +2 P
|
|
|
|
# 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
|
|
|
|
# 89 1 LANDLAT G
|
|
|
|
# 2 LANDLONG G
|
|
|
|
# 3 LANDALT JJ
|
|
|
|
# 90 1 RANGE JJ
|
|
|
|
# 2 RRATE S
|
|
|
|
# 3 RTHETA H
|
|
|
|
# 91 1 CDUS D
|
|
|
|
# 2 CDUT J
|
|
|
|
# 92 1 SAC D
|
|
|
|
# 2 PAC J
|
|
|
|
# 93 1 OGC G
|
|
|
|
# 2 OGC +2 G
|
|
|
|
# 3 OGC +4 G
|
|
|
|
# 94 1 MRKBUF1 +3 D
|
|
|
|
# 2 MRKBUF1 +5 J
|
|
|
|
# 95 1 PRAXIS D
|
|
|
|
# 2 PRAXIS +1 D
|
|
|
|
# 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
|
|
|
|
# 3 DSPTEM1 +2 C
|
|
|
|
# 98 1 DSPTEM2 C
|
|
|
|
# 2 DSPTEM2 +1 B
|
|
|
|
# 3 DSPTEM2 +2 C
|
|
|
|
# 99 1 WWPOS XX
|
|
|
|
# 2 WWVEL YY
|
|
|
|
# 3 WWOPT C
|
|
|
|
|
|
|
|
# Page 19
|
|
|
|
|
|
|
|
# NOUN SCALES AND FORMATS
|
|
|
|
#
|
|
|
|
# -SCALE TYPE- PRECISION
|
|
|
|
# UNITS DECIMAL FORMAT -- AGC FORMAT
|
|
|
|
# ------------ -------------- -- ----------
|
|
|
|
#
|
|
|
|
# -A-
|
|
|
|
# OCTAL XXXXX SP OCTAL
|
|
|
|
#
|
|
|
|
# -B- -14
|
|
|
|
# FRACTIONAL .XXXXX SP BIT 1 = 2 UNITS
|
|
|
|
# (MAX .99996)
|
|
|
|
#
|
|
|
|
# -C-
|
|
|
|
# WHOLE XXXXX. SP BIT 1 = 1 UNIT
|
|
|
|
# (MAX 16383.)
|
|
|
|
#
|
|
|
|
# -D- 15
|
|
|
|
# CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360/2 DEGREES
|
|
|
|
# (MAX 359.99) (USES 15 BITS FOR MAGNI-
|
|
|
|
# TUDE AND 2'S COMP.)
|
|
|
|
#
|
|
|
|
# -E- 14
|
|
|
|
# ELEVATION DEGREES XX.XXX DEGREES SP BIT 1 = 90/2 DEGREES
|
|
|
|
# (MAX 89.999)
|
|
|
|
#
|
|
|
|
# -F- 14
|
|
|
|
# DEGREES (180) XXX.XX DEGREES SP BIT 1 = 180/2 DEGREES
|
|
|
|
# (MAX 179.99)
|
|
|
|
#
|
|
|
|
# -G-
|
|
|
|
# DP DEGREES (90) XX.XXX DEGREES DP BIT 1 OF LOW REGISTER =
|
|
|
|
# 28
|
|
|
|
# 360/2 DEGREES
|
|
|
|
#
|
|
|
|
# -H-
|
|
|
|
# DP DEGREES (360) XXX.XX DEGREES DP BIT 1 OF LOW REGISTER =
|
|
|
|
# (MAX 359.99) 28
|
|
|
|
# 360/2 DEGREES
|
|
|
|
#
|
|
|
|
# -J- 15
|
|
|
|
# Y OPTICS DEGREES XX.XXX DEGREES SP BIT 1 = 90/2 DEGREES
|
|
|
|
# (BIAS OF 19.775 (USES 15 BITS FOR MAGNI-
|
|
|
|
# DEGREES ADDED FOR TUDE AND S'S COMP.)
|
|
|
|
# DISPLAY, SUBTRACTED
|
|
|
|
# FOR LOAD.)
|
|
|
|
# NOTE: NEGATIVE NUM-
|
|
|
|
# BERS CANNOT BE
|
|
|
|
# LOADED.
|
|
|
|
#
|
|
|
|
# -K-
|
|
|
|
|
|
|
|
# Page 20
|
|
|
|
|
|
|
|
# TIME (HR, MIN, SEC) 00XXX. HR DP BIT 1 OF LOW REGISTER =
|
|
|
|
# 000XX. MIN -2
|
|
|
|
# 0XX.XX SEC 10 SEC
|
|
|
|
# (DECIMAL ONLY.
|
|
|
|
# MAX MIN COMP = 59
|
|
|
|
# MAX SEC COMP = 59.99
|
|
|
|
# MAX CAPACITY = 745 HRS
|
|
|
|
# 39 MINS
|
|
|
|
# 14.55 SECS.
|
|
|
|
# WHEN LOADING, ALL 3
|
|
|
|
# COMPONENTS MUST BE
|
|
|
|
# SUPPLIED.)
|
|
|
|
#
|
|
|
|
# -L-
|
|
|
|
# TIME (MIN/SEC) XXBXX MIN/SEC DP BIT 1 OF LOW REGISTER =
|
|
|
|
# (B IS A BLANK -2
|
|
|
|
# POSITION, DECIMAL 10 SEC
|
|
|
|
# ONLY, DISPLAY OR
|
|
|
|
# MONITOR ONLY. CANNOT
|
|
|
|
# BE LOADED.
|
|
|
|
# MAX MIN COMP = 59
|
|
|
|
# MAX SEC COMP = 59
|
|
|
|
# VALUES GREATER THAN
|
|
|
|
# 59 MIN 59 SEC
|
|
|
|
# ARE DISPLAYED AS
|
|
|
|
# 59 MIN 59 SEC.)
|
|
|
|
#
|
|
|
|
# -M- -2
|
|
|
|
# TIME (SEC) XXX.XX SEC SP BIT 1 = 10 SEC
|
|
|
|
# (MAX 163.83)
|
|
|
|
#
|
|
|
|
# -N-
|
|
|
|
# TIME (SEC) DP XXX.XX SEC DP BIT 1 OF LOW REGISTER =
|
|
|
|
# -2
|
|
|
|
# 10 SEC
|
|
|
|
#
|
|
|
|
# -P-
|
|
|
|
# VELOCITY 2 XXXXX. FEET/SEC DP BIT 1 OF HIGH REGISTER =
|
|
|
|
# (MAX 41994.) -7
|
|
|
|
# 2 METERS/CENTI-SEC
|
|
|
|
#
|
|
|
|
# -Q-
|
|
|
|
# POSITION 4 XXXX.XX 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)
|
|
|
|
#
|
|
|
|
# -FF-
|
|
|
|
# TRIM DEGREES XXX.XX DEG. SP LOW ORDER BIT = 85.41 SEC
|
|
|
|
# (MAX 388.69) OF ARC
|
|
|
|
#
|
|
|
|
# -GG-
|
|
|
|
# INERTIA XXXXXBB. SLUG FT SQ SP FRACTIONAL PART OF
|
|
|
|
# (MAX 07733BB.) 20 2
|
|
|
|
# 2 KG M
|
|
|
|
#
|
|
|
|
# -II- 20
|
|
|
|
# THRUST MOMENT XXXXXBB. FT LBS SP FRACTIONAL PART OF 2
|
|
|
|
# (MAX 07733BB.) NEWTON METER
|
|
|
|
#
|
|
|
|
# -JJ-
|
|
|
|
# POSITION5 XXX.XX NAUT MI DP BIT 1 OF LOW REGISTER =
|
|
|
|
# 2 METERS
|
|
|
|
#
|
|
|
|
# -KK- 16
|
|
|
|
# WEIGHT2 XXXXX. LBS SP FRACTIONAL PART OF 2 KG
|
|
|
|
#
|
|
|
|
# -LL-
|
|
|
|
# POSITION6 XXXX.X NAUT MI DP BIT 1 OF LOW REG =
|
|
|
|
# -28
|
|
|
|
# (6,373,338)(2(PI))x2
|
|
|
|
# -----------------------
|
|
|
|
# 1852
|
|
|
|
# NAUT MI.
|
|
|
|
#
|
|
|
|
# -MM-
|
|
|
|
# DRAG ACCELERATION XXX.XX G DP BIT 1 OF LOW REGISTER =
|
|
|
|
# MAX (024.99) -28
|
|
|
|
# 25x2 G
|
|
|
|
#
|
|
|
|
# -PP-
|
|
|
|
# 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
|
|
|
|
# MONITOR ONLY. CANNOT (EACH REGISTER MUST
|
|
|
|
# BE LOADED.) LESS THAN 100.)
|
|
|
|
# (MAX 99B99)
|
|
|
|
#
|
|
|
|
# -UU-
|
|
|
|
# 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
|
|
|
|
# 4 x 6,373,338 x 2
|
|
|
|
# --------------------
|
|
|
|
# 1852
|
|
|
|
# NAUT MI.
|
|
|
|
#
|
|
|
|
# -XX-
|
|
|
|
# POSITION 9 XXX.XX NAUT MI DP BIT 1 OF LOW REGISTER =
|
|
|
|
# (MAX 283.09) -9
|
|
|
|
# 2 METERS.
|
|
|
|
#
|
|
|
|
# -YY-
|
|
|
|
# VELOCITY 4 XXXX.X FEET/SEC DP FRACTIONAL PART OF
|
|
|
|
# (MAX 328.0) METERS/CENTI-SEC
|
|
|
|
#
|
|
|
|
# -ZZ-
|
|
|
|
# DP FRACTIONAL .XXXXX DP BIT 1 OF HIGH REGISTER =
|
|
|
|
# -14
|
|
|
|
# 2 UNITS
|
|
|
|
|
|
|
|
|
|
|
|
# THAT'S ALL ON THE NOUNS.
|
|
|
|
|
|
|
|
# Page 23
|
|
|
|
|
|
|
|
# ALARM CODES FOR 504
|
|
|
|
|
|
|
|
# REPORT DEFICIENCIES TO JOHN SUTHERLAND: MIT 617-864-6900 X1458
|
|
|
|
|
|
|
|
# *9 *18 *60 *25 COLUMN
|
|
|
|
#
|
|
|
|
# CODE * TYPE SET BY ALARM ROUTINE
|
|
|
|
#
|
|
|
|
# 00110 NO MARK SINCE LAST MARK REJECT SXTMARK ALARM
|
|
|
|
# 00112 MARK NOT BEING ACCEPTED SXTMARK ALARM
|
|
|
|
# 00113 NO NBITS SXTMARK ALARM
|
|
|
|
# 00114 MARK MADE BUT NOT DESIRED SXTMARK ALARM
|
|
|
|
# 00115 OPTICS TORQUE REQUEST WITH SWITCH NOT AT EXT VERB OPTICS CDU ALARM
|
|
|
|
# CGC
|
|
|
|
# 00116 OPTICS SWITCH ALTERED BEFORE 15 SEC ZERO T4RUPT ALARM
|
|
|
|
# TIME ELAPSED.
|
|
|
|
# 00117 OPTICS TORQUE REQUEST WITH OPTICS NOT EXT VERB OPTICS CDU ALARM
|
|
|
|
# AVAILABLE (OPTIND=-0)
|
|
|
|
# 00120 OPTICS TORQUE REQUEST WITH OPTICS T4RUPT ALARM
|
|
|
|
# NOT ZEROED.
|
|
|
|
# 00121 CDUS NO GOOD AT TIME OF MARK SXTMARK ALARM
|
|
|
|
# 00122 MARKING NOT CALLED FOR SXTMARK ALARM
|
|
|
|
# 00124 P17 TPI SEARCH - NO SAFE PERICTR HERE. TPI SEARCH ALARM
|
|
|
|
# 00205 BAD PIPA READING SERVICER ALARM
|
|
|
|
# 00206 ZERO ENCODE NOT ALLOWED WITH COARSE ALIGN IMU MODE SWITCHING ALARM
|
|
|
|
# + GIMBAL LOCK.
|
|
|
|
# 00207 ISS TURNON REQUEST NOT PRESENT FOR 90 SEC T4RUPT ALARM
|
|
|
|
# 00210 IMU NOT OPERATING IMU MODE SWITCH, ALARM, VARALARM
|
|
|
|
# IMU-2, R02, P51
|
|
|
|
# 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
|
|
|
|
# 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
|
|
|
|
# 00217 BAD RETURN FROM STALL ROUTINES CURTAINS ALARM2
|
|
|
|
# 00220 IMU NOT ALIGNED - NO REFSMMAT R02,P51 VARALARM
|
|
|
|
# 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
|
|
|
|
# 00407 AUTO OPTICS REQUEST TRUN ANGLE > 50 DEG. R52 ALARM
|
|
|
|
# 00421 W-MATRIX OVERFLOW INTEGRV ALARM
|
|
|
|
# 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
|
|
|
|
# 00602 PERIGEE ALTITUDE LT PMIN2 P32,P72 VARALARM
|
|
|
|
# 00603 CSI TO CDH TIME LT PMIN22 P32,P72,P33,P73 VARALARM
|
|
|
|
# 00604 CDH TO TPI TIME LT PMIN23 P32,P72 VARALARM
|
|
|
|
# 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
|
|
|
|
# 01104 * DELAY ROUTINE BUSY EXEC BAILOUT
|
|
|
|
# 01105 DOWNLINK TOO FAST T4RUPT ALARM
|
|
|
|
# 01106 UPLINK TOO FAST T4RUPT ALARM
|
|
|
|
# 01107 PHASE TABLE FAILURE. ASSUME RESATRT ALARM
|
|
|
|
# ERASABLE MEMORY IS DESTROYED
|
|
|
|
# 01201 * EXECUTIVE OVERFLOW - NO VAC AREAS EXEC BAILOUT
|
|
|
|
# 01202 * EXECUTIVE OVERFLOW - NO CORE SETS EXEC BAILOUT
|
|
|
|
# 01203 * WAITLIST OVERFLOW - TOO MANY TASKS WAITLIST BAILOUT
|
|
|
|
# 01204 * NEGATIVE OR ZERO WAITLIST CALL WAITLIST POODOO
|
|
|
|
# 01206 * SECOND JOB ATTEMPTS TO GO TO SLEEP PINBALL P00DOO
|
|
|
|
# VIA KEYBOARD AND DISPLAY PROGRAM
|
|
|
|
# 01207 * NO VAC AREA FOR MARKS SXTMARK BAILOUT
|
|
|
|
# 01210 * TWO PROGRAMS USING DEVICE AT SAME TIME IMU MODE SWITCH P00DOO
|
|
|
|
# 01211 * ILLEGAL INTERRUPT OF EXTENDED VERB SXTMARK BAILOUT
|
|
|
|
# 01301 ARCSIN-ARCCOS ARGUMENT TOO LARGE INTERPRETER ALARM
|
|
|
|
# 01302 * SQRT CALLED WITH NEGATIVE ARGUMENT. ABORT. INTERPRETER P00DOO
|
|
|
|
# 01407 VG INCREASING S40.8 ALARM
|
|
|
|
# 01426 IMU UNSATISFACTORY P61,P62 ALARM
|
|
|
|
# 01427 IMU REVERSED P61,P62 ALARM
|
|
|
|
# 01501 * KEYBOARD AND DISPLAY ALARM DURING PINBALL P00DOO
|
|
|
|
# INTERNAL USE (NVSUB). ABORT.
|
|
|
|
# 01502 * ILLEGAL FLASHING DISPLAY GOPLAY P00DOO
|
|
|
|
# 01520 V37 REQUEST NOT PERMITTED AT THIS TIME V37 ALARM
|
|
|
|
# 01521 * P01 ILLEGALLY SELECTED P01, P07 POODOO
|
|
|
|
# 01600 OVERFLOW IN DRIFT TEST OPT PRE ALIGN CALIB ALARM
|
|
|
|
# 01601 * BAD IMU TORQUE - ABORT. OPT PRE ALIGN CALIB ALARM
|
|
|
|
# 01602 BAD OPTICS DURING VERIFICATION OPTALGN CALIB (CSM) ALARM
|
|
|
|
# 01703 INSUF. TIME FOR INTEG., TIG WAS SLIPPED R41 ALARM
|
|
|
|
# 03777 ICDU FAIL CAUSED THE ISS WARNING T4RUPT VARALARM
|
|
|
|
# 04777 ICDU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT VARALARM
|
|
|
|
# 07777 IMU FAIL CAUSED THE ISS WARNING T4RUPT VARALARM
|
|
|
|
# 10777 IMU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT VARALARM
|
|
|
|
# 13777 IMU, ICDU FAILS CAUSED THE ISS WARNING T4RUPT VARALARM
|
|
|
|
# 14777 IMU, ICDU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT VARALARM
|
|
|
|
#
|
|
|
|
# * INDICATES ABORT TYPE. ALL OTHERS ARE NON-ABORTIVE
|
|
|
|
|
|
|
|
# Page 25
|
|
|
|
|
|
|
|
# CHECKLIST CODES FOR 504
|
|
|
|
|
|
|
|
# PLEASE REPORT ANY DEFICIENCIES IN THIS LIST TO JOHN SUTHERLAND.
|
|
|
|
|
|
|
|
# *9 *17 *26 COLUMN
|
|
|
|
#
|
|
|
|
# R1 CODE ACTION TO BE EFFECTED
|
|
|
|
#
|
|
|
|
# 00014 KEY IN FINE ALIGNMENT OPTION
|
|
|
|
# 00015 PERFORM CELESTIAL BODY ACQUISITION
|
|
|
|
# 00016 KEY IN TERMINATE MARK SEQUENCE
|
|
|
|
# 00041 SWITCH CM/SM SEPARATION TO UP
|
|
|
|
# 00062 SWITCH AGC POWER DOWN
|
|
|
|
# 00202 PERFORM GNCS AUTOMATIC MANEUVER
|
|
|
|
# 00203 SWITCH TO CMC-AUTO
|
|
|
|
# 00204 PERFORM SPS GIMBAL TRIM
|
|
|
|
# 00403 SWITCH OPTICS TO MANUAL OR ZERO
|
|
|
|
#
|
|
|
|
# SWITCH DENOTES CHANGE OF POSITION OF A CONSOLE SWITCH
|
|
|
|
# PERFORM DENOTES START OF END OF A TASK
|
|
|
|
# KEY IN DENOTES KEY IN OF DATA THRU THE DSKY
|
|
|
|
|
|
|
|
# Page 26
|
|
|
|
|
|
|
|
# OPTION CODES FOR 504
|
|
|
|
|
|
|
|
# PLEASE REPORT ANY DEFICIENCIES IN THIS LIST TO JOHN SUTHERLAND.
|
|
|
|
|
|
|
|
# THE SPECIFIED OPTION CODES WILL BE FLASHED IN COMPONENT R1 IN
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# CONJUNCTION WITH VERB04NOUN06 TO REQUEST THE ASTRONAUT TO LOAD INTO
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# COMPONENT R2 THE OPTION HE DESIRES.
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# *9 *17 #52 #11 #25 COLUMNN
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#
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# OPTION
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# CODE PURPOSE INPUT FOR COMPONENT 2 PROGRAM(S) APPLICABILITY
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#
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# 00001 SPECIFY IMU ORIENTATION 1=PREF 2=NOM 3=REFSMMAT P50'S ALL
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# 00002 SPECIFY VEHICLE 1=THIS 2=OTHER P21,R30 ALL
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# 00003 SPECIFY TRACKING ATTITUDE 1=PREFERRED 2=OTHER R63 ALL
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# 00004 SPECIFY RADAR 1=RR 2=LR R04 SUNDANCE + LUMINARY
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# 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY
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# 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY
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# 00007 SPECIFY PROPULSION SYSTEM 1=SPS 2=RCS P37 COLOSSUS
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2016-07-08 10:45:31 +00:00
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# 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT + G P57 LUMINARY
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2016-07-07 08:47:26 +00:00
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# 2=TWO BODIES 3=ONE BODY + G
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# 00011 SPEC. SEPARATION MONITOR PHASE 1=DELTAV 2=STATE VECTOR UPDATE P46 LUMINARY
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# 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY
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# ORBIT TO PASS OVER LM
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