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			30 KiB
		
	
	
	
		
			Plaintext
		
	
	
	
	
	
| # Copyright:	Public domain.
 | |
| # Filename:	ASSEMBLY_AND_OPERATION_INFORMATION.agc
 | |
| # Purpose:	Part of the source code for Colossus 2A, AKA Comanche 055.
 | |
| #		It is part of the source code for the Command Module's (CM)
 | |
| #		Apollo Guidance Computer (AGC), for Apollo 11.
 | |
| # Assembler:	yaYUL
 | |
| # Contact:	Ron Burkey <info@sandroid.org>.
 | |
| # Website:	www.ibiblio.org/apollo.
 | |
| # Mod history:	2009-05-05 RSB	Adapted from the Colossus249/ file of the
 | |
| #				same name, using Comanche055 page images.
 | |
| #
 | |
| # This source code has been transcribed or otherwise adapted from digitized
 | |
| # images of a hardcopy from the MIT Museum.  The digitization was performed
 | |
| # by Paul Fjeld, and arranged for by Deborah Douglas of the Museum.  Many
 | |
| # thanks to both.  The images (with suitable reduction in storage size and
 | |
| # consequent reduction in image quality as well) are available online at
 | |
| # www.ibiblio.org/apollo.  If for some reason you find that the images are
 | |
| # illegible, contact me at info@sandroid.org about getting access to the
 | |
| # (much) higher-quality images which Paul actually created.
 | |
| #
 | |
| # Notations on the hardcopy document read, in part:
 | |
| #
 | |
| #	Assemble revision 055 of AGC program Comanche by NASA
 | |
| #	2021113-051.  10:28 APR. 1, 1969
 | |
| #
 | |
| #	This AGC program shall also be referred to as
 | |
| #			Colossus 2A
 | |
| 
 | |
| # Page 2
 | |
| 
 | |
| # ASSEMBLY AND OPERATIONS INFORMATION
 | |
| # TAGS FOR RELATIVE SETLOC AND BLANK BANK CARDS
 | |
| # SUBROUTINE CALLS
 | |
| #
 | |
| #
 | |
| #	COMERASE
 | |
| #		ERASABLE ASSIGNMENTS
 | |
| #	COMAID
 | |
| #		INTERRUPT LEAD INS
 | |
| #		T4RUPT PROGRAM
 | |
| #		DOWNLINK LISTS
 | |
| #		FRESH START AND RESTART
 | |
| #		RESTART TABLES
 | |
| #		SXTMARK
 | |
| #		EXTENDED VERBS
 | |
| #		PINBALL NOUN TABLES
 | |
| #		CSM GEOMETRY
 | |
| #		IMU COMPENSATION PACKAGE
 | |
| #		PINBALL GAME  BUTTONS AND LIGHTS
 | |
| #		R60,R62
 | |
| #		ANGLFIND
 | |
| #		GIMBAL LOCK AVOIDANCE
 | |
| #		KALCMANU STEERING
 | |
| #		SYSTEM TEST STANDARD LEAD INS
 | |
| #		IMU CALIBRATION AND ALIGNMENT
 | |
| #	COMEKISS
 | |
| #		GROUND TRACKING DETERMINATION PROGRAM - P21
 | |
| #		P34-P35, P74-P75
 | |
| #		R31
 | |
| #		P76
 | |
| #		R30
 | |
| #		STABLE ORBIT - P38-P39
 | |
| #	TROUBLE
 | |
| #		P11
 | |
| #		TPI SEARCH
 | |
| #		P20-P25
 | |
| #		P30,P37
 | |
| #		P32-P33, P72-P73
 | |
| #		P40-P47
 | |
| #		P51-P53
 | |
| #		LUNAR AND SOLAR EPHEMERIDES SUBROUTINES
 | |
| #		P61-P67
 | |
| #		SERVICER207
 | |
| #		ENTRY LEXICON
 | |
| #		REENTRY CONTROL
 | |
| #		CM BODY ATTITUDE
 | |
| #		P37,P70
 | |
| #		S-BAND ANTENNA FOR CM
 | |
| #	TVCDAPS
 | |
| #		TVCINITIALIZE
 | |
| # Page 3
 | |
| #		TVCEXECUTIVE
 | |
| #		TVCMASSPROP
 | |
| #		TVCRESTARTS
 | |
| #		TVCDAPS
 | |
| #		TVCSTROKETEST
 | |
| #		TVCROLLDAP
 | |
| #		MYSUBS
 | |
| #		RCS-CSM DIGITAL AUTOPILOT
 | |
| #		AUTOMATIC MANEUVERS
 | |
| #		RCS-CSM DAP EXECUTIVE PROGRAMS
 | |
| #		JET SELECTION LOGIC
 | |
| #		CM ENTRY DIGITAL AUTOPILOT
 | |
| #	CHIEFTAN
 | |
| #		DOWN-TELEMETRY PROGRAM
 | |
| #		INTER-BANK COMMUNICATION
 | |
| #		INTERPRETER
 | |
| #		FIXED-FIXED CONSTANT POOL
 | |
| #		INTERPRETIVE CONSTANTS
 | |
| #		SINGLE PRECISION SUBROUTINES
 | |
| #		EXECUTIVE
 | |
| #		WAITLIST
 | |
| #		LATITUDE LONGITUDE SUBROUTINES
 | |
| #		PLANETARY INERTIAL ORIENTATION
 | |
| #		MEASUREMENT INCORPORATION
 | |
| #		CONIC SUBROUTINES
 | |
| #		INTEGRATION INITIALIZATION
 | |
| #		ORBITAL INTEGRATION
 | |
| #		INFLIGHT ALIGNMENT ROUTINES
 | |
| #		POWERED FLIGHT SUBROUTINES
 | |
| #		TIME OF FREE FALL
 | |
| #		STAR TABLES
 | |
| #		AGC BLOCK TWO SELF-CHECK
 | |
| #		PHASE TABLE MAINTENANCE
 | |
| #		RESTARTS ROUTINE
 | |
| #		IMU MODE SWITCHING ROUTINES
 | |
| #		KEYRUPT, UPRUPT
 | |
| #		DISPLAY INTERFACE ROUTINES
 | |
| #		SERVICE ROUTINES
 | |
| #		ALARM AND ABORT
 | |
| #		UPDATE PROGRAM
 | |
| #		RTB OP CODES
 | |
| #
 | |
| #
 | |
| #       SYMBOL TABLE LISTING
 | |
| #       UNREFERENCED SYMBOL LISTING
 | |
| #       ERASABLE & EQUALS CROSS-REFERENCE TABLE
 | |
| #       SUMMARY OF SYMBOL TABLE LISTINGS
 | |
| #       MEMORY TYPE & AVAILABILITY DISPLAY
 | |
| #       COUNT TABLE
 | |
| #       PARAGRAPHS GENERATED FOR THIS ASSEMBLY
 | |
| # Page 4
 | |
| #       OCTAL LISTING
 | |
| #       OCCUPIED LOCATIONS TABLE
 | |
| #       SUBROS CALLED & PROGRAM STATUS
 | |
| 
 | |
| # Page 5
 | |
| # VERB LIST FOR CSM
 | |
| 
 | |
| # 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)
 | |
| # 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)
 | |
| # 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
 | |
| # 26
 | |
| # 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)
 | |
| # 38
 | |
| # 39
 | |
| 
 | |
| # Page 6
 | |
| 
 | |
| # 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.
 | |
| # 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
 | |
| # 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
 | |
| 
 | |
| # 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
 | |
| # 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 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
 | |
| # 03	SPECIFY MACHINE ADDRESS (DEGREES)	3COMP	XXX.XX DEG FOR EACH
 | |
| # 04	SPARE
 | |
| # 05	ANGULAR ERROR/DIFFERENCE		1COMP	XXX.XX DEG
 | |
| # 06	OPTION CODE				2COMP	OCTAL ONLY FOR EACH
 | |
| # LOADING NOUN 07 WILL SET OR RESET SELECTED BITS IN ANY ERASABLE REGISTER
 | |
| # 07	ECADR OF WORD TO BE MODIFIED		3COMP	OCTAL ONLY FOR EACH
 | |
| #	ONES FOR BITS TO BE MODIFIED
 | |
| #	1 TO SET OR 0 TO RESET SELECTED BITS
 | |
| # 08	ALARM DATA				3COMP	OCTAL ONLY FOR EACH
 | |
| # 09	ALARM CODES				3COMP	OCTAL ONLY FOR EACH
 | |
| # 10	CHANNEL TO BE SPECIFIED			1COMP	OCTAL ONLY
 | |
| # 11	TIG OF CSI				3COMP	00XXX. HRS		DEC ONLY
 | |
| #							000XX. MIN		MUST LOAD 3 COMPS
 | |
| #							0XX.XX SEC
 | |
| # 12	OPTION CODE				2COMP	OCTAL ONLY FOR EACH
 | |
| #	 (USED BY EXTENDED VERBS ONLY)
 | |
| # 13	TIG OF CDH				3COMP	00XXX. HRS		DEC ONLY
 | |
| #							000XX. MIN		MUST LOAD 3 COMPS
 | |
| #							0XX.XX SEC
 | |
| # 14	SPARE
 | |
| # 15	INCREMENT MACHINE ADDRESS		1COMP	OCTAL ONLY
 | |
| # 16	TIME OF EVENT				3COMP	00XXX. HRS		DEC ONLY
 | |
| #	 (USED BY EXTENDED VERBS ONLY)			000XX. MIN		MUST LOAD 3 COMPS
 | |
| #							0XX.XX SEC
 | |
| # 17	ASTRONAUT TOTAL ATTITUDE		3COMP	XXX.XX DEG FOR EACH
 | |
| # 18	AUTO MANEUVER BALL ANGLES		3COMP	XXX.XX DEG FOR EACH
 | |
| # 19	BYPASS ATTITUDE TRIM MANEUVER		3COMP	XXX.XX DEG FOR EACH
 | |
| # 20	ICDU ANGLES				3COMP	XXX.XX DEG FOR EACH
 | |
| # 21	PIPAS					3COMP	XXXXX. PULSES FOR EACH
 | |
| # 22	NEW ICDU ANGLES				3COMP	XXX.XX DEG FOR EACH
 | |
| # 23	SPARE
 | |
| # 24	DELTA TIME FOR AGC CLOCK		3COMP	00XXX. HRS.		DEC ONLY
 | |
| #							000XX. MIN		MUST LOAD 3 COMPS
 | |
| #							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
 | |
| # 							0XX.XX SEC
 | |
| # 32	TIME FROM PERIGEE			3COMP	00XXX. HRS		DEC ONLY
 | |
| #							000XX. MIN		MUST LOAD 3 COMPS
 | |
| #							0XX.XX SEC
 | |
| # 33	TIME OF IGNITION			3COMP	00XXX. HRS		DEC ONLY
 | |
| #							000XX. MIN		MUST LOAD 3 COMPS
 | |
| #							0XX.XX SEC
 | |
| # 34	TIME OF EVENT				3COMP	00XXX. HRS		DEC ONLY
 | |
| #							000XX. MIN		MUST LOAD 3 COMPS
 | |
| #							0XX.XX SEC
 | |
| # 35	TIME FROM EVENT				3COMP	00XXX. HRS		DEC ONLY
 | |
| #							000XX. MIN		MUST LOAD 3 COMPS
 | |
| #							0XX.XX SEC
 | |
| # 36	TIME OF AGC CLOCK			3COMP	00XXX. HRS		DEC ONLY
 | |
| #							000XX. MIN		MUST LOAD 3 COMPS
 | |
| #							0XX.XX SEC
 | |
| # 37	TIG OF TPI				3COMP	00XXX. HRS		DEC ONLY
 | |
| #							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
 | |
| 
 | |
| # Page 11
 | |
| 
 | |
| # 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
 | |
| #	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.XX 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 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
 | |
| #	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              MUST LOAD 3 COMPS
 | |
| #							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		DEC ONLY
 | |
| #      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
 | |
| #				TRUNION			XX.XXX DEG
 | |
| # 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 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	XXXXX.FT	        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		B
 | |
| # 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		TTPI		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	STARSAV3	ZZ
 | |
| #	2	STARSAV3 +2	ZZ
 | |
| #	3	STARSAV3 +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 =
 | |
| #			        			     28
 | |
| #			(MAX 359.99)			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 2-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.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)
 | |
| #
 | |
| # -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.)                     CONTAIN A POSITIVE INTEGER
 | |
| #			(MAX 99B99)                      LESS THAN 100)
 | |
| #
 | |
| # -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		XXXXX. FEET		DP	BIT 1 OF LOW REGISTER =
 | |
| #							 -9
 | |
| #							2   METERS
 | |
| #
 | |
| # -YY-
 | |
| # VELOCITY 4		XXXX.X FEET/SEC		DP	FRACTIONAL PART OF
 | |
| #			(MAX 328.0)			METERS/CENTI-SEC
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| #
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| # -ZZ-
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| # DP FRACTIONAL		.XXXXX			DP	BIT 1 OF HIGH REGISTER =
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| #							 -14
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| #							2    UNITS
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| 
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| # THAT-S ALL ON THE NOUNS.
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| 
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| # Page 23
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| 
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| # 		ALARM CODES FOR 504
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| 
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| # 		REPORT DEFICIENCIES TO JOHN SUTHERLAND @ MIT 617-864-6900 X1458
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| 
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| # *9		*18						*60			                *25  COLUMN
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| #
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| # CODE       *	TYPE						SET BY			                ALARM ROUTINE
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| #
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| # 00110		NO MARK SINCE LAST MARK REJECT			SXTMARK			                ALARM
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| # 00112		MARK NOT BEING ACCEPTED				SXTMARK			                ALARM
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| # 00113		NO INBITS					SXTMARK			                ALARM
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| # 00114		MARK MADE BUT NOT DESIRED			SXTMARK			                ALARM
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| # 00115		OPTICS TORQUE REQUESTWITH SWITCH NOT AT	        EXT VERB OPTICS CDU	                ALARM
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| # 		 CGC
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| # 00116		OPTICS SWITCH ALTERED BEFORE 15 SEC ZERO	T4RUPT			                ALARM
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| #		 TIME ELAPSED.
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| # 00117		OPTICS TORQUE REQUEST WITH OPTICS NOT		EXT VERB OPTICS CDU	                ALARM
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| #		 AVAILABLE (OPTIND=-0)
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| # 00120		OPTICS TORQUE REQUEST WITH OPTICS		T4RUPT			                ALARM
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| #		 NOT ZEROED
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| # 00121		CDUS NO GOOD AT TIME OF MARK			SXTMARK			                ALARM
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| # 00122		MARKING NOT CALLED FOR				SXTMARK			                ALARM
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| # 00124		P17 TPI SEARCH - NO SAFE PERICTR HERE.		TPI SEARCH		                ALARM
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| # 00205		BAD PIPA READING				SERVICER		                ALARM
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| # 00206		ZERO ENCODE NOT ALLOWED WITH COARSE ALIGN	IMU MODE SWITCHING	                ALARM
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| # 		 + GIMBAL LOCK
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| # 00207		ISS TURNON REQUEST NOT PRESENT FOR 90 SEC	T4RUPT			                ALARM
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| # 00210		IMU NOT OPERATING				IMU MODE SWITCH, IMU-2, R02, P51        ALARM,VARALARM
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| # 00211		COARSE ALIGN ERROR - DRIVE > 2 DEGREES		IMU MODE SWITCH		                ALARM
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| # 00212		PIPA FAIL BUT PIPA IS NOT BEING USED		IMU MODE SWITCH,T4RPT	                ALARM
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| # 00213		IMU NOT OPERATING WITH TURN-ON REQUEST		T4RUPT			                ALARM
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| # 00214		PROGRAM USING IMU WHEN TURNED OFF		T4RUPT			                ALARM
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| # 00215		PREFERRED ORIENTATION NOT SPECIFIED		P52,P54			                ALARM
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| # 00217		BAD RETURN FROM STALL ROUTINES.			CURTAINS		                ALARM2
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| # 00220		IMU NOT ALIGNED - NO REFSMMAT			R02,P51			                VARALARM
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| # 00401		DESIRED GIMBAL ANGLES YIELD GIMBAL LOCK		IMF ALIGN, IMU-2	                ALARM
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| # 00404		TARGET OUT OF VIEW - TRUN ANGLE > 90 DEG	R52			                PRIOLARM
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| # 00405		TWO STARS NOT AVAILABLE				P52,P54			                ALARM
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| # 00406		REND NAVIGATION NOT OPERATING			R21,R23			                ALARM
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| # 00407		AUTO OPTICS REQUEST TRUN ANGLE > 50 DEG.	R52			                ALARM
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| # 00421		W-MATRIX OVERFLOW				INTEGRV			                VARALARM
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| # 00430	     *	INTEG. ABORT DUE TO SUBSURFACE S. V.		ALL CALLS TO INTEG	                POODOO
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| # 00600		IMAGINARY ROOTS ON FIRST ITERATION		P32, P72		                VARALARM
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| # 00601		PERIGEE ALTITUDE LT PMIN1			P32,P72,		                VARALARM
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| # 00602		PERIGEE ALTITUDE LT PMIN2			P32,P72,		                VARALARM
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| # 00603		CSI TO CDH TIME LT PMIN22			P32,P72,P33,P73		                VARALARM
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| # 00604		CDH TO TPI TIME LT PMIN23			P32,P72			                VARALARM
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| # 00605		NUMBER OF ITERATIONS EXCEEDS LOOP MAXIMUM	P32,P72,P37		                VARALARM
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| # 00606		DV EXCEEDS MAXIMUM				P32,P72			                VARALARM
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| # 00607	     *	NO SOLN FROM TIME-THETA OR TIME-RADIUS		TIMETHET,TIMERAD	                POODOO
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| # Page 24
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| # 00610      *	LAMBDA LESS THAN UNITY				P37			                POODOO
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| # 00611		NO TIG FOR GIVEN ELEV ANGLE			P34,P74			                VARALARM
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| # 00612		STATE VECTOR IN WRONG SPHERE OF INFLUENCE	P37			                VARALARM
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| # 00613		REENTRY ANGLE OUT OF LIMITS			P37			                VARALARM
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| # 00777		PIPA FAIL CAUSED ISS WARNING.			T4RUPT			                VARALARM
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| # 01102		CMC SELF TEST ERROR							                ALARM2
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| # 01103      *	UNUSED CCS BRANCH EXECUTED			ABORT			                POODOO
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| # 01104      *	DELAY ROUTINE BUSY				EXEC			                BAILOUT
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| # 01105		DOWNLINK TOO FAST				T4RUPT			                ALARM
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| # 01106		UPLINK TOO FAST					T4RUPT			                ALARM
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| # 01107		PHASE TABLE FAILURE. ASSUME			RESATRT			                ALARM
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| #		ERASABLE MEMORY IS DESTROYED
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| # 01201	     *	EXECUTIVE OVERFLOW-NO VAC AREAS		        EXEC			                BAILOUT
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| # 01202	     *	EXECUTIVE OVERFLOW-NO CORE SETS		        EXEC			                BAILOUT
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| # 01203      *	WAITLIST OVERFLOW-TOO MANY TASKS		WAITLIST		                BAILOUT
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| # 01204      *	NEGATIVE OR ZERO WAITLIST CALL			WAITLIST		                POODOO
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| # 01206      *	SECOND JOB ATTEMPTS TO GO TO SLEEP		PINBALL			                POODOO
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| #		VIA KEYBOARD AND DISPLAY PROGRAM
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| # 01207      *	NO VAC AREA FOR MARKS				SXTMARK			                BAILOUT
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| # 01210	     *	TWO PROGRAMS USING DEVICE AT SAME TIME		IMU MODE SWITCH		                POODOO
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| # 01211      *	ILLEGAL INTERRUPT OF EXTENDED VERB		SXTMARK			                BAILOUT
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| # 01301		ARCSIN-ARCCOS ARGUMENT TOO LARGE		INTERPRETER		                ALARM
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| # 01302      *	SQRT CALLED WITH NEGATIVE ARGUMENT.ABORT	INTERPRETER		                POODOO
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| # 01407		VG INCREASING					S40.8			                ALARM
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| # 01426		IMU UNSATISFACTORY				P61, P62			        ALARM
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| # 01427		IMU REVERSED					P61, P62			        ALARM
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| # 01501	     *	KEYBOARD AND DISPLAY ALARM DURING		PINBALL			                POODOO
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| #		 INTERNAL USE (NVSUB). ABORT.
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| # 01502	     *	ILLEGAL FLASHING DISPLAY			GOPLAY			                POODOO
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| # 01520		V37 REQUEST NOT PERMITTED AT THIS TIME		V37			                ALARM
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| # 01521	     *	P01 ILLEGALLY SELECTED				P01, P07                                POODOO
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| # 01600		OVERFLOW IN DRIFT TEST				OPT PRE ALIGN CALIB	                ALARM
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| # 01601      	BAD IMU TORQUE  				OPT PRE ALIGN CALIB	                ALARM
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| # 01602		BAD OPTICS DURING VERIFICATION			OPTALGN CALIB (CSM)	                ALARM
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| # 01703		INSUF. TIME FOR INTEG., TIG WAS SLIPPED		R41			                ALARM
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| # 03777		ICDU FAIL CAUSED THE ISS WARNING		T4RUPT			                VARALARM
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| # 04777		ICDU , PIPA FAILS CAUSED THE ISS WARNING	T4RUPT			                VARALARM
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| # 07777		IMU FAIL CAUSED THE ISS WARNING			T4RUPT			                VARALARM
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| # 10777		IMU , PIPA FAILS CAUSED THE ISS WARNING		T4RUPT			                VARALARM
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| # 13777		IMU , ICDU FAILS CAUSED THE ISS WARNING		T4RUPT			                VARALARM
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| # 14777		IMU,ICDU,PIPA FAILS CAUSED THE ISSWNING	        T4RUPT			                VARALARM
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| # 	     *	INDICATES ABORT TYPE.ALL OTHERS ARE NON-ABORTIVE
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| 
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| # Page 25
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| 
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| #               CHECKLIST CODES FOR 504
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| 
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| #               PLEASE REPORT ANY DEFICIENCIES IN THIS LIST TO JOHN SUTHERLAND
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| 
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| # *9		*17		*26  COLUMN
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| #
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| # R1 CODE	   ACTION TO BE EFFECTED
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| #
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| # 00014		KEY IN		FINE ALIGNMENT OPTION
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| # 00015		PERFORM		CELESTIAL BODY ACQUISITION
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| # 00016		KEY IN		TERMINATE MARK SEQUENCE
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| # 00041		SWITCH		CM/SM SEPARATION TO UP
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| # 00062		SWITCH		AGC POWER DOWN
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| # 00202		PERFORM		GNCS AUTOMATIC MANEUVER
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| # 00203		SWITCH		TO CMC-AUTO
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| # 00204		PERFORM		SPS GIMBAL TRIM
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| # 00403		SWITCH		OPTICS TO MANUAL OR ZERO
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| #		                  SWITCH DENOTES CHANGE POSITION OF A CONSOLE SWITCH
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| #		                  PERFORM DENOTES START OR END OF A TASK
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| #		                  KEY IN DENOTES KEY IN OF DATA THRU THE DSKY
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| 
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| # Page 26
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| 
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| #          OPTION CODES FOR 504
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| 
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| #          PLEASE REPORT ANY DEFICIENCIES IN THIS LIST TO JOHN SUTHERLAND
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| 
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| # 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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| 
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| # *9		*17					*52				*11		*25  COLUMN
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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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| # 00010		SPECIFY ALIGNMENT MODE			0=ANY TIME 1=REFSMMAT +G	P57		LUMINARY
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| #							2=TWO BODIES 3=ONE BODY + G
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| # 00011		SPECIFY 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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