mirror of
				https://github.com/chrislgarry/Apollo-11.git
				synced 2025-10-26 04:16:18 +00:00 
			
		
		
		
	
		
			
				
	
	
		
			206 lines
		
	
	
		
			4.5 KiB
		
	
	
	
		
			Plaintext
		
	
	
	
	
	
			
		
		
	
	
			206 lines
		
	
	
		
			4.5 KiB
		
	
	
	
		
			Plaintext
		
	
	
	
	
	
| # Copyright:	Public domain.
 | |
| # Filename:	GROUND_TRACKING_DETERMINATION_PROGRAM.agc
 | |
| # Purpose:	Part of the source code for Comanche, build 055.
 | |
| #		It is part of the source code for the Command Module's (CM)
 | |
| #		Apollo Guidance Computer (AGC), Apollo 11.
 | |
| # Assembler:	yaYUL
 | |
| # Reference:	pp. 456-459
 | |
| # Contact:	Onno Hommes <ohommes@cmu.edu>.
 | |
| # Website:	www.ibiblio.org/apollo.
 | |
| # Mod history:	2009-05-07 OH	Transcription Batch 1 Assignment
 | |
| #		2009-05-20 RSB	Corrected a couple of DIMOFLAG to DIM0FLAG.
 | |
| #
 | |
| # The contents of the "Comanche055" files, in general, are transcribed
 | |
| # from scanned documents.
 | |
| #
 | |
| #	Assemble revision 055 of AGC program Comanche by NASA
 | |
| #	2021113-051.  April 1, 1969.
 | |
| #
 | |
| #	This AGC program shall also be referred to as Colossus 2A
 | |
| #
 | |
| #	Prepared by
 | |
| #			Massachusetts Institute of Technology
 | |
| #			75 Cambridge Parkway
 | |
| #			Cambridge, Massachusetts
 | |
| #
 | |
| #	under NASA contract NAS 9-4065.
 | |
| #
 | |
| # Refer directly to the online document mentioned above for further information.
 | |
| # Please report any errors to info@sandroid.org.
 | |
| 
 | |
| # Page 456
 | |
| # GROUND TRACKING DETERMINATION PROGRAM P21
 | |
| # PROGRAM DESCRIPTION
 | |
| # MOD NO - 1
 | |
| # MOD BY - N.M.NEVILLE
 | |
| # FUNCTIONAL DECRIPTION-
 | |
| #
 | |
| # TO PROVIDE THE ASTRONAUT DETAILS OF THE LM OR CSM GROUND TRACK WITHOUT
 | |
| # THE NEED FOR GROUND COMMUNICATION (REQUESTED BY DSKY).
 | |
| # CALLING SEQUENCE -
 | |
| #
 | |
| # ASTRONAUT REQUEST THROUGH DSKY V37E21E
 | |
| # SUBROUTINES CALLED-
 | |
| #
 | |
| # GOPERF4
 | |
| # GOFLASH
 | |
| # THISPREC
 | |
| # OTHPREC
 | |
| # LAT-LONG
 | |
| # NORMAL EXIT MODES-
 | |
| #
 | |
| # ASTRONAUT REQUEST THROUGH DSKY TO TERMINATE PROGRAM V34E
 | |
| # ALARM OR ABORT EXIT MODES-
 | |
| #
 | |
| # NONE
 | |
| # OUTPUT -
 | |
| #
 | |
| # OCTAL DISPLAY OF OPTION CODE AND VEHICLE WHOSE GROUND TRACK IS TO BE
 | |
| # COMPUTED
 | |
| #	OPTION CODE	00002
 | |
| #	THIS		00001
 | |
| #	OTHER		00002
 | |
| # DECIMAL DISPLAY OF TIME TO BE INTEGRATED TO HOURS , MINUTES , SECONDS
 | |
| # DECIMAL DISPLAY OF LAT,LONG,ALT
 | |
| # ERASABLE INITIALIZATION REQUIRED
 | |
| #
 | |
| # AX0		2DEC	4.652459653 E-5		RADIANS		"68-69 CONSTANTS"
 | |
| #
 | |
| # -AY0		2DEC	2.147535898 E-5		RADIANS
 | |
| #
 | |
| # AZ0		2DEC	.7753206164		REVOLUTIONS
 | |
| # FOR LUNAR ORBITS 504LM VECTOR IS NEEDED
 | |
| #
 | |
| # 504LM		2DEC	-2.700340600 E-5	RADIANS
 | |
| #
 | |
| # 504LM _2	2DEC	-7.514128400 E-4	RADIANS
 | |
| #
 | |
| # 504LM _4	2DEC	_2.553198641 E-4	RADIANS
 | |
| #
 | |
| # NONE
 | |
| # DEBRIS
 | |
| 
 | |
| # Page 457
 | |
| # CENTRALS-A,Q,L
 | |
| # OTHER-THOSE USED BY THE ABOVE LISTED SUBROUTINES
 | |
| # SEE LEMPREC,LAT-LONG
 | |
| 		SBANK=	LOWSUPER	# FOR LOW 2CADR'S.
 | |
| 
 | |
| 		BANK	33
 | |
| 		SETLOC	P20S
 | |
| 		BANK
 | |
| 
 | |
| 		EBANK=	P21TIME
 | |
| 		COUNT	24/P21
 | |
| 
 | |
| PROG21		CAF	ONE
 | |
| 		TS	OPTION2		# ASSUMED VEHICLE IS LM , R2 = 00001
 | |
| 		CAF	BIT2		#  OPTION 2
 | |
| 		TC	BANKCALL
 | |
| 		CADR	GOPERF4
 | |
| 		TC	GOTOPOOH	# TERMINATE
 | |
| 		TC	+2		# PROCEED VALUE OF ASSUMED VEHICLE OK
 | |
| 		TC	-5		# R2 LOADED THROUGH DSKY
 | |
| P21PROG1	CAF	V6N34		# LOAD DESIRED TIME OF LAT-LONG.
 | |
| 		TC	BANKCALL
 | |
| 		CADR	GOFLASH
 | |
| 		TC	GOTOPOOH	# TERM
 | |
| 		TC	+2		# PROCEED VALUES OK
 | |
| 		TC	-5		# TIME LOADED THROUGH DSKY
 | |
| 		TC	INTPRET
 | |
| 		DLOAD
 | |
| 			DSPTEM1
 | |
| 		STCALL	TDEC1		# INTEG TO TIME SPECIFIED IN TDEC
 | |
| 			INTSTALL
 | |
| 		BON	SET
 | |
| 			P21FLAG
 | |
| 			P21CONT		# ON...RECYCLE USING BASE VECTOR
 | |
| 			VINTFLAG	# OFF..1ST PASS CALC BASE VECTOR
 | |
| 		SLOAD	SR1
 | |
| 			OPTION2
 | |
| 		BHIZ	CLEAR
 | |
| 			+2		# ZERO..THIS VEHICLE (CM)
 | |
| 			VINTFLAG	# ONE...OTHER VEHICLE(LM)
 | |
| 		CLEAR	CLEAR
 | |
| 			DIM0FLAG
 | |
| 			INTYPFLG	# PRECISION
 | |
| 		CALL
 | |
| 			INTEGRV		# CALCULATE
 | |
| 		GOTO			# .AND
 | |
| 			P21VSAVE	# ..SAVE BASE VECTOR
 | |
| P21CONT		VLOAD			# RECYCLE..INTEG FROM BASE VECTOR
 | |
| 			P21BASER
 | |
| # Page 458
 | |
| 		STOVL	RCV		# ..POS
 | |
| 			P21BASEV
 | |
| 		STODL	VCV		# ..VEL
 | |
| 			P21TIME
 | |
| 		STORE	TET		# ..TIME
 | |
| 		CLEAR	CLEAR
 | |
| 			DIM0FLAG
 | |
| 			MOONFLAG
 | |
| 		SLOAD	BZE
 | |
| 			P21ORIG
 | |
| 			+3		# ZERO = EARTH
 | |
| 		SET			# ...2 = MOON
 | |
| 			MOONFLAG
 | |
| 		CALL
 | |
| 			INTEGRVS
 | |
| P21VSAVE	DLOAD			# SAVE CURRENT BASE VECTOR
 | |
| 			TAT
 | |
| 		STOVL	P21TIME		# ..TIME
 | |
| 			RATT1
 | |
| 		STOVL	P21BASER	# ..POS B-29 OR B-27
 | |
| 			VATT1
 | |
| 		STORE	P21BASEV	# ..VEL B-7  OR B-5
 | |
| 		ABVAL	SL*
 | |
| 			0,2
 | |
| 		STOVL	P21VEL		# /VEL/ FOR N73 DSP
 | |
| 			RATT
 | |
| 		UNIT	DOT
 | |
| 			VATT		# U(R).(V)
 | |
| 		DDV	ASIN		# U(R).U(V)
 | |
| 			P21VEL
 | |
| 		STORE	P21GAM		# SIN-1 U(R).U(V), -90 TO +90
 | |
| 		SXA,2	SET
 | |
| 			P21ORIG		# 0 = EARTH  2 = MOON
 | |
| 			P21FLAG
 | |
| P21DSP		CLEAR	SLOAD		# GENERATE DISPLAY DATA
 | |
| 			LUNAFLAG
 | |
| 			X2
 | |
| 		BZE	SET
 | |
| 			+2		# 0 = EARTH
 | |
| 			LUNAFLAG
 | |
| 		VLOAD
 | |
| 			RATT
 | |
| 		STODL	ALPHAV
 | |
| 			TAT
 | |
| 		CLEAR	CALL
 | |
| 			ERADFLAG
 | |
| 			LAT-LONG
 | |
| 		DMP			# MPAC = ALT, METERS B-29
 | |
| 			K.01
 | |
| 		STORE	P21ALT		# ALT/100 FOR N73 DSP
 | |
| # Page 459
 | |
| 		EXIT
 | |
| 		CAF	V06N43		# DISPLAY LAT,LONG,ALT
 | |
| 		TC	BANKCALL	# LAT,LONG = REVS B0 BOTH EARTH/MOON
 | |
| 		CADR	GOFLASH		# ALT = METERS B-29  BOTH EARTH/MOON
 | |
| 		TC	GOTOPOOH	# TERM
 | |
| 		TC	GOTOPOOH
 | |
| 		TC	INTPRET		# V32E RECYCLE
 | |
| 		DLOAD	DAD
 | |
| 			P21TIME
 | |
| 			600SEC		# 600 SECONDS OR 10 MIN
 | |
| 		STORE	DSPTEM1
 | |
| 		RTB
 | |
| 			P21PROG1
 | |
| 600SEC		2DEC	60000		# 10 MIN
 | |
| 
 | |
| P21ONENN	OCT	00001		# NEEDED TO DETERMINE VEHICLE
 | |
| 		OCT	00000		# TO BE INTEGRATED
 | |
| V06N43		VN	00643
 | |
| V6N34		VN	00634
 | |
| K.01		2DEC	.01
 | |
| 
 |