https://github.com/virtualagc/virtualagc
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Tip revision: 7d6cec3857985b92ed11312dcdeac0a49edb0ab8 authored by Mike Stewart on 13 March 2018, 04:58:16 UTC
yaAGC: Integrated the LR and RR into the new PulseInput/PulseOutput interface
Tip revision: 7d6cec3
GROUND_TRACKING_DETERMINATION_PROGRAM_-_P21.agc
### FILE="Main.annotation"
## Copyright:   Public domain.
## Filename:	GROUND_TRACKING_DETERMINATION_PROGRAM_-_P21.agc
## Purpose:     Part of the source code for Colossus build 237.
##              This is for the Command Module's (CM) Apollo Guidance
##              Computer (AGC), for Apollo 8.
## Assembler:   yaYUL
## Contact:     Jim Lawton <jim DOT lawton AT gmail DOT com>
## Website:     www.ibiblio.org/apollo/index.html
## Page Scans:  www.ibiblio.org/apollo/ScansForConversion/Colossus237/
## Mod history: 2011-02-02 JL   Adapted from corresponding Colossus 249 file.
##		2016-12-31 RSB	Proofed comment text using octopus/ProoferComments,
##				and corrected errors found.
##		2017-01-14 RSB	Corrected comment-errors located in diff'ing
##				vs Colossus 249

## Page 447
# 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 TROUGH 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 448
#
# 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
		STORE	P21TIME
		SLOAD	DSU
			OPTION2
			P21ONENN
		BHIZ	DLOAD
			P21PROG2	# VEHICLE TO BE INTEGRATED IS LEM
			P21TIME		# VEHICLE TO BE INTEGRATED IS CSM
		STCALL	TDEC1		# INTEGRATE TO TIME SPECIFIED IN TDEC
			OTHPREC		# ADJUST UNITS FOR LAT-LONG ROUTINE
P21PROGA	SLOAD	BHIZ
			X2
			P21PROG3
		VLOAD	SETGO
			RATT
			LUNAFLAG
			P21PROG4
P21PROG2	DLOAD
			P21TIME
		STCALL	TDEC1
			THISPREC
## Page 449
		GOTO
			P21PROGA
P21PROG3	VLOAD	CLEAR
			RATT
			LUNAFLAG
P21PROG4	STODL	ALPHAV
			TAT
		CLEAR	CALL
			ERADFLAG
			LAT-LONG
		EXIT
		CAF	V06N43		# DISPLAY LAT,LONG,ALT
		TC	BANKCALL	# LAT,LONG = 1/2 REVS B0
		CADR	GOFLASH		# ALT = KM  B14
		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
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