Apollo-11/Luminary099/DAPIDLER_PROGRAM.agc

# Copyright:	Public domain.
# Filename:	DAPIDLER_PROGRAM.agc
# Purpose: 	Part of the source code for Luminary 1A build 099.
#		It is part of the source code for the Lunar Module's (LM)
#		Apollo Guidance Computer (AGC), for Apollo 11.
# Assembler:	yaYUL
# Contact:	Ron Burkey <info@sandroid.org>.
# Website:	www.ibiblio.org/apollo.
# Pages:	1410-1420
# Mod history:  2009-05-10 SN   (Sergio Navarro).  Started adapting
#				from the Luminary131/ file of the same
#				name, using Luminary099 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 001 of AGC program LMY99 by NASA 2021112-061
#	16:27 JULY 14, 1969

# Page 1410
# THE DAPIDLER PROGRAM IS STARTED BY FRESH START AND RESTART.		  THE DAPIDLER PROGRAM IS DONE 10 TIMES
# PER SECOND UNTIL THE ASTRONAUT DESIRES THE DAP TO WAKE UP, AND THE IMU AND CDUS ARE READY FOR USE BY THE DAP.
# THE NECESSARY INITIALIZATION OF THE DAP IS DONE BY THE DAPIDLER PROGRAM.
		BANK	16
		SETLOC	DAPS1
		BANK

		EBANK=	AOSQ

		COUNT*	$$/DAPID

CHEKBITS	EXTEND
		READ	CHAN31		# IF BOTH BIT13 AND BIT14 ARE ONE, THEN
		COM			# THE MODE SELECT SWITCH IS IN THE OFF
		MASK	BIT13-14	# POSITION, AND SO THE DAP SHOULD BE OFF,
		EXTEND			# WITH NO ATTITUDE ERROR DISPLAY.
		BZF	MOREIDLE

		CS	IMODES33
		MASK	BIT6
		CCS	A
		TCF	JUMPDSP
		CS	RCSFLAGS	# IMU NOT USABLE.  SET UP INITIALIZATION
		MASK	BIT3		# FLAG FOR ATT ERROR DISPLAY ROUTINE.
		ADS	RCSFLAGS
		TCF	SHUTDOWN

CHEKMORE	CAF	BIT10		# BIT 10 OF 30 IS PGNCS CONTROL OF S/C
		EXTEND
		RAND	CHAN30		# BITS IN 30 ARE INVERTED
		CCS	A
		TCF	MOREIDLE

		RETURN

# Page 1411
# DAPIDLER ENTRY.

DAPIDLER	LXCH	BANKRUPT	# INTERRUPT LEAD INS (CONTINUED)
		EXTEND
		QXCH	QRUPT

		CA	RCSFLAGS
		MASK	BIT13
		CCS	A		# CHECK IF 1/ACCJOB HAS BEEN SET UP SINCE
		TCF	CHECKUP		# THE LAST FRESH START OR RESTART.
		CA	BIT13
		ADS	RCSFLAGS	# BIT 13 IS 1.
		CAF	PRIO27
		TC	NOVAC		# SET UP JOB TO DO A LITTLE INITIALIZATION
		EBANK=	AOSQ		#   AND EXECUTE 1/ACCS.
		2CADR	1/ACCSET	# (WILL BRANCH TO MOREIDLE ON ACCSOKAY)

CHECKUP		TC	CHEKBITS	# CHECK TO SEE IF LM DAP IS TO GO ON AND
					#   DO ERROR DISPLAY.

		CAE	DAPBOOLS	# IF 1/ACCS HAS NOT BEEN COMPLETED, IDLE.
		MASK	ACCSOKAY	#   NOTE: ONLY FRESH START AND RESTART
		EXTEND			# 	  KNOCK THIS BIT DOWN.
		BZF	MOREIDLE

STARTDAP	TC	IBNKCALL	# ZERO ATTITUDE ERROR AND DESIRED RATES.
		FCADR	ZATTEROR
		CAF	ZERO		# ********** INITIALIZE: **********
		TS	TJP
		TS	TJU
		TS	TJV
		TS	OMEGAP		# RATES IN BODY (PILOT) COORDINATES.
		TS	OMEGAQ
		TS	OMEGAR
		TS	TRAPEDP
		TS	TRAPEDQ
		TS	TRAPEDR
		TS	AOSQ		# OFFSET ACCELERATION ESTIMATES.
		TS	AOSQ +1
		TS	AOSR
		TS	AOSR +1
		TS	ALPHAQ		# COPIES OF OFFSET ESTIMATES FOR DOWNLIST.
		TS	ALPHAR
		TS	NEGUQ
		TS	NEGUR
		TS	AOSQTERM	# QRAXIS RATE DERIVATION TERMS AND KALMAN
		TS	AOSRTERM	# FILTER INITIALIZATION TERMS.
		TS	QACCDOT		# DESCENT ACCELERATION DERIVATIVE EST.
		TS	RACCDOT
# Page 1412
		TS	ALLOWGTS	# AOSTASK FLAG FOR QRAXIS RCS CONTROL USE.
		TS	COTROLER	# DO TRYGTS ON FIRST PASS (WILL GO TO RCS)
		TS	INGTS		# RECOGNIZE FIRST GTS PASS AS SUCH.
		TS	QGIMTIMR	# STOP GIMBAL DRIVES.  (PROBABLY WOULD BE
		TS	RGIMTIMR	#   GOOD ENOUGH JUST TO INACTIVATE TIMERS)
		TS	OLDPMIN		# MINIMUM IMPULSE MODE ERASABLES
		TS	OLDQRMIN
		TS	PJETCTR		# INITIALIZE DOCKED JET INHIBITION
		TS	UJETCTR		# COUNTERS
		TS	VJETCTR
CALLGMBL	EQUALS	BIT5		# RCSFLAGS INITIALIZATION.
		CS	MANFLAG
		MASK	RCSFLAGS	# NEGUQ(R) HAVE BEEN GENERATED.
		TS	RCSFLAGS

# SET UP "OLD" MEASURED CDU ANGLES:

		EXTEND
		DCA	CDUX		# OLDXFORP AND OLDYFORP
		DXCH	OLDXFORP
		CA	CDUZ
		TS	OLDZFORQ
		CS	RCSFLAGS
		MASK	BIT12
		ADS	RCSFLAGS	# BIT 12 SET TO 1.
		CA	FOUR
		TS	SKIPU
		TS	SKIPV
		CA	POSMAX
		TS	TIME6
		TS	T6NEXT
		TS	T6FURTHA
		CA	ZERO
		TS	T6NEXT +1
		TS	T6FURTHA +1
		TS	NXT6ADR
		TS	NEXTP
		TS	NEXTU
		TS	NEXTV
		CS	TEN
		TS	DAPZRUPT	# JASK NOT IN PROGRESS, INITIALIZE NEG.
		CA	TWO
		TS	NPTRAPS
		TS	NQTRAPS
		TS	NRTRAPS
		EXTEND
		DCA	PAXADIDL
		DXCH	T5ADR
SETTIME5	CAF	MS100
		TS	TIME5
# Page 1413
		TCF	RESUME
		EBANK=	AOSQ
IDLERADR	2CADR	DAPIDLER

MOREIDLE	TC	IBNKCALL	# CALCULATE Q,R-AXES ATTITUDE ERRORS.
		CADR	QERRCALC

		TC	IBNKCALL
		CADR	CALCPERR	# CALCULATE P AXIS ATTITUDE ERRORS.

SHUTDOWN	EXTEND
		DCA	IDLERADR
		DXCH	T5ADR

		CAF	ZERO		# KILL ANY POSSIBLE JET REQUESTS
		TS	NEXTP
		TS	NEXTU
		TS	NEXTV
		EXTEND			# COMMAND JETS OFF.
		WRITE	CHAN5
		EXTEND
		WRITE	CHAN6
		CS	BGIM23		# TURN TRIM GIMBAL OFF
		EXTEND
		WAND	CHAN12
		TCF	SETTIME5	# RETURN IN 100 MSEC.

MANFLAG		OCT	03021
BGIM23		OCTAL	07400
		EBANK=	OMEGAP
PAXADIDL	2CADR	PAXIS

MS100		=	OCT37766
COSMG		=	ITEMP1
JUMPDSP		EXTEND			# TRANSFER TO BANK 20
		DCA	DSPCADR		# FOR ATTITUDE ERROR DISPLAYS
		DTCB

		EBANK=	AK
DSPCADR		2CADR	ALTDSPLY

# Page 1414
		BANK	20
		SETLOC	DAPS3
		BANK
		COUNT*	$$/NEEDL

# PROGRAM: ALTDSPLY
#
# MOD 0.  6 DEC 1967
#
# AUTHOR:  CRAIG WORK, DON KEENE, MIT IL
#
# MOD 3 BY DON KEENE AUG 1, 1968 MOVED PROGRAM TO BANK 20
#
# PROGRAM DESCRIPTION:
#
# ALTDSPLY REVERSES THE DSPLYALT BIT OF RCSFLAGS EACH TIME IT IS CALLED, WHICH IS PRESUMABLY EVERY 100 MS.
# IF THE REVERSED BIT IS ONE, NEEDLER IS CALLED TO DISPLAY ATTITUDE ERRORS.  IF THE BIT IS ZERO, THE ATTITUDE ERR-
# ORS ARE CALCULATED AS 1) DAP FOLLOWING ERRORS, IF NEEDLFLG = 0, AND 2) TOTAL ATTITUDE ERRORS FOR NEEDLFLG = 1.
#
# WARNING:  ALTDSPLY MAY ONLY BE CALLED WITH INTERRUPT INHIBITED.
#
# WARNING:  EBANK MUST BE SET TO 6 WHEN USING THIS ROUTINE.
#
# INPUT:  RCSFLAGS AND 1) IF NEEDLFLG=0, INPUT PERROR,QERROR,RERROR.
# 		       2) IF NEEDLFLG=1, INPUT CPHI,CTHETA,CPSI,CDUX,CDUY,CDUZ,M11,M21,M32,M22,M32. (GPMATRIX)
#
# OUTPUTS:  RCSFLAGS WITH DSPLYALT REVERSED,AK,AK1,AK2,+ NEEDLER OUTPUTS.
#
# ENTRY:   TCF    ALTDSPLY
#
# EXIT:    TCF    CHEKMORE
#
# ALARM OR ABORT EXITS:  NONE
#
# SUBPROGRAMS CALLED: NEEDLER, OVERSUB2
#
# DEBRIS:  A,L,AND NEEDLER DEBRIS.

ALTDSPLY	CA	RCSFLAGS	# INVERT THE DISPLAY ALTERNATION BIT.
		TS	L
		CA	DSPLYALT
		EXTEND
		RXOR	LCHAN
		TS	RCSFLAGS

		MASK	DSPLYALT
		CCS	A		# IS ALTERNATION FLAG ZERO?
		TCF	NEEDLER

		CAE	FLAGWRD0	# NEEDLFLG WILL INDICATE TOTAL OR DAP AT-
# Page 1415
		MASK	NEEDLBIT	# TITUDE ERROR DISPLAY REQUEST.
		CCS	A
		TCF	DSPLYTOT	# TOTAL ERROR IS NEEDED IN AK,AK +1,AK +2

		CS	QERROR		# YES. DISPLAY ATT ERRORS ON THE ,-BALL.
		TS	AK +1		# ERROR COMPLEMENTS ARE INPUT TO NEEDLER.
		CS	RERROR
		TS	AK +2
		CS	PERROR
		XCH	AK

		TCF	RETNMORE	# DISPLAY THESE THE NEXT TIME THROUGH

# CALCULATE GIMBAL ANGLE TOTAL ERRORS, RESOLVE INTO PILOT AXES, STORE TOTAL ERRORS FOR NEEDLER.  Q-AXIS FIRST.

DSPLYTOT	EXTEND
		QXCH	ITEMP1		# SAVE Q FOR CHEKBITS RETURN.

		CA	CTHETA		# DESIRED ATTITUDE, Y-AXIS, 2'S COMP.
		EXTEND			# SUBTRACT CURRENT ATTITUDE.
		MSU	CDUY		# DIFFERENCE SCALED AT PI, 1'S COMP.
		TS	AK		# SAVE FOR R-ERROR CALCULATION.
		EXTEND
		MP	M21		# (CHTETA-CDUY)*M21 SCALED AT PI RADIANS.
		XCH	AK +1		# STORE FIRST TERM OF Q ERROR.
		CA	CPSI		# DESIRED ATTITUDE,Z-AXIS, 2'S COMP.
		EXTEND			# SUBTRACT CURRENT ATTITUDE.
		MSU	CDUZ		# DIFFERENCE SCALED AT PI, 1'S COMP.
		TS	AK +2		# SAVE Z-AXIS TERM FOR R ERROR CALCULATION
		EXTEND
		MP	M22		# (CPSI-CDUZ)*M22, SCALED AT PI RADIANS.
		AD	AK +1		# Q ERROR COMPLETE	   , AT PI RAD.
		TC	OVERSUB2	# PIN NEEDLES IN CASE OF OVERFLOW
		TS	AK +1

# R ERROR CALCULATION NEXT.

		CA	AK		# Y-AXIS DIFFERENCE STORED BY Q-AXIS CALC.
		EXTEND
		MP	M31		# (CTHETA-CDUY)*M31, SCALED AT PI RADIANS.
		XCH	AK +2		# FIRST TERM OF R ERROR.
					# Z-AXIS DIFFERENCE, STORED BY A CALC. IS
		EXTEND			# RECOVERED BY THE EXCHANGE.
		MP	M32		# (CPSI-CDUZ)*M32, SCALED AT PI RADIANS.
		AD	AK +2		# R ERROR COMPLETE	   , AT PI RAD.
		TC	OVERSUB2	# PIN NEEDLES IN CASE OF OVERFLOW.
		TS	AK +2

# NOW CALCULATE P ERROR.  (NOTE THAT M13 = 1, SCALED AT 1, SO THE MULTIPLICATION IS BY-PASSED.)
# Page 1416
		CA	AK		# Y-AXIS DIFFERENCE STORED BY Q AXIS CALC.
		EXTEND
		MP	M11		# (CTHETA-CDUY)*M11 SCALED AT PI RADIANS.
		XCH	AK		# FIRST TERM OF P ERROR IN AK, AT PI RAD.
		CAE	CPHI		# DESIRED ATTITUDE, X-AXIS, 2'S COMP.
		EXTEND			# SUBTRACT CURRENT X ATTITUDE.
		MSU	CDUX		# X-AXIS DIFFERENCE, 1'S COMP, AT PI RAD.

# M13 = 1, SO BYPASS THE MULTIPLICATION.
#		EXTEND
#		MP	M13		  (CPHI-CDUX)*M13 SCALED AT PI RADIANS.

		AD	AK		# P ERROR COMPLETE	, SCALED AT PI RAD
		TC	OVERSUB2	# PIN NEEDLES IN CASE OF OVERFLOW.
		TS	AK

		EXTEND
		QXCH	ITEMP1		# RESTORE Q FOR CHEKBITS RETURN.

		TCF	RETNMORE	# DISPLAY THESE THE NEXT TIME THROUGH

# Page 1417
# FDAI ATTITUDE ERROR DISPLAY SUBROUTINE
#
# PROGRAM DESCRIPTION:    D. KEENE   5/24/67
#
# MOD 1 BY CRAIG WORK, 12 DEC 67
#
# MOD 2 BY CRAIG WORK, 6 APRIL 68 CONVERTS ATTITUDE ERROR DISPLAY SCALING FROM 16 7/8 DEG. TO 42 3/16 DEGREES.
#
#     THIS SUBROUTINE IS USED TO DISPLAY ATTITUDE ERRORS ON THE FDAI VIA THE DIGITAL TO ANALOG CONVERTERS (DACS)
# IN THE CDUS.  CARE IS TAKEN TO METER OUT THE APPROPRIATE NUMBER OF PULSES TO THE IMU ERROR COUNTERS AND PREVENT
# OVERFLOW, TO CONTROL THE RELAY SEQUENCING, AND TO AVOID INTERFERENCE WITH THE COARSE ALIGN LOOP WHICH ALSO USES
# THE DACS.
#
#
# CALLING SEQUENCE:
#
#     DURING THE INITIALIZATION SECTION OF THE USER'S PROGRAM, BIT3 OF RCSFLAGS SHOULD BE SET TO INITIATE THE
# TURN-ON SEQUENCE WITHIN THE NEEDLES PROGRAM:
#
#	   CS	  RCSFLAGS	  IN EBANK6
#	   MASK	  BIT3
#	   ADS	  RCSFLAGS
#
# THEREAFTER, THE ATTITUDE ERRORS GENERATED BY THE USER SHOULD BE TRANSFERRED TO THE FOLLOWING LOCATIONS IN EBANK6:
#
#	   AK	  SCALED 180 DEGREES  NOTE: THESE LOCATIONS ARE SUBJECT
#	   AK1	  SCALED 180 DEGREES	    TO CHANGE
#	   AK2	  SCALED 180 DEGREES
#
# FULL SCALED DEFLECTION OF THE NEEDLES CORRESPONDS TO 5 1/16 DEGREES, WHILE 384 BITS IN THE IMU ERROR COUNTER
# CORRESPONDS TO 42 3/16 DEGREES.  (DAC MAXIMUM CAPACITY IS 384 BITS.) 46 BITS EFFECTIVELY PIN THE NEEDLES.
#
# A CALL TO NEEDLER WILL THEN UPDATE THE DISPLAY:
#
#	   INHINT
#	   TC	  IBNKCALL	 NOTE: EBANK SHOULD BE SET TO E6
#	   CADR	  NEEDLER
#	   RELINT
#
#     THIS PROCESS SHOULD BE REPEATED EACH TIME THE ERRORS ARE UPDATED.  AT LEAST 3 PASSES THRU THE PROGRAM ARE
# REQUIRED BEFORE ANYTHING IS ACTUALLY DISPLAYED ON THE ERROR METERS.
# NOTE: EACH CALL TO NEEDLER MUST BE SEPARATED BY AT LEAST 50MS TO ASSURE PROPER RELAY SEQUENCING.
#
# ERASABLES USED:
#		       AK	  CDUXCMD
#		       AK1	  CDUYCMD
#		       AK2	  CDUZCMD
#		       EDRIVEX	  A,L,Q
#		       EDRIVEY	  T5TEMP
#		       EDRIVEZ	  DINDX
# Page 1418
#
# SWITCHES:	       RCSFLAGS	  BITS 3,2
#
# I/O CHANNELS:	       CHAN12	  BIT 4 (COARSE ALIGN - READ ONLY)
#		       CHAN12	  BIT 6 (IMU ERROR COUNTER ENABLE)
#		       CHAN14	  BIT 13,14,15 (DAC ACTIVITY)
#
#
# SIGN CONVENTION<   AK = THETAC - THETA
#	    WHERE    THETAC = COMMAND ANGLE
#		     THETA  = PRESENT ANGLE


NEEDLER		CA	RCSFLAGS
		MASK	SIX
		EXTEND
		BZF	NEEDLES3
		MASK	BIT3
		EXTEND
		BZF	NEEDLER2	# BIT3 = 0, BIT2 = 1

		CS	BIT6		# FIRST PASS BIT3 = 1
		EXTEND			# DISABLE IMU ERROR COUNTER TO ZERO DACS
		WAND	CHAN12		# MUST WAIT AT LEAST 60 MS BEFORE
NEEDLE11	CS	ZERO		# ENABLING COUNTERS.
		TS	AK		# ZERO THE INPUTS ON FIRST PASS
		TS	AK1
		TS	AK2
		TS	EDRIVEX		# ZERO THE DISPLAY REGISTERS
		TS	EDRIVEY
		TS	EDRIVEZ
		TS	CDUXCMD		# ZERO THE OUT COUNTERS
		TS	CDUYCMD
		TS	CDUZCMD
		CS	SIX		# RESET RCSFLAGS FOR PASS2
		MASK	RCSFLAGS
		AD	BIT2
		TS	RCSFLAGS
		TCF	RETNMORE

NEEDLER2	CAF	BIT6		# ENABLE IMU ERROR COUNTERS
		EXTEND
		WOR	CHAN12
		CS	SIX		# RESET RCSFLAGS TO DISPLAY ATTITUDE
		MASK	RCSFLAGS	# ERRORS    WAIT ATLEAST 4 MS FOR
		TS	RCSFLAGS	# RELAY CLOSURE
		TCF	RETNMORE

NEEDLES3	CAF	BIT6		# CHECK TO SEE IF IMU ERROR COUNTER
		EXTEND			# IS ENABLED
		RAND	CHAN12
# Page 1419
		CCS	A		# IF NOT, RE-INITIALIZE NEEDLER.
		TCF	NEEDLES

		CS	RCSFLAGS	# SET UP INITIALIZATION FLAG IN RCSFLAGS.
		MASK	BIT3
		ADS	RCSFLAGS
		TCF	RETNMORE

NEEDLES		CAF	TWO
DACLOOP		TS	DINDX
		CS	ONETENTH	# RESCALE INPUTS TO + OR - 1800 DEGREES.
		EXTEND
		INDEX	DINDX
		MP	AK
		TS	L
		CCS	A
		CA	DACLIMIT
		TCF	+2
		CS	DACLIMIT
		AD	L
		TS	T5TEMP		# OVFLO CHK
		TCF	+4
		INDEX	A		# ON OVERFLOW LIMIT OUTPUT TO +-384
		CAF	DACLIMIT
		TS	L
		INDEX	DINDX
		CS	EDRIVEX		# CURRENT VALUE OF DAC
		AD	L
		INDEX	DINDX
		ADS	CDUXCMD
		INDEX	DINDX
		LXCH	EDRIVEX
		CCS	DINDX
		TCF	DACLOOP
		CAF	13,14,15
		EXTEND
		WOR	CHAN14		# SET DAC ACTIVITY BITS
		TCF	RETNMORE

		DEC	-384
DACLIMIT	DEC	16000
		DEC	384

ONETENTH	OCT	03146		# DECIMAL +0.1, SCALED AT 1.
DSPLYALT	EQUALS	BIT4		# 100 MS ALTERNATION BIT IN RCSFLAGS

OVERSUB2	TS	7		# RETURNS  A  UNCHANGED  OR LIMITED TO
		TC	Q		# POSMAX OR NEGMAX IF A HAS OVERFLOW
		INDEX	A
# Page 1420
		CS	LIMITS		# DUPLICATE CODING IN  BANK 16
		TC	Q

RETNMORE	EXTEND			# RETURN TO CHEKMORE
		DCA	MORECADR
		DTCB

		EBANK=	AOSQ
MORECADR	2CADR	CHEKMORE