Apollo-11/Luminary099/THE_LUNAR_LANDING.s

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# Copyright: Public domain.
# Filename: THE_LUNAR_LANDING.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: Hartmuth Gutsche<hgutsche@xplornet.com>.
# Website: www.ibiblio.org/apollo.
# Pages: 785-792
# Mod history: 2009-05-20 HG Transcribed from 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 2021112-61
# 16:27 JULY 14, 1969
# Page 785
BANK 32
SETLOC F2DPS*32
BANK
EBANK= E2DPS
# *************************************
# P63: THE LUNAR LANDING, BRAKING PHASE
# *************************************
COUNT* $$/P63
P63LM TC PHASCHNG
OCT 04024
TC BANKCALL # DO IMU STATUS CHECK ROUTINE R02
CADR R02BOTH
CAF P63ADRES # INITIALIZE WHICH FOR BURNBABY
TS WHICH
CAF DPSTHRSH # INITIALIZE DVMON
TS DVTHRUSH
CAF FOUR
TS DVCNTR
CS ONE # INITIALIZE WCHPHASE AND FLPASS0
TS WCHPHASE
CA ZERO
TS FLPASS0
CS BIT14
EXTEND
WAND CHAN12 # REMOVE TRACK-ENABLE DISCRETE.
FLAGORGY TC INTPRET # DIONYSIAN FLAG WAVING
CLEAR CLEAR
NOTHROTL
REDFLAG
CLEAR SET
LRBYPASS
MUNFLAG
CLEAR CLEAR
P25FLAG # TERMINATE P25 IF IT IS RUNNING.
RNDVZFLG # TERMINATE P20 IF IT IS RUNNING.
# ********************************
IGNALG SETPD VLOAD # FIRST SET UP INPUTS FOR RP-TO-R:
# Page 786
0 # AT 0D LANDING SITE IN MOON FIXED FRAME
RLS # AT 6D ESTIMATED TIME OF LANDING
PDDL PUSH # MPAC NON-ZERO TO INDICATE LUNAR CASE
TLAND
STCALL TPIP # ALSO SET TPIP FOR FIRST GUIDANCE PASS
RP-TO-R
VSL4 MXV
REFSMMAT
STCALL LAND
GUIDINIT # GUIDINIT INITIALIZES WM AND /LAND/
DLOAD DSU
TLAND
GUIDDURN
STCALL TDEC1 # INTEGRATE STATE FORWARD TO THAT TIME
LEMPREC
SSP VLOAD
NIGNLOOP
40D
UNITX
STOVL CG
UNITY
STOVL CG +6
UNITZ
STODL CG +14
99999CON
STOVL DELTAH # INITIALIZE DELTAH FOR V16N68 DISPLAY
ZEROVECS
STODL UNFC/2 # INITIALIZE TRIM VELOCITY CORRECTION TERM
HI6ZEROS
STORE TTF/8
IGNALOOP DLOAD
TAT
STOVL PIPTIME1
RATT1
VSL4 MXV
REFSMMAT
STCALL R
MUNGRAV
STCALL GDT/2
?GUIDSUB # WHICH DELIVERS N PASSES OF GUIDANCE
# DDUMCALC IS PROGRAMMED AS FOLLOWS:
# 2 ___
# (RIGNZ - RGU )/16 + 16(RGU )KIGNY/B8 + (RGU - RIGNX)KIGNX/B4 + (ABVAL(VGU) - VIGN)KIGNV/B4
# 2 1 0
# DDUM = -------------------------------------------------------------------------------------------
# 10
# 2 (VGU - 16 VGU KIGNX/B4)
# 2 0
# Page 787 new page is actually one line earlier but this would put the indices on a seperate line
# disconnected from their respective variables
# THE NUMERATOR IS SCALED IN METERS AT 2(28). THE DENOMINATOR IS A VELOCITY IN UNITS OF 2(10) M/CS.
# THE QUOTIENT IS THUS A TIME IN UNITS OF 2(18) CENTISECONDS. THE FINAL SHIFT RESCALES TO UNITS OF 2(28) CS.
# THERE IS NO DAMPING FACTOR. THE CONSTANTS KIGNX/B4, KIGNY/B8 AND KIGNV/B4 ARE ALL NEGATIVE IN SIGN.
DDUMCALC TS NIGNLOOP
TC INTPRET
DLOAD DMPR # FORM DENOMINATOR FIRST
VGU
KIGNX/B4
SL4R BDSU
VGU +4
PDDL DSU
RIGNZ
RGU +4
SR4R PDDL
RGU +2
DSQ DMPR
KIGNY/B8
SL4R PDDL
RGU
DSU DMPR
RIGNX
KIGNX/B4
PDVL ABVAL
VGU
DSU DMPR
VIGN
KIGNV/B4
DAD DAD
DAD DDV
SRR
10D
PUSH DAD
PIPTIME1
STODL TDEC1 # STORE NEW GUESS FOR NEXT INTEGRATION
ABS DSU
DDUMCRIT
BMN CALL
DDUMGOOD
INTSTALL
SET SET
INTYPFLG
MOONFLAG
DLOAD
PIPTIME1
STOVL TET # HOPEFULLY ?GUIDSUB DID NOT
RATT1 # CLOBBER RATT1 AND VATT1
# Page 788
STOVL RCV
VATT1
STCALL VCV
INTEGRVS
GOTO
IGNALOOP
DDUMGOOD SLOAD SR
ZOOMTIME
14D
BDSU
TDEC1
STOVL TIG # COMPUTE DISTANCE LANDING SITE WILL BE
V # OUT OF LM'S ORBITAL PLANE AT IGNITION:
VXV UNIT # SIGN IS + IF LANDING SITE IS TO THE
R # RIGHT, NORTH; - IF TO THE LEFT, SOUTH.
DOT SL1
LAND
R60INIT STOVL OUTOFPLN # INITIALIZATION FOR CALCMANU
UNFC/2
STORE R60VSAVE # STORE UNFC/2 TEMPORARILY IN R60SAVE
EXIT
# *******************************************
IGNALGRT TC PHASCHNG # PREVENT REPEATING IGNALG
OCT 04024
ASTNCLOK CS ASTNDEX
TC BANKCALL
CADR STCLOK2
TCF ENDOFJOB # RETURN IN NEW JOB AND IN EBANK FIVE
ASTNRET TC INTPRET
SSP RTB # GO PICK UP DISPLAY AT END OF R51:
QMAJ # "PROCEED" WILL DO A FINE ALIGNMENT
FCADR P63SPOT2 # "ENTER" WILL RETURN TO P63SPOT2
R51P63
P63SPOT2 VLOAD UNIT # INITIALIZE KALCMANU FOR BURN ATTITUDE
R60VSAVE
STOVL POINTVSM
UNITX
STORE SCAXIS
EXIT
CAF EBANK7
TS EBANK
INHINT
TC IBNKCALL
CADR PFLITEDB
# Page 789
RELINT
TC BANKCALL
CADR R60LEM
TC PHASCHNG # PREVENT RECALLING R60
OCT 04024
P63SPOT3 CA BIT6 # IS THE LR ANTENNA IN POSITION 1 YET
EXTEND
RAND CHAN33
EXTEND
BZF P63SPOT4 # BRANCH IF ANTENNA ALREADY IN POSITION 1
CAF CODE500 # ASTRONAUT: PLEASE CRANK THE
TC BANKCALL # SILLY THING AROUND
CADR GOPERF1
TCF GOTOP00H # TERMINATE
TCF P63SPOT3 # PROCEED SEE IF HE'S LYING
P63SPOT4 TC BANKCALL # ENTER INITIALIZE LANDING RADAR
CADR SETPOS1
TC POSTJUMP # OFF TO SEE THE WIZARD ...
CADR BURNBABY
# ---------------------------------
# CONSTANTS FOR P63LM AND IGNALG
P63ADRES GENADR P63TABLE
ASTNDEX = MD1 # OCT 25: INDEX FOR CLOKTASK
CODE500 OCT 00500
99999CON 2DEC 30479.7 B-24
GUIDDURN 2DEC +66440 # GUIDDURN +6.64400314 E+2
DDUMCRIT 2DEC +8 B-28 # CRITERION FOR IGNALG CONVERGENCE
# Page 790
# --------------------------------
# Page 791
# *************************
# P68: LANDING CONFIRMATION
# *************************
BANK 31
SETLOC F2DPS*31
BANK
COUNT* $$/P6567
LANDJUNK TC PHASCHNG
OCT 04024
INHINT
TC BANKCALL # ZERO ATTITUDE ERROR
CADR ZATTEROR
TC BANKCALL # SET 5 DEGREE DEADBAND
CADR SETMAXDB
TC INTPRET # TO INTERPRETIVE AS TIME IS NOT CRITICAL
SET CLEAR
SURFFLAG
LETABORT
SET VLOAD
APSFLAG
RN
STODL ALPHAV
PIPTIME
SET CALL
LUNAFLAG
LAT-LONG
SETPD VLOAD # COMPUTE RLS AND STORE IT AWAY
0
RN
VSL2 PDDL
PIPTIME
PUSH CALL
R-TO-RP
STORE RLS
EXIT
CAF V06N43* # ASTRONAUT: NOW LOOK WHERE TO ENDED UP
TC BANKCALL
CADR GOFLASH
TCF GOTOP00H # TERMINATE
TCF +2 # PROCEED
TCF -5 # RECYCLE
TC INTPRET
# Page 792
VLOAD # INITIALIZE GSAV AND (USING REFMF)
UNITX # YNBSAV, ZNBSAV AND ATTFLAG FOR P57
STCALL GSAV
REFMF
EXIT
TCF GOTOP00H # ASTRONAUT: PLEASE SELECT P57
V06N43* VN 0643