https://github.com/virtualagc/virtualagc
Revision 078c79d8734a9ed2860303a7c1662004284fe853 authored by Ron Burkey on 07 August 2022, 15:04:04 UTC, committed by Ron Burkey on 07 August 2022, 15:04:04 UTC
assembly listings from yaASM and yaLEMAP. Added some debugging messages to 'make install'. Tweaked debugging messages that VirtualAGC embeds in 'simulate'. Verified buildability in Mint 21, 20, 19, 17, and verified buildability using clang in Mint 17.
1 parent 6bb1acc
Tip revision: 078c79d8734a9ed2860303a7c1662004284fe853 authored by Ron Burkey on 07 August 2022, 15:04:04 UTC
Fixed a potential string-overflow bug in yaASM. Removed timestamps from
Fixed a potential string-overflow bug in yaASM. Removed timestamps from
Tip revision: 078c79d
THROTTLE_CONTROL_ROUTINES.agc
### FILE="Main.annotation"
## Copyright: Public domain.
## Filename: THROTTLE_CONTROL_ROUTINES.agc
## Purpose: A section of LUM69 revision 2.
## It is part of the reconstructed source code for the flown
## version of the flight software for the Lunar Module's (LM)
## Apollo Guidance Computer (AGC) for Apollo 10. The code has
## been recreated from a copy of Luminary revsion 069, using
## changes present in Luminary 099 which were described in
## Luminary memos 75 and 78. The code has been adapted such
## that the resulting bugger words exactly match those specified
## for LUM69 revision 2 in NASA drawing 2021152B, which gives
## relatively high confidence that the reconstruction is correct.
## Reference: pp. 797-801
## Assembler: yaYUL
## Contact: Ron Burkey <info@sandroid.org>.
## Website: www.ibiblio.org/apollo/index.html
## Mod history: 2019-07-27 MAS Created from Luminary 69.
## Page 797
BANK 31
SETLOC FTHROT
BANK
EBANK= PIF
COUNT* $$/THROT
# * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * *
# HERE FC, DESIRED THRUST, AND FP, PRESENT THRUST, UNWEIGHTED, ARE COMPUTED.
THROTTLE CA ABDELV # COMPUTE PRESENT ACCELERATION IN UNITS OF
EXTEND # 2(-4) M/CS/CS, SAVING SERVICER TROUBLE
MP /AF/CNST
+3 EXTEND
QXCH RTNHOLD
AFDUMP TC MASSMULT
DXCH FP # FP = PRESENT THRUST
EXTEND
DCA /AFC/
TC MASSMULT
TS FC # FC = THRUST DESIRED BY GUIDANCE
DXCH FCODD # FCODD = WHAT IT IS GOING TO GET
# IF IT HAS BEEN LESS THAN 3 SECONDS SINCE THE LAST THROTTLING, AUGMENT FP USING THE FWEIGHT CALCULATED THEN.
CS TTHROT # THIS CODING ASSUMES A FLATOUT WITHIN
AD TIME1 # 80 SECONDS BEFORE FIRST THROTTLE CALL
MASK POSMAX
COM
AD 3SECS
EXTEND
BZMF WHERETO # BRANCH IF (TIME1-TTHROT +1) > 3 SECONDS
EXTEND
DCA FWEIGHT
DAS FP
# THIS LOGIC DETERMINES THE THROTTLING IN THE REGION 10% - 94%. THE MANUAL THROTTLE, NOMINALLY SET AT
# MINIMUM BY ASTRONAUT OR MISSION CONTROL PROGRAMS, PROVIDES THE LOWER BOUND. A STOP IN THE THROTTLE HARDWARE
# PROVIDES THE UPPER.
WHERETO CA EBANK5 # INITIALIZE L*WCR*T AND H*GHCR*T FROM
TS EBANK # PAD LOADED ERASABLES IN W-MATRIX
## Page 798
EBANK= LOWCRIT
EXTEND
DCA LOWCRIT
DXCH L*WCR*T
CA EBANK7
TS EBANK
EBANK= PIF
CS ZERO # INITIALIZE PIFPSET
TS PIFPSET
CS H*GHCR*T
AD FCOLD
EXTEND
BZMF LOWFCOLD # BRANCH IF FCOLD < OR = HIGHCRIT
CS L*WCR*T
AD FCODD
EXTEND
BZMF FCOMPSET # BRANCH IF FC < OR = LOWCRIT
CA FP # SEE NOTE 1
TCF FLATOUT1
FCOMPSET CS FMAXODD # SEE NOTE 2
AD FP
TCF FLATOUT2
LOWFCOLD CS H*GHCR*T
AD FCODD
EXTEND
BZMF DOPIF # BRANCH IF FC < OR = HIGHCRIT
CA FLAGWRD6 # IS POUTFLAG SET?
MASK POUTBIT
EXTEND
BZF FLATOUT1 -1
CA H*GHCR*T # YES: THROTTLE-UP ONLY TO HIGHCRIT
TS FCODD
TCF DOPIF
CA FMAXPOS # NO: THROTTLE-UP
FLATOUT1 DXCH FCODD
CA FEXTRA
FLATOUT2 TS PIFPSET
# NOTE 1 FC IS SET EQUAL TO FP SO PIF WILL BE ZERO. THIS IS DESIRABLE
# AS THERE IS ACTUALLY NO THROTTLE CHANGE.
#
# NOTE2 HERE, SINCE WE ARE ABOUT TO RETURN TO THE THROTTLEABLE REGION
# (BELOW 55%) THE QUANTITY -(FMAXODD-FP) IS COMPUTED AND PUT
# INTO PIFPSET TO COMPENSATE FOR THE DIFFERENCE BETWEEN THE
# NUMBER OF BITS CORRESPONDING TO FULL THROTTLE (FMAXODD) AND THE
## Page 799
# NUMBER CORRESPONDING TO ACTUAL THRUST (FP). THUS THE TOTAL
# THROTTLE COMMAND PIF = FC - FP - (FMAXODD - FP) = FC - FMAXODD.
DOPIF TC FASTCHNG # RESTART PROTECTION
EXTEND
DCA FCODD
TS FCOLD
DXCH PIF
EXTEND
DCS FP
DAS PIF # PIF = FC - FP, NEVER EQUALS +0
DOIT CA PIF
AD PIFPSET # ADD IN PIFPSET, WITHOUT CHANGING PIF
TS PSEUDO55
TS THRUST
CAF BIT4
EXTEND
WOR CHAN14
CA TIME1
TS TTHROT
# SINCE /AF/ IS NOT AN INSTANTANEOUS ACCELERATION, BUT RATHER AN "AVERAGE" OF THE ACCELERATION LEVELS DURING
# THE PRECEEDING PIPA INTERVAL, AND SINCE FP IS COMPUTED DIRECTLY FROM /AF/, FP IN ORDER TO CORRESPOND TO THE
# ACTUAL THRUST LEVEL AT THE END OF THE INTERVAL MUST BE WEIGHTED BY
#
# PIF(PPROCESS + TL) PIF /PIF/
# FWEIGHT = ------------------ + -------------
# PGUID 2 PGUID FRATE
#
# WHERE PPROCESS IS THE TIME BETWEEN PIPA READING AND THE START OF THROTTLING, PGUID IS THE GUIDANCE PERIOD, AND
# FRATE IS THE THROTTLING RATE (32 UNITS PER CENTISECOND). PGUID IS ASSUMED TO BE 2 SECONDS. THE "TL" IN THE
# FIRST TERM REPRESENTS THE ENGINE'S RESPONSE LAG. HERE FWEIGHT IS COMPUTED FOR USE NEXT PASS.
CA 4SECS
TS Q
CS PIPTIME +1 # TIME OF LAST PIPA READING
AD TIME1
AD THROTLAG # COMPENSATE FOR ENGINE RESPONSE LAG
MASK LOW8 # MAKE SURE SMALL AND POSITIVE
ZL
EXTEND
DV Q
EXTEND
MP PIF
DOUBLE
DXCH FWEIGHT
CA 2.PG.FRT
TS Q
## Page 800
CCS PIF
AD ONE
TCF +2
AD ONE
EXTEND
MP PIF
EXTEND
DV Q
ZL
DAS FWEIGHT
THDUMP TC RTNHOLD
# FLATOUT THROTTLES UP THE DESCENT ENGINE, AND IS CALLED AS A BASIC SUBROUTINE.
FLATOUT CAF BIT13 # 4096 PULSES
WHATOUT TS PIFPSET # USE PIFPSET SO FWEIGHT WILL BE ZERO
CS ZERO
TS FCOLD
TS PIF
EXTEND
QXCH RTNHOLD
TCF DOIT
# MASSMULT SCALES ACCELERATION, ARRIVING IN A AND L IN UNITS OF 2(-4) M/CS/CS, TO FORCE IN PULSE UNITS.
MASSMULT EXTEND
QXCH BUF
EXTEND
MP MASS # LEAVES ODDLY SCALED FORCE IN A AND L
DXCH MPAC
TC DMP # LEAVES PROPERLY SCALED FORCE IM MPAC
ADRES SCALEFAC
TC TPAGREE
CA MPAC
EXTEND
BZF +3
CAF POSMAX
TC BUF
DXCH MPAC +1
TC BUF
# CONSTANTS:-
FEXTRA = BIT13
## Page 801
2.PG.FRT = PRIO31 # DECIMAL 12800
/AF/CNST DEC .13107
# * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * *
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