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
LUNAR_LANDING_GUIDANCE_EQUATIONS.agc
### FILE="Main.annotation"
## Copyright: Public domain.
## Filename: LUNAR_LANDING_GUIDANCE_EQUATIONS.agc
## Purpose: A section of Luminary revision 173.
## It is part of the reconstructed source code for the second
## (unflown) release of the flight software for the Lunar
## Module's (LM) Apollo Guidance Computer (AGC) for Apollo 14.
## The code has been recreated from a reconstructed copy of
## Luminary 178, as well as Luminary memo 167 (revision 1).
## It has been adapted such that the resulting bugger words
## exactly match those specified for Luminary 173 in NASA
## drawing 2021152N, which gives relatively high confidence
## that the reconstruction is correct.
## Reference: pp. 784-821
## Assembler: yaYUL
## Contact: Ron Burkey <info@sandroid.org>.
## Website: www.ibiblio.org/apollo/index.html
## Mod history: 2019-09-18 MAS Created from Luminary 178.
## 2019-09-21 MAS Added calculation of VBIAS back to STRTP66A.
## Moved the setting of RODFLAG into interpretive
## alongside VBIAS calculation. Also added back
## the definition of BIASFACT.
## Page 794
EBANK= E2DPS
COUNT* $$/F2DPS
# ****************************************************************************************************************
# LUNAR LANDING FLIGHT SEQUENCE TABLES
# ****************************************************************************************************************
# FLIGHT SEQUENCE TABLES ARE ARRANGED BY FUNCTION. THEY ARE REFERENCED USING AS AN INDEX THE REGISTER WCHPHASE:
# WCHPHASE = -1 ---> IGNALG
# WCHPHASE = 0 ---> BRAKQUAD
# WCHPHASE = 1 ---> APPRQUAD
# WCHPHASE = 2 ---> VERTICAL
# ***************************************************************************************************************
# ROUTINES FOR STARTING NEW GUIDANCE PHASES:
TCF TTFINCR # IGNALG
NEWPHASE TCF TTFINCR # BRAKQUAD
TCF STARTP64 # APPRQUAD
TCF STARTP66 # VERTICAL
#
# PRE-GUIDANCE COMPUTATIONS:
TCF CALCRGVG # IGNALG
PREGUIDE TCF RGVGCALC # BRAKQUAD
TCF REDESIG # APPRQUAD
#
# GUIDANCE EQUATIONS:
TCF TTF/8CL # IGNALG
WHATGUID TCF TTF/8CL # BRAKQUAD
TCF TTF/8CL # APPRQUAD
#
# POST GUIDANCE EQUATION COMPUTATIONS:
TCF CGCALC # IGNALG
AFTRGUID TCF EXTLOGIC # BRAKQUAD
TCF EXTLOGIC # APPRQUAD
## Page 795
# WINDOW VECTOR COMPUTATIONS:
TCF EXGSUB # IGNALG
WHATEXIT TCF EXBRAK # BRAKQUAD
TCF EXNORM # APPRQUAD
#
# DISPLAY ROUTINES:
WHATDISP TCF P63DISPS # BRAKQUAD
TCF P64DISPS # APPRQUAD
TCF VERTDISP # VERTICAL
#
# ALARM ROUTINE FOR TTF COMPUTATION:
TCF 1406POO # IGNALG
WHATALM TCF 1406ALM # BRAKQUAD
TCF 1406ALM # APPRQUAD
#
# INDICES FOR REFERENCING TARGET PARAMETERS:
OCT 0 # IGNALG
TARGTDEX OCT 0 # BRAKQUAD
OCT 2 # APPRQUAD
## Page 796
# ****************************************************************************************************************
# ENTRY POINTS: ?GUIDSUB FOR THE IGNITION ALGORITHM, LUNLAND FOR SERVOUT
# ****************************************************************************************************************
# IGNITION ALGORITHM ENTRY: DELIVERS N PASSES OF QUADRATIC QUIDANCE
?GUIDSUB EXIT
CAF TWO # N = 3
TS NGUIDSUB
TCF GUILDRET +2
GUIDSUB TS NGUIDSUB # ON SUCEEDING PASSES SKIP TTFINCR
TCF CALCRGVG
# NORMAL ENTRY: CONTROL COMES HERE FROM SERVOUT
LUNLAND TC PHASCHNG
OCT 00035 # GROUP 5: RETAIN ONLY PIPA TASK
CA FLAGWRD5 # HAS THROTTLE-UP COME YET?
MASK ZOOMBIT
EXTEND
BZF DISPEXIT +3 # NO: DO DISPLAYS ONLY
TC PHASCHNG # YES: DO GUIDANCE
OCT 05023
OCT 20000
## Page 797
# ****************************************************************************************************************
# GUILDENSTERN: AUTO-MODES MONITOR (R13)
# ****************************************************************************************************************
COUNT* $$/R13
# THE PHILOSOPHY OF GUILDENSTERN: ON EVERY APPEARANCE OF THE ATTITUDE-HOLD DISCRETE CHECK TO SEE IF THE ROD SWITCH
# HAS BEEN CLICKED. IF SO, SELECT P66. IF THE DAP IS IN AUTO AND THE PRESENT
# 9PROGRAM IN PROGRESS IS P66, CHECK FOR A
# RESTART. IF ONE HAS OCCURED RE-INITIALIZE P66 AND CONTINUE OTHERWISE YOUCONTINUE WITH PRESENT DATA IN P66.TO
# SELECT P66 THE ATTITUDE-HOLD DISCRETE MUST BE PRESENT AND THE ROD SWITCH MUST HAVE BEEN CLICKED. OTHERWISE THE
# AUTOMATIC LANDING WILL CONTINUE.
GUILDEN CS MODREG # ARE WE IN P66? (EVEN THO WE ARE IN AUTO
STERN AD DEC66 # DAP)
EXTEND
BZF RESTART? # YES: GO SE IF THERE HAS BEEN A RESTART
CAF BIT13 # NO: IS UN-ATTITUDE-HOLD DISCRETE HERE?
EXTEND
RAND CHAN31
CCS A
TCF GUILDRET # YES: ALL'S WELL, OR AT LEAST AUTOMATIC
CA RODCOUNT # NO: HAS ROD SWITCH BEEN CLICKED
EXTEND
BZF GUILDRET # NO: CONTINUE WITH THE AUTOMATIC LANDING
STARTP66 TC FASTCHNG # YES
TC NEWMODEX
DEC66 DEC 66
EXTEND
DCA HDOTDISP # SET DESIRED ALTITUDE RATE = CURRENT
DXCH VDGVERT # ALTITUDE RATE.
TC UPFLAG # SET FLAG TO CONTINUE P66 HORIZONTAL
ADRES P66PROFL # UNTIL 'PROCEED' AFTER TOUCHDOWN
CS TOOFEW # INITIALIZE CNTTHROT TO -TOOFEW
TS CNTTHROT
STRTP66A TC INTPRET
VLOAD VXV # COMPUTE HORIZONTAL VELOCITY COMMAND
WM # MOON'S ANGULAR RATE IN 2(-17)RAD/CS
R # LM POSITION IN 2(24)M
STORE VHZC
SLOAD PUSH # COMPUTE PIPA BIAS VECTOR FOR USE BY
PBIASZ # P66ROD AND LANDING ANALOG DISPLAYS
SLOAD PUSH
PBIASY
SLOAD VDEF
PBIASX
VXSC SET
BIASFACT
RODFLAG
STOVL VBIAS # ONE SECOND'S BIAS IN UNITS OF 2(7) M/CS
TEMX
VCOMP
STOVL OLDPIPAX
ZEROVECS
STODL DELVROD
## Page 798
RODSCALE
STODL RODSCAL1
PIPTIME
STORE LASTTPIP
EXIT
TC BANKCALL # REFER CURRENT PIPAX READING TO THE CM:
FCADR DEIMUBOB # ALAS, OMEGAQ AT PIPTIME NOT AVAILABLE
CAF ZERO
TS FCOLD
TS FWEIGHT
TS FWEIGHT +1
CAF TWO # WCHPHOLD=2 --> VERTICAL PHASE
TS WCHPHOLD
TS WCHPHASE
TC DOWNFLAG # PERMIT X-AXIS OVERRIDE
ADRES XOVINFLG # SHOULD DO INTERPRETIVELY TO SAVE A WORD
TC UPFLAG # TERMINATE TERRAIN MODEL
ADRES NOTERFLG # SHOULD DO INTERPRETIVELY TO SAVE A WORD
TCF P66
RESTART? CA FLAGWRD1 # HAS THERE BEEN A RESTART?
MASK RODFLBIT
EXTEND
BZF STRTP66A # Y
# N
TCF P66
## Page 799
# ****************************************************************************************************************
# INITIALIZATION FOR THIS PASS
# ****************************************************************************************************************
COUNT* $$/F2DPS
GUILDRET CAF ZERO
TS RODCOUNT
EXTEND
DCA TPIP
DXCH TPIPOLD
TC FASTCHNG
EXTEND
DCA PIPTIME1
DXCH TPIP
EXTEND
DCA TTF/8
DXCH TTF/8TMP
CCS FLPASS0
TCF TTFINCR
BRSPOT1 INDEX WCHPHASE
TCF NEWPHASE
# ****************************************************************************************************************
# ROUTINES TO START NEW PHASES
# ****************************************************************************************************************
STARTP64 TC NEWMODEX
DEC 64
CA DELTTFAP # AUGMENT TTF/8
ADS TTF/8TMP
INHINT
TC C13STALL
CA BIT12 # ENABLE RUPT10
EXTEND
WOR CHAN13
CAF P64DB
TS DB
TC DOWNFLAG # INITIALIZE REDESIGNATION FLAG
ADRES REDFLAG
CA LRWH1 # PUT P64 LR WEIGHTING FUNCTION INTO
TS LRWH # LRWH SO LR UPDATES ARE DONE PROPERLY
# (CONTINUE TO TTFINCR)
# ****************************************************************************************************************
# INCREMENT TTF/8, UPDATE LAND FOR LUNAR ROTATION, DO OTHER USEFUL THINGS
# ****************************************************************************************************************
## Page 800
#
# TTFINCR COMPUTATIONS ARE AS FOLLOWS:-
# TTF/8 UPDATED FOR TIME SINCE LAST PASS:
# TTF/8 = TTF/8 + (TPIP - TPIPOLD)/8
# LANDING SITE VECTOR UPDATED FOR LUNAR ROTATION:
# - - - -
# LAND = /LAND/ UNIT(LAND - LAND(TPIP - TPIPOLD) * WM)
# SLANT RANGE TO LANDING SITE, FOR DISPLAY:
# - -
# RANGEDSP = ABVAL(LAND - R)
TTFINCR TC INTPRET
DLOAD DSU
TPIP
TPIPOLD
SLR PUSH # SHIFT SCALES DELTA TIME TO 2(17) CSECS
11D
VXSC VXV
LAND
WM
BVSU RTB
LAND
NORMUNIT
VXSC VSL1
/LAND/
STODL LANDTEMP
EXIT
DXCH MPAC
DAS TTF/8TMP # NOW HAVE INCREMENTED TTF/8 IN TTF/8TMP
TC FASTCHNG
EXTEND
DCA TTF/8TMP
DXCH TTF/8
TC TDISPSET
CAF PRIO31 # TEMPORARILY OVER-PRIO CHARIN
TC PRIOCHNG
TC INTPRET
VLOAD VAD # ADD IN CORRECTION FROM NOUN 69
LANDTEMP
## Page 801
DLAND
STORE LAND
ABVAL # RECOMPUTE /LAND/
STORE /LAND/
EXIT
TC FASTCHNG # SINCE REDESIG MAY CHANGE LANDTEMP
CAF EBANK5
EBANK= DLAND
TS EBANK
CAF ZERO # ZERO N 69 REGISTERS
TS DLAND
TS DLAND +1
TS DLAND +2
TS DLAND +3
TS DLAND +4
TS DLAND +5
CAF EBANK7
EBANK= TREDES
TS EBANK
CAF PRIO20
TC PRIOCHNG
BRSPOT2 INDEX WCHPHASE
TCF PREGUIDE
# ****************************************************************************************************************
# LANDING SITE PERTURBATION EQUATIONS
# ****************************************************************************************************************
REDESIG CA FLAGWRD6 # IS REDFLAG SET?
MASK REDFLBIT
EXTEND
BZF RGVGCALC # NO: SKIP REDESIGNATION LOGIC
CA TREDES # YES: HAS TREDES REACHED ZERO?
EXTEND
BZF RGVGCALC # YES: SKIP REDESIGNATION LOGIC
INHINT
CA ELINCR1
TS ELINCR
CA AZINCR1
TS AZINCR
TC FASTCHNG
CA ZERO
TS ELINCR1
## Page 802
TS AZINCR1
TS ELINCR +1
TS AZINCR +1
CA FIXLOC # SET PD TO 0
TS PUSHLOC
TC INTPRET
VLOAD VSU
LAND
R # - -
RTB PUSH # PUSH DOWN UNIT (LAND - R)
NORMUNIT
VXV VSL1
YNBPIP # - - -
VXSC PDDL # PUSH DOWN - ELINCR(YNB * UNIT(LAND - R))
ELINCR
AZINCR
VXSC VSU
YNBPIP
VAD PUSH # RESULTING VECTOR IS 1/2 REAL SIZE
DLOAD DSU # MAKE SURE REDESIGNATION IS NOT
0 # TOO CLOSE TO THE HORIZON
DEPRCRIT
BMN DLOAD
REDES1
DEPRCRIT
STORE 0
REDES1 DLOAD DSU
LAND
R
DDV VXSC
0
VAD UNIT
R
VXSC VSL1
/LAND/
STORE LANDTEMP
EXIT # LOOKANGL WILL BE COMPUTED AT RGVGCALC
TC FASTCHNG
EXTEND
DCA LANDTEMP
DXCH LAND
EXTEND
DCA LANDTEMP +2
DXCH LAND +2
EXTEND
## Page 803
DCA LANDTEMP +4
DXCH LAND +4
TCF RGVGCALC
# ****************************************************************************************************************
# COMPUTE STATE IN GUIDANCE COORDINATES
# ****************************************************************************************************************
# RGVGCALC COMPUTATIONS ARE AS FOLLOWS:-
# VELOCITY RELATIVE TO THE SURFACE:
# - - - -
# ANGTERM = V + R * WM
# STATE IN GUIDANCE COORDINATES:
# - * - -
# RGU = CG (R - LAND)
# - * - - -
# VGU = CG (V - WM * R)
# DEPRESSION ANGLE FOR DISPLAY:
# - - -
# LOOKANGL = ARCSIN(UNIT(R - LAND).XMBPIP)
CALCRGVG TC INTPRET # IN IGNALG, COMPUTE V FROM INTEGRATION
VLOAD MXV # OUTPUT AND TRIM CORRECTION TERM
VATT1 # COMPUTED LAST PASS AND LEFT IN UNFC/2
REFSMMAT
VSR1 VAD
UNFC/2
STORE V
EXIT
RGVGCALC TC INTPRET # ENTER HERE TO RECOMPUTE RG AND VG
VLOAD VXV
R
WM
VAD VSR2 # RESCALE TO UNITS OF 2(9) M/CS
V
STORE ANGTERM
MXV
CG # NO SHIFT SINCE ANGTERM IS DOUBLE SIZED
STOVL VGU
R # - -
VSU PUSH # PUSH DOWN R - LAND
## Page 804
LAND
MXV VSL1
CG
STORE RGU
ABVAL
STOVL RANGEDSP # SM Z-AXIS RANGE FOR DISPLAY IN N68
RTB DOT # NOW IN MPAC IS SINE(LOOKANGL)/4
NORMUNIT
XNBPIP
EXIT
CA FIXLOC # RESET PUSH DOWN POINTER
TS PUSHLOC
CA MPAC # COMPUTE LOOKANGL ITSELF
DOUBLE
TC BANKCALL
CADR SPARCSIN -1
AD 1/2DEG
AD ELBIAS # BIAS LPD ANGLE FOR WINDOW BENDING
EXTEND
MP 180DEGS
TS LOOKANGL # LOOKANGL FOR DISPLAY DURING P64
BRSPOT3 INDEX WCHPHASE
TCF WHATGUID
# ****************************************************************************************************************
# TTF/8 COMPUTATION
# ****************************************************************************************************************
TTF/8CL TC INTPRETX
DLOAD*
JDG2TTF,1
STODL* TABLTTF +6 # A(3) = 8 JDG TO TABLTTF
ADG2TTF,1 # 2
STODL TABLTTF +4 # A(2) = 6 ADG TO TABLTTF
VGU +4 # 2
DMP DAD*
3/4DP
VDG2TTF,1
STODL* TABLTTF +2 # A(1) = (6 VGU + 18 VDG )/8 TO TABLTTF
RDG +4,1 # 2 2
DSU DMP
RGU +4
3/8DP
STORE TABLTTF # A(0) = -24 (RGU - RDG )/64 TO TABLTTF
EXIT # 2 2
## Page 805
CA BIT8
TS TABLTTF +10 # FRACTIONAL PRECISION FOR TTF TO TABLE
EXTEND
DCA TTF/8
DXCH MPAC # LOADS TTF/8 (INITIAL GUESS) INTO MPAC
CAF TWO # DEGREE - ONE
TS L
CAF TABLTTFL
TC ROOTPSRS # YIELDS TTF/8 IN MPAC
INDEX WCHPHASE
TCF WHATALM
EXTEND # GOOD RETURN
DCA MPAC # FETCH TTF/8 KEEPING IT IN MPAC
DXCH TTF/8 # CORRECTED TTF/8
TC TDISPSET
# (CONTINUE TO QUADGUID)
# ****************************************************************************************************************
# MAIN GUIDANCE EQUATION
# ****************************************************************************************************************
# AS PUBLISHED:-
# - - - -
# - - 6(VDG + VG) 12(RDG - RG)
# ACG = ADG + ----------- + ------------
# TTF (TTF)(TTF)
# AS HERE PROGRAMMED:-
# - -
# 3 (1/4(RDG - RG) - - )
# - (------------- + VDG + VG)
# - 4 ( TTF/8 ) -
# ACG = ---------------------------- + ADG
# TTF/8
QUADGUID CS TTF/8
AD LEADTIME # LEADTIME IS A NEGATIVE NUMBER
AD POSMAX # SAFEGUARD THE COMPUTATIONS THAT FOLLOW
TS L # BY FORCING -TTF+LEADTIME > OR = ZERO
CS L
AD L
ZL
EXTEND
## Page 806
DV TTF/8
TS BUF # - RATIO OF LAG-DIMINISHED TTF TO TTF
EXTEND
SQUARE
TS BUF +1
AD BUF
XCH BUF +1 # RATIO SQUARED - RATIO
AD BUF +1
TS MPAC # COEFFICIENT FOR VGU TERM
AD BUF +1
INDEX FIXLOC
TS 26D # COEFFICIENT FOR RDG-RGU TERM
AD BUF +1
INDEX FIXLOC
TS 28D # COEFFICIENT FOR VDG TERM
AD BUF
AD POSMAX
AD BUF +1
AD BUF +1
INDEX FIXLOC
TS 30D # COEFFICIENT FOR ADG TERM
CAF ZERO
TS MODE
TC INTPRETX
VXSC PDDL
VGU
28D
VXSC* RTB
VDG,1
ZEROMID
PDVL* RTB
RDG,1
ZEROMID
VSU V/SC
RGU
TTF/8
VSR2 VXSC
26D
VAD VAD
V/SC VXSC
TTF/8
3/4DP
PDDL VXSC*
30D
ADG,1
RTB VAD
ZEROMID
## Page 807
AFCCALC1 VXM VSL1 # VERTGUID COMES HERE
CG
PDVL V/SC
GDT/2
GSCALE
BVSU STADR
STORE UNFC/2 # UNFC/2 NEED NOT BE UNITIZED
ABVAL
AFCCALC2 STODL /AFC/ # MAGNITUDE OF AFC FOR THROTTLE
UNFC/2 # VERTICAL COMPONENT
DSQ PDDL
UNFC/2 +2 # OUT-OF-PLANE
DSQ PDDL
HIGHESTF
DDV DSQ
MASS # 2 2 2
DSU DSU # AMAXHORIZ = SQRT(ATOTAL - A - A )
BPL DLOAD # 1 0
AFCCALC3
ZEROVECS
AFCCALC3 SQRT DAD
UNFC/2 +4
BPL BDSU
AFCCLEND
UNFC/2 +4
STORE UNFC/2 +4
AFCCLEND EXIT
TC FASTCHNG
CA WCHPHASE # PREPARE FOR PHASE SWITCHING LOGIC
TS WCHPHOLD
INCR FLPASS0 # INCREMENT PASS COUNTER
BRSPOT4 INDEX WCHPHASE
TCF AFTRGUID
# ****************************************************************************************************************
# NEW PHASE NOW?
# ****************************************************************************************************************
EXTLOGIC INDEX WCHPHASE # IS TTF NEARER ZERO THAN CRITERION?
CA TENDBRAK
AD TTF/8
EXTEND
BZMF CGCALC # NO
TC FASTCHNG # YES: INCREMENT WCHPHASE, ZERO FLPASS0
CA WCHPHOLD
AD ONE
## Page 808
TS WCHPHASE
CAF ZERO
TS FLPASS0
# (CONTINUE TO CGCALC)
# ***************************************************************************************************************
# ERECT GUIDANCE-STABLE MEMBER TRANSFORMATION MATRIX
# ***************************************************************************************************************
CGCALC CAF EBANK5
TS EBANK
EBANK= TCGIBRAK
EXTEND
INDEX WCHPHASE
INDEX TARGTDEX
DCA TCGFBRAK
INCR BBANK
INCR BBANK
EBANK= TTF/8
AD TTF/8
XCH L
AD TTF/8
CCS A
CCS L
TCF EXITSPOT
TCF EXITSPOT
NOOP
TC INTPRETX
VLOAD UNIT
LAND
STODL CG
TTF/8
DMP* VXSC
GAINBRAK,1 # NUMERO MYSTERIOSO
ANGTERM
VAD
LAND
VSU RTB
R
NORMUNIT
VXV RTB
LAND
NORMUNIT
STOVL CG +6 # SECOND ROW
CG
VXV VSL1
CG +6
STORE CG +14
EXIT
EXITSPOT INDEX WCHPHOLD
TCF WHATEXIT
# ****************************************************************************************************************
## Page 809
# ROUTINES FOR EXITING FROM LANDING GUIDANCE
# ****************************************************************************************************************
# 1. EXGSUB IS THE RETURN WHEN GUIDSUB IS CALLED BY THE IGNITION ALGORITHM.
# 2. EXBRAK IN THE EXIT USED DURING THE BRAKING PHASE. IN THIS CASE UNIT(R) IS THE WINDOW POINTING VECTOR.
# 3. EXNORM IS THE EXIT USED AT OTHER TIMES DURING THE BURN.
# (EXOVFLOW IS A SUBROUTINE OF EXBRAK AND EXNORM CALLED WHEN OVERFLOW OCCURRED ANYWHERE IN GUIDANCE.)
EXGSUB TC INTPRET # COMPUTE TRIM VELOCITY CORRECTION TERM
VLOAD RTB
UNFC/2
NORMUNIT
VXSC VXSC
ZOOMTIME
TRIMACCL
STORE UNFC/2
EXIT
CCS NGUIDSUB
TCF GUIDSUB
CCS NIGNLOOP
TCF +3
TC ALARM
OCT 01412
+3 TC POSTJUMP
CADR DDUMCALC
EXBRAK TC INTPRET
VLOAD
UNIT/R/
STORE UNWC/2
EXIT
TCF STEER?
EXNORM TC INTPRET
VLOAD VSU
LAND
R
RTB
NORMUNIT
STORE UNWC/2 # UNIT(LAND - R) IS TENTATIVE CHOICE
VXV DOT
XNBPIP
CG +6
EXIT # WITH PROJ IN MPAC 1/8 REAL SIZE
## Page 810
CS MPAC # GET COEFFICIENT FOR CG +14
AD PROJMAX
AD POSMAX
TS BUF
CS BUF
ADS BUF # RESULT IS 0 IF PROJMAX - PROJ NEGATIVE
CS PROJMIN # GET COEFFICIENT FOR UNIT(LAND - R)
AD MPAC
AD POSMAX
TS BUF +1
CS BUF +1
ADS BUF +1 # RESULT IS 0 IF PROJ - PROJMIN NEGATIVE
CAF FOUR
UNWCLOOP MASK SIX
TS Q
CA EBANK5
TS EBANK
EBANK= CG
CA BUF
EXTEND
INDEX Q
MP CG +14
INCR BBANK
EBANK= UNWC/2
INDEX Q
DXCH UNWC/2
EXTEND
MP BUF +1
INDEX Q
DAS UNWC/2
CCS Q
TCF UNWCLOOP
CA AZBIAS # SET OUTER GIMBAL
TS OGABIAS # ANGLE BIAS FOR WINDOW BENDING
INCR BBANK
EBANK= PIF
STEER? CA OVFIND # OVERFLOW?
EXTEND
BZF STEERSW? # N: CHECK STEERSW
TC OVFDESC # Y: REMEDIAL ACTION AND
TCF DISPEXIT # SKIP ISSUANCE OF CMDS. NO STEERSW CHK
STEERSW? CS FLAGWRD2 # IS STEERSW UP?
MASK STEERBIT
## Page 811
EXTEND
BZF THRTCALL # Y: ISSUE GUIDANCE CMDS
RATESTOP INHINT # N: REMEDIAL ACTION
TC IBNKCALL # AND
FCADR STOPRATE # SKIP ISSUANCE OF CMDS
RELINT
TCF DISPEXIT
GDUMP1 = THRTCALL
THRTCALL TC THROTTLE
TC FASTCHNG
TC INTPRET
CALL
FINDCDUW -2
EXIT
# (CONTINUE TO DISPEXIT)
# ****************************************************************************************************************
# GUIDANCE LOOP DISPLAYS
# ****************************************************************************************************************
DISPEXIT EXTEND # KILL GROUP 3: DISPLAYS WILL BE
DCA NEG0 # RESTORED BY NEXT GUIDANCE CYCLE
DXCH -PHASE3
ENDLLJOB = DISPEXIT +3
DISPEX66 = DISPEXIT +3
+3 CS FLAGWRD8 # IF FLUNDISP IS SET, NO DISPLAY THIS PASS
MASK FLUNDBIT
EXTEND
BZF ENDOFJOB
INDEX WCHPHOLD
TCF WHATDISP
P63DISPS TC VACRLEAS
CAF V06N63
DISPCOMN TC BANKCALL
CADR REGODSP
P64DISPS CA TREDES # HAS TREDES REACHED ZERO?
EXTEND
BZF RED-OVER # YES: CLEAR REDESIGNATION FLAG
CS FLAGWRD6 # NO: IS REDFLAG SET?
MASK REDFLBIT
EXTEND
BZF REDES-OK # YES: DO STATIC DISPLAY
TC VACRLEAS
CAF V06N64 # OTHERWISE USE FLASHING DISPLAY
TC BANKCALL
CADR REFLASH
TCF GOTOPOOH # TERMINATE
TCF P64CEED # PROCEED PERMIT REDESIGNATIONS
TCF P64DISPS # RECYCLE
P64CEED CAF ZERO
TS ELINCR1
TS AZINCR1
TC UPFLAG # ENABLE REDESIGNATION LOGIC
ADRES REDFLAG
TCF ENDOFJOB
RED-OVER TC DOWNFLAG
ADRES REDFLAG
REDES-OK TC VACRLEAS
CAF V06N64
TCF DISPCOMN
VERTDISP TC VACRLEAS
CAF V06N60
TC BANKCALL
CADR REFLASH
## Page 813
TCF GOTOPOOH # TERMINATE
TCF STOPFIRE # PROCEED
TCF STOPFIRE # V32E
STOPFIRE TC DOWNFLAG
ADRES P66PROFL # FLAG TO STOP P66 HORIZONTAL
TCF ENDOFJOB
THROT66 TC THROTTLE +3
INCR CNTTHROT # COUNT ONE THROTTLE COMPLETION
TCF DISPEX66
## Page 814
# ****************************************************************************************************************
# GUIDANCE FOR P66
# ****************************************************************************************************************
# THE P66 HORIZONTAL (HZ) EQUATION IS:
# UNFC/2X = GHZ
# UNFC/2Y = (LIMIT AHZLIM)(-QHZ UNFC/2Y -(VY-VHZCY)/TAUHZ)
# I-1
# UNFC/2Z = (LIMIT AHZLIM)(-QHZ UNFC/2Z -(VZ-VHZCZ)/TAUHZ)
# I-1
# WHERE GHZ IS LUNAR GRAVITY
# QHZ AND 1/TAUHZ ARE GAIN CONSTANTS
# VHZCY AND VHZCZ ARE THE Y AND Z COMPONENTS OF COMMANDED
# VELOCITY, PLATFORM COORDINATES. THESE ARE INITIALIZED
# TO MOONRATE
# (LIMIT AHZLIM) INDICATES THE CONTENT OF THE SUBSEQUENT
# PARENTHESES IS MAGNITUDE LIMITED TO AHZLIM
P66 TC PHASCHNG # TERMINATE GROUP 3
OCT 00003
TC INTPRET
RTB DSU # IS THERE TIME FOR P66?
LOADTIME
PIPTIME
BDSU BPL
2LATE466
P66HZ # Y: DOIT
CLEAR EXIT # N: OMIT
RODFLAG
CS TOOFEW # INITIALIZE CNTTHROT TO TOOFEW AND LOAD
XCH CNTTHROT # ACCUMULATOR WITH ITS PREVIOUS CONTENTS
EXTEND # TOO FEW THROTTLINGS SINCE LAST OMISSION?
BZMF OMITWALM
TCF DISPEX66 # N: PERMIT OMISSION SANS ALARM
OMITWALM INHINT
TC BANKCALL
CADR STOPRATE
TC ALARM # Y: PERMIT OMISSION WITH ALARM
OCT 01466
TCF DISPEX66
## Page 815
# ****************************************************************************************************************
# GUIDANCE FOR P66
# ****************************************************************************************************************
SETLOC P66LOC
BANK
COUNT* $$/F2DPS
P66HZ VLOAD VXSC
UNFC/2 # P63, P64, & P66 UNITS 2(-4)M/CS/CS
QHZ
PDVL VSU
VHZC # IN 2(7)M/CS
V # IN 2(7)M/CS
V/SC VSU # YIELDS UNLIM HZ ACCEL CMD, 2(-4)M/CS/CS
TAUHZ # IN 2(1))CS
EXIT
CA PRIO21 # ASSURE THIS SERVICER JOB ENDS
TC PRIOCHNG # BEFORE NEXT SERVICER JOB BEGINS
CA GHZ
TS MPAC # X COMPONENT = G
CA EBANK5
TS EBANK
EBANK= END-E5
LXCH MPAC +3
CA AHZLIM
TC BANKCALL
FCADR LIMITSUB
TS MPAC +3 # Y COMPONENT LIMITED TO AHZLIM
LXCH MPAC +5
CA AHZLIM
TC BANKCALL
FCADR LIMITSUB
TS MPAC +5 # Z COMPONENT LIMITED TO AHZLIM
CA EBANK7
TS EBANK
EBANK= END-E7
CA OVFIND # OVERFLOW?
EXTEND
BZF ENGARM? # N: KEEP CHECKING
TC BANKCALL # Y: TAKE REMEDIAL ACTION
FCADR OVFDESC # AND
TCF P66VERT # SKIP ISSUANCE OF HZ CMDS
## Page 816
ENGARM? CA BIT3 # IS ENGINE ARM SWITCH STILL ON?
EXTEND
RAND CHAN30
EXTEND
BZF CDUWHZ # Y: ISSUE HZ CMDS
CA FLAGWRD0 # N: HAVE WE PROCEEDED AFTER TOUCHDOWN?
MASK P66PROBT
EXTEND
BZF ASTROPRO # Y: PREVENT RCS FIRINGS
CDUWHZ TC INTPRET # N: ISSUE HZ CMDS
STORE UNFC/2 # MUST STORE FOR SUCCEEDING PASS
CALL
FINDCDUW
EXIT
TCF P66VERT
ASTROPRO CA IDLADR # Y: PREVENT RCS JET FIRINGS
TS T5ADR # AND
TCF P66VERT # SKIP HZ CMDS, BUT CONTINUE DISPLAYS
# ***************************************************************************************************************
# P66 VERTICAL CHANNEL
# ***************************************************************************************************************
RODTASK CA PRIO22 # BUMPS ALL OF SERVICER JOB EXCEPT RODCOMP
TC FINDVAC
EBANK= DVCNTR
2CADR RODCOMP
TCF TASKOVER
P66VERT CA 1SEC
TC TWIDDLE
ADRES RODTASK
RODCOMP CA PRIO23 # LET ONLY ONE JOB THRU RODCOMP AT A TIME
TC PRIOCHNG
INHINT
CAF ZERO
XCH RODCOUNT
EXTEND
MP RODSCAL1
DAS VDGVERT # UPDATE DESTRED ALTITUDE RATE.
CAF BIT5 # ARE WE IN AUTO THROTTLE?
EXTEND
RAND CHAN30
EXTEND
BZF RODCOMPA # Y: CONTINUE ROD
EXTEND # N: RESET VDGVERT TO CURRENT HDOT
DCA HDOTDISP
DXCH VDGVERT
# READ THE PIPAS FOR P66
RODCOMPA EXTEND
DCA PIPAX
DXCH OLDPIPAX # CURRENT PIPA READINGS INTO OLDPIPAX,Y,Z
DXCH RUPTREG1 # SAVE PRIOR READINGS IN RUPTREG1,2,3
CA PIPAZ
XCH OLDPIPAZ
XCH RUPTREG3
EXTEND # SNAPSHOT TIME OF PIPA READING.
DCA TIME2
DXCH THISTPIP
TC DEIMUBOB # REFER CURRENT PIPAX READING TO THE CM
# COMPUTE DELV SINCE PIPTIME. RETURN FROM DEIMUBOB WITH CORRECTED OLDPIPAX IN A
# CURRENT P66 PIPA
AD PIPATMPX # + PIPA BY PIPASR IF B4 COPYCYCL, 0 AFTER
TS MPAC # = DELV SINCE VALIDITY OF V, 2(14)CM/SEC
CA OLDPIPAY
AD PIPATMPY
TS MPAC +3
CA OLDPIPAZ
AD PIPATMPZ
TS MPAC +5
# COMPUTE DELV SINCE THE LAST P66 PASS
CS OLDPIPAX # - CURRENT P66 PIPA
AD TEMX # - PIPA BY PIPASR IF INTERVENING, ELSE 0
AD RUPTREG1 # + PIPA BY P66 ON THE LAST P66 PASS
TS DELVROD # = -DELV SINCE LAST P66 PASS, 2(14)CM/SEC
CS OLDPIPAY
AD TEMY
AD RUPTREG2
## Page 818
TS DELVROD +2
CS OLDPIPAZ
AD TEMZ
AD RUPTREG3
TS DELVROD +4
CAF ZERO
TS MPAC +1 # ZERO LO-ORDER MPAC COMPONENTS
TS MPAC +4
TS MPAC +6
TS TEMX # ZERO TEMX, TEMY, AND TEMZ SO WE WILL
TS TEMY # KNOW WHEN READACCS CHANGES THEM.
TS TEMZ
CS ONE
TS MODE
TC INTPRET
ITRPNT1 VXSC PDDL # SCALE MPAC TO M/CS *2(-7) AND PUSH (6)
KPIP1
THISTPIP
DSU
PIPTIME
STORE 30D # 30-31D CONTAINS TIME IN CS SINCE PIPTIME
DDV PDVL # (8)
4SEC(28)
GDT/2
VSU VXSC # (6)
VBIAS
VSL2 VAD
V
VAD STADR # (0)
STOVL 24D # STORE UPDATED VELOCITY IN 24-29D
R
UNIT
STORE 14D
DOT SL1
24D
STODL HDOTDISP # UPDATE ALTITUDE RATE FOR NOUN 60
30D
SL DMP
11D
HDOTDISP
DAD DSU
36D
/LAND/
STODL HCALC1 # UPDATE ALTITUDE FOR NOUN 60
## Page 819
HDOTDISP
BDSU DDV
VDGVERT
TAUROD
PDVL ABVAL # (2)
GDT/2
DDV SR2
GSCALE
STORE 20D
RTB DAD # (0)
QTPROLOG # QUICTRIG PRESERVES MPAC
PDVL CALL # (2)
UNITX # X AXIS IN NB COORDS
*NBSM* # TRANSFORMS TO SM COORDS
DOT
14D
STORE 22D
BDDV STADR # (0)
STOVL /AFC/
DELVROD
VXSC VAD
KPIP1
VBIAS
ABVAL PDDL # (2)
THISTPIP
DSU PDDL # (4)
LASTTPIP
THISTPIP
STODL LASTTPIP # (2)
DDV BDDV # (0)
SHFTFACT
PDDL DMP # (2)
FWEIGHT
BIT1H
DDV DDV
MASS
SCALEFAC
DAD PDDL # (4)
0D
20D
DDV DSU # (2)
22D
## Page 820
DMP DAD
LAG/TAU
/AFC/
PDDL DDV # (4)
MAXFORCE
MASS
PDDL DDV # (6)
MINFORCE
MASS
PUSH BDSU # (8)
2D
BMN DLOAD # (6)
AFCSPOT
DLOAD PUSH # (6)
BDSU BPL
2D
AFCSPOT
DLOAD # (4)
AFCSPOT DLOAD # (2),(4),OR (6)
SETPD # (2)
2D
STODL /AFC/ # (0)
ITRPNT2 EXIT
DXCH MPAC # MPAC = MEASURED ACCELERATION.
TC POSTJUMP
FCADR THROT66
# THE FOLLOWING SUBROUTINE REFERS THE X PIPA READING TO THE CENTER OF MASS
# BY SUBTRACTING THOSE PIPA COUNTS PRODUCED BY VERTICAL IMU MOTION
# RELATIVE TO THE CENTER OF MASS. THE SPACECRAFT X AXIS IS ASSUMED
# APPROXIMATELY VERTICAL. THE EQUATION IS:
# OLDPIPAX = OLDPIPAX - OMEGAQ RIMUZ
# WHERE OLDPIPAX IS THE CURRENT P66 PIPA READING, OMEGAQ IS THE ATTITUDE
# RATE ABOUT THE Q (Y) AXIS, AND RIMUZ IS THE Z COORDINATE OF THE IMU.
DEIMUBOB CA EBANK6
TS EBANK
EBANK= END-E6
CS OMEGAQ # PITCH RATE IN UNITS 45 DEG/SEC
INCR BBANK
EBANK= END-E7
EXTEND
MP RIMUZ # IMU Z IN UNITS (180/PI 45) 2(14) CM
ADS OLDPIPAX # CURRENT P66 PIPA X IN UNITS 2(14) CM/SEC
TC Q
## Page 821
# CONSTANTS FOR P66
IDLADR GENADR DAPIDLER
GHZ DEC 1.62292 E-4 B+4 # GRAVITY IN 2(-4)M/CS/CS
BIT1H OCT 00001 # MUST PRECEDE A ZERO
SHFTFACT 2DEC 1 B-17 # SCALES P66 PERIOD TO 2(1))CS
BIASFACT 2DEC 655.36 B-26
RIMUZ DEC 99.486 B-14 # 1.2667 M IN UNITS (180/PI 45) 2(14) CM
## Page 822
# ****************************************************************************************************************
# REDESIGNATOR TRAP
# ****************************************************************************************************************
# END INSERT
BANK 11
SETLOC F2DPS*11
BANK
COUNT* $$/F2DPS
PITFALL XCH BANKRUPT
EXTEND
QXCH QRUPT
TC CHECKMM # IF NOT IN P64, NO REASON TO CONTINUE
DEC 64
TCF RESUME
EXTEND
READ CHAN31
COM
MASK ALL4BITS
TS ELVIRA
CAF TWO
TS ZERLINA
CAF FIVE
TC TWIDDLE
ADRES REDESMON
TCF RESUME
# REDESIGNATION MONITOR (INITIATED BY PITFALL)
PREMON1 TS ZERLINA
PREMON2 CAF SEVEN
TC VARDELAY
REDESMON EXTEND
READ 31
COM
MASK ALL4BITS
XCH ELVIRA
TS L
CCS ELVIRA # DO ANY BITS APPEAR THIS PASS?
TCF PREMON2 # Y: CONTINUE MONITOR
CCS L # N: ANY LAST PASS?
TCF COUNT'EM # Y: COUNT 'EM, RESET RUPT, TERMINATE
CCS ZERLINA # N: HAS ZERLINA REACHED ZERO YET?
## Page 823
TCF PREMON1 # N: DIMINISH ZERLINA, CONTINUE
RESETRPT TC C13STALL # Y: RESET RUPT, TERMINATE
CAF BIT12
EXTEND
WOR CHAN13
TCF TASKOVER
COUNT'EM CAF BIT13 # ARE WE IN ATTITUDE-HOLD?
EXTEND
RAND CHAN31
EXTEND
BZF RESETRPT # YES: SKIP REDESIGNATION LOGIC.
CA L # NO
MASK -AZBIT
CCS A
-AZ CS AZEACH
ADS AZINCR1
CA L
MASK +AZBIT
CCS A
+AZ CA AZEACH
ADS AZINCR1
CA L
MASK -ELBIT
CCS A
-EL CS ELEACH
ADS ELINCR1
CA L
MASK +ELBIT
CCS A
+EL CA ELEACH
ADS ELINCR1
TCF RESETRPT
# THESE EQUIVALENCIES ARE BASED ON GSOP CHAPTER 4, REVISION 16 OF P64LM
+ELBIT = BIT2 # -PITCH
-ELBIT = BIT1 # +PITCH
+AZBIT = BIT5
-AZBIT = BIT6
## Page 824
ALL4BITS OCT 00063
AZEACH DEC .03491 # 2 DEGREES
ELEACH DEC .00873 # 1/2 DEGREE
# ****************************************************************************************************************
# R.O.D. TRAP
# ************************************************************************
SETLOC RODTRAP
BANK
COUNT* $$/F2DPS # ****************************************
DESCBITS MASK BIT7 # COME HERE FROM MARKRUPT CODING WITH BIT
CCS A # 7 OR 6 OF CHANNEL 16 IN A: BIT 7 MEANS
CS TWO # - RATE INCREMENT, BIT 6 + INCREMENT
AD ONE
ADS RODCOUNT
TCF RESUME # TRAP IS RESET WHEN SWITCH IS RELEASED
BANK 31
SETLOC F2DPS*31
BANK
COUNT* $$/F2DPS
# ****************************************************************************************************************
# DOUBLE PRECISION ROOT FINDER SUBROUTINE (BY ALLAN KLUMPP)
# ****************************************************************************************************************
# N N-1
# ROOTPSRS FINDS ONE ROOT OF THE POWER SERIES A X + A X + ... + A X + A
# N N-1 1 0
# USING NEWTON'S METHOD STARTING WITH AN INITIAL GUESS FOR THE ROOT. THE ENTERING DATA MUST BE AS FOLLOWS:
# A SP LOC-3 ADRES FOR REFERENCING PWR COF TABL
# L SP N-1 N IS THE DEGREE OF THE POWER SERIES
# MPAC DP X INITIAL GUESS FOR ROOT
# LOC-2N DP A(0)
# ...
# LOC DP A(N)
# LOC+2 SP PRECROOT PREC RQD OF ROOT (AS FRACT OF 1ST GUESS)
# THE DP RESULT IS LEFT IN MPAC UPON EXIT, AND A SP COUNT OF THE ITERATIONS TO CONVERGENCE IS LEFT IN MPAC+2.
# RETURN IS NORMALLY TO LOC(TC ROOTPSRS)+3. IF ROOTPSRS FAILS TO CONVERGE IN 8 PASSES, RETURN IS TO LOC+1 AND
# OUTPUTS ARE NOT TO BE TRUSTED.
# PRECAUTION: ROOTPSRS MAKES NO CHECKS FOR OVERFLOW OR FOR IMPROPER USAGE. IMPROPER USAGE COULD
# PRECLUDE CONVERGENCE OR REQUIRE EXCESSIVE ITERATIONS. AS A SPECIFIC EXAMPLE, ROOTPSRS FORMS A DERIVATIVE
# COEFFICIENT TABLE BY MULTIPLYING EACH A(I) BY I, WHERE I RANGES FROM 1 TO N. IF AN ELEMENT OF THE DERIVATIVE
# COEFFICIENT TABLE = 1 OR > 1 IN MAGNITUDE, ONLY THE EXCESS IS RETAINED. ROOTPSRS MAY CONVERGE ON THE CORRECT
# ROOT NONETHELESS, BUT IT MAY TAKE AN EXCESSIVE NUMBER OF ITERATIONS. THEREFORE THE USER SHOULD RECOGNIZE:
# 1. USER'S RESPONSIBILITY TO ASSURE THAT I X A(I) < 1 IN MAGNITUDE FOR ALL I.
# 2. USER'S RESPONSIBILITY TO ASSURE OVERFLOW WILL NOT OCCUR IN EVALUATING EITHER THE RESIDUAL OR THE DERIVATIVE
# POWER SERIES. THIS OVERFLOW WOULD BE PRODUCED BY SUBROUTINE POWRSERS, CALLED BY ROOTPSRS, AND MIGHT NOT
# PRECLUDE EVENTUAL CONVERGENCE.
## Page 825
# 3. AT PRESENT, ERASABLE LOCATIONS ARE RESERVED ONLY FOR N UP TO 5. AN N IN EXCESS OF 5 WILL PRODUCE CHAOS.
# ALL ERASABLES USED BY ROOTPSRS ARE UNSWITCHED LOCATED IN THE REGION FROM MPAC-33 OCT TO MPAC+7.
# 4. THE ITERATION COUNT RETURNED IN MPAC+2 MAY BE USED TO DETECT ABNORMAL PERFORMANCE.
# STORE ENTERING DATA, INITLIZE ERASABLES
ROOTPSRS EXTEND
QXCH RETROOT # RETURN ADRES
TS PWRPTR # PWR TABL POINTER
DXCH MPAC +3 # PWR TABL ADRES, N-1
CA DERTABLL
TS DERPTR # DER TABL POINTER
TS MPAC +5 # DER TABL ADRES
CCS MPAC +4 # NO POWER SERIES OF DEGREE 1 OR LESS
TS MPAC +6 # N-2
CA ZERO # MODE USED AS ITERATION COUNTER. MODE
TS MODE # MUST BE POS SO ABS WON'T COMP MPAC+3 ETC
# COMPUTE CRITERION TO STOP ITERATING
EXTEND
DCA MPAC # FETCH ROOT GUESS, KEEPING IT IN MPAC
DXCH ROOTPS # AND IN ROOTPS
INDEX MPAC +3 # PWR TABL ADRES
CA 5 # PRECROOT TO A
TC SHORTMP # YIELDS DP PRODUCT IN MPAC
TC USPRCADR
CADR ABS # YIELDS ABVAL OF CRITERION ON DX IN MPAC
DXCH MPAC
DXCH DXCRIT # CRITERION
# SET UP DER COF TABL
EXTEND
INDEX PWRPTR
DCA 3
DXCH MPAC # A(N) TO MPAC
CA MPAC +4 # N-1 TO A
DERCLOOP TS PWRCNT # LOOP COUNTER
AD ONE
TC DMPNSUB # YIELDS DERCOF = I X A(I) IN MPAC
EXTEND
INDEX PWRPTR
DCA 1
DXCH MPAC # A(I-1) TO MPAC, FETCHING DERCOF
INDEX DERPTR
DXCH 3 # DERCOF TO DER TABL
## Page 826
CS TWO
ADS PWRPTR # DECREMENT PWR POINTER
CS TWO
ADS DERPTR # DECREMENT DER POINTER
CCS PWRCNT
TCF DERCLOOP
# CONVERGE ON ROOT
ROOTLOOP EXTEND
DCA ROOTPS # FETCH CURRENT ROOT
DXCH MPAC # LEAVE IN MPAC
EXTEND
DCA MPAC +5 # LOAD A, L WITH DER TABL ADRES, N-2
TC POWRSERS # YIELDS DERIVATIVE IN MPAC
EXTEND
DCA ROOTPS
DXCH MPAC # CURRENT ROOT TO MPAC, FETCHING DERIVTIVE
DXCH BUF # LEAVE DERIVATIVE IN BUF AS DIVISOR
EXTEND
DCA MPAC +3 # LOAD A, L WITH PWR TABL ADRES, N-1
TC POWRSERS # YIELDS RESIDUAL IN MPAC
TC USPRCADR
CADR DDV/BDDV # YIELDS -DX IN MPAC
EXTEND
DCS MPAC # FETCH DX, LEAVING -DX IN MPAC
DAS ROOTPS # CORRECTED ROOT NOW IN ROOTPS
TC USPRCADR
CADR ABS # YIELDS ABS(DX) IN MPAC
EXTEND
DCS DXCRIT
DAS MPAC # ABS(DX)-ABS(DXCRIT) IN MPAC
CA MODE
MASK BIT4 # KLUMPP SAYS GIVE UP AFTER EIGHT PASSES
CCS A
BADROOT TC RETROOT
INCR MODE # INCREMENT ITERATION COUNTER
CCS MPAC # TEST HI ORDER DX
TCF ROOTLOOP
TCF TESTLODX
TCF ROOTSTOR
TESTLODX CCS MPAC +1 # TEST LO ORDER DX
TCF ROOTLOOP
TCF ROOTSTOR
## Page 827
TCF ROOTSTOR
ROOTSTOR DXCH ROOTPS
DXCH MPAC
CA MODE
TS MPAC +2 # STORE SP ITERATION COUNT IN MPAC+2
INDEX RETROOT
TCF 2
DERTABLL ADRES DERCOFN -3
# ****************************************************************************************************************
# TRASHY LITTLE SUBROUTINES
# ****************************************************************************************************************
ZEROMID CAF ZERO # ROUTINE TO ZERO THE MIDDLE COMPONENT
TS MPAC +3 # OF A VECTOR IN MPAC. "TCF DANZIG"
TS MPAC +4 # COULD BE A "TC Q" AT THE EXPENSE OF
TCF DANZIG # A TINY AMOUNT OF TIME.
INTPRETX INDEX WCHPHASE # SET X1 ON THE WAY TO THE INTERPRETER
CS TARGTDEX
INDEX FIXLOC
TS X1
TCF INTPRET
TDISPSET CA TTF/8
EXTEND
MP TSCALINV
DXCH TTFDISP
CA EBANK5 # TREDES BECOMES ZERO TWO PASSES
TS EBANK # BEFORE TCGFAPPR IS REACHED
EBANK= TCGFAPPR
CA TCGFAPPR
INCR BBANK
INCR BBANK
EBANK= TTF/8
AD TTF/8
EXTEND
MP TREDESCL
AD -DEC103
AD NEGMAX
TS L
CS L
AD L
AD +DEC99
AD POSMAX
## Page 828
TS TREDES
CS TREDES
ADS TREDES
TC Q
1406POO TC POODOO
OCT 21406
1406ALM TC ALARM
OCT 01406
TCF RATESTOP
# DESCENT OVERFLOW SUBROUTINE
OVFDESC EXTEND
QXCH OVFRET
TC ALARM
OCT 01410
INHINT # MUST USE INHINT, IBNKCALL, RELINT
TC IBNKCALL # BECAUSE DAP COULD INTERRUPT STOPRATE AND
FCADR STOPRATE # BECAUSE WE COME FROM P66HZ VIA BANKCALL
RELINT
CA ZERO
TS OVFIND
TC OVFRET
## Page 829
# ****************************************************************************************************************
# SPECIALIZED "PHASCHNG" SUBROUTINE
# ****************************************************************************************************************
EBANK= PHSNAME2
FASTCHNG CA EBANK3 # SPECIALIZED 'PHASCHNG' ROUTINE
XCH EBANK
DXCH L
TS PHSNAME3
LXCH EBANK
EBANK= E2DPS
TC A
# ****************************************************************************************************************
# PARAMETER TABLE INDIRECT ADDRESSES
# ****************************************************************************************************************
RDG = RBRFGX
VDG = VBRFGX
ADG = ABRFGX
VDG2TTF = VBRFG*
ADG2TTF = ABRFG*
JDG2TTF = JBRFG*
# ****************************************************************************************************************
# LUNAR LANDING CONSTANTS
# ***************************************************************************************************************
TABLTTFL ADRES TABLTTF +3 # ADDRESS FOR REFERENCING TTF TABLE
TTFSCALE = BIT12
TSCALINV = BIT4
-DEC103 DEC -103
P64DB OCT 00155 # 0.3 DEGREES SCALED AT CDU SCALING
+DEC99 DEC +99
TREDESCL DEC -.08
## Page 830
180DEGS DEC +180
1/2DEG DEC +.00278
PROJMAX DEC .42262 B-3 # SIN(25')/8 TO COMPARE WITH PROJ
PROJMIN DEC .25882 B-3 # SIN(15')/8 TO COMPARE WITH PROJ
V06N63 VN 0663 # P63
V06N64 VN 0664 # P64
V06N60 VN 0660 # P65, P66, P67
BANK 22
SETLOC LANDCNST
BANK
COUNT* $$/F2DPS
HIGHESTF 2DEC 4.34546769 B-12
GSCALE 2DEC 100 B-11
3/8DP 2DEC .375
3/4DP 2DEC .750
DEPRCRIT 2DEC -.02 B-1
# ****************************************************************************************************************
# ****************************************************************************************************************
Computing file changes ...
