Initial commit of source code.
This commit is contained in:
chrislgarry
parent
a6f6fe22e1
commit
491ec007d6
302
CM_BODY_ATTITUDE.s
Normal file
302
CM_BODY_ATTITUDE.s
Normal file
@ -0,0 +1,302 @@
|
|||||||
|
# Copyright: Public domain.
|
||||||
|
# Filename: CM_BODY_ATTITUDE.s
|
||||||
|
# Purpose: Part of the source code for Comanche, build 055. It
|
||||||
|
# is part of the source code for the Command Module's
|
||||||
|
# (CM) Apollo Guidance Computer (AGC), Apollo 11.
|
||||||
|
# Assembler: yaYUL
|
||||||
|
# Reference: pp. 883-889
|
||||||
|
# Contact: Ron Burkey <info@sandroid.org>
|
||||||
|
# Website: http://www.ibiblio.org/apollo.
|
||||||
|
# Mod history: 2009-05-12 RSB Adapted from Colossus249 file of the same
|
||||||
|
# name and Comanche 055 page images.
|
||||||
|
#
|
||||||
|
# The contents of the "Comanche055" files, in general, are transcribed
|
||||||
|
# from scanned documents.
|
||||||
|
#
|
||||||
|
# Assemble revision 055 of AGC program Comanche by NASA
|
||||||
|
# 2021113-051. April 1, 1969.
|
||||||
|
#
|
||||||
|
# This AGC program shall also be referred to as Colossus 2A
|
||||||
|
#
|
||||||
|
# Prepared by
|
||||||
|
# Massachussets Institute of Technology
|
||||||
|
# 75 Cambridge Parkway
|
||||||
|
# Cambridge, Massachusetts
|
||||||
|
#
|
||||||
|
# under NASA contract NAS 9-4065.
|
||||||
|
#
|
||||||
|
# Refer directly to the online document mentioned above for further
|
||||||
|
# information. Please report any errors to info@sandroid.org.
|
||||||
|
|
||||||
|
# Page 883
|
||||||
|
BANK 35
|
||||||
|
|
||||||
|
SETLOC BODYATT
|
||||||
|
BANK
|
||||||
|
|
||||||
|
COUNT 37/CMBAT
|
||||||
|
|
||||||
|
# PDL 12D - 15D SAFE.
|
||||||
|
|
||||||
|
# VALUE OF GIMBAL AND BODY ANGLES VALID AT PIP TIME ARE SAVED DURING READACCS.
|
||||||
|
|
||||||
|
EBANK= RTINIT # LET INTERPRETER SET EB
|
||||||
|
|
||||||
|
CM/POSE TC INTPRET # COME HERE VIA AVEGEXIT.
|
||||||
|
|
||||||
|
SETPD VLOAD
|
||||||
|
0
|
||||||
|
VN # KVSCALE = (12800/ .3048) /2VS
|
||||||
|
VXSC PDVL
|
||||||
|
-KVSCALE # KVSCALE = .81491944
|
||||||
|
UNITW # FULL UNIT VECTOR
|
||||||
|
VXV VXSC # VREL = V - WE*R
|
||||||
|
UNITR
|
||||||
|
KWE
|
||||||
|
VAD STADR
|
||||||
|
STORE -VREL # SAVE FOR ENTRY GUIDANCE. REF COORDS
|
||||||
|
|
||||||
|
UNIT LXA,1
|
||||||
|
36D # ABVAL( -VREL) TO X1
|
||||||
|
STORE UXA/2 # -UVREL REF COORDS
|
||||||
|
|
||||||
|
VXV VCOMP
|
||||||
|
UNITR # .5 UNIT REF COORDS
|
||||||
|
UNIT SSP # THE FOLLOWING IS TO PROVIDE A STABLE
|
||||||
|
S1 # UN FOR THE END OF THE TERMINAL PHASE.
|
||||||
|
SPVQUIT DEC .019405 # 1000/ 2 VS
|
||||||
|
TIX,1 VLOAD # IF V-VQUIT POS, BRANCH.
|
||||||
|
CM/POSE2 # SAME UYA IN OLDUYA
|
||||||
|
OLDUYA # OTHERWISE CONTINUE TO USE OLDUYA
|
||||||
|
CM/POSE2 STORE UYA/2 # REF COORDS
|
||||||
|
|
||||||
|
STORE OLDUYA # RESTORE, OR SAVE AS CASE MAY BE.
|
||||||
|
|
||||||
|
VXV VCOMP
|
||||||
|
UXA/2 # FINISH OBTAINING TRAJECTORY TRIAD.
|
||||||
|
VSL1
|
||||||
|
STORE UZA/2 # REF COORDS
|
||||||
|
# Page 884
|
||||||
|
TLOAD # PICK UP CDUX, CDUY, CDUZ CORRESPONDING
|
||||||
|
AOG/PIP # TO PIPUP TIME IN 2'S C AND SAVE.
|
||||||
|
CM/TRIO STODL 24D
|
||||||
|
25D # AIG/PIP
|
||||||
|
|
||||||
|
RTB PUSH # TO PDL0
|
||||||
|
CDULOGIC
|
||||||
|
COS
|
||||||
|
STODL UBX/2 # CI /2
|
||||||
|
# AIG/PIP FROM PDL 0
|
||||||
|
SIN DCOMP
|
||||||
|
STODL UBX/2 +4 # -SI /2
|
||||||
|
26D # AMG/PIP
|
||||||
|
RTB PUSH # TO PDL 0
|
||||||
|
CDULOGIC
|
||||||
|
SIN PDDL # XCH PDL 0. SAVE SM /2
|
||||||
|
COS PDDL # CM /2 TO PDL 2
|
||||||
|
0 # SM /2
|
||||||
|
DCOMP VXSC
|
||||||
|
UBX/2
|
||||||
|
VSL1 # NOISE WON'T OVFL
|
||||||
|
STODL UBY/2 # =(-SMCI, NOISE, SMSI)/2
|
||||||
|
2 # CM /2 REPLACES NOISE
|
||||||
|
STODL UBY/2 +2 # UBY/2=(-SMCI, CM, SMSI)/2
|
||||||
|
24D # AOG/PIP
|
||||||
|
RTB PUSH # TO PDL 4
|
||||||
|
CDULOGIC
|
||||||
|
SIN PDDL # XCH PDL 4. SAVE SO /2
|
||||||
|
COS VXSC # CO /2
|
||||||
|
UBY/2
|
||||||
|
STODL UBY/2 # UBY/2=(-COSMCI, COCM, COSMSI)/4
|
||||||
|
4D # SO /2
|
||||||
|
DMP DCOMP
|
||||||
|
UBX/2 +4 # -SI /2
|
||||||
|
DAD
|
||||||
|
UBY/2 # INCREMENT BY (SOSI /4)
|
||||||
|
STODL UBY/2
|
||||||
|
# SO /2 FROM PDL 4
|
||||||
|
DMP DAD
|
||||||
|
UBX/2 # CI /2
|
||||||
|
UBY/2 +4
|
||||||
|
STOVL UBY/2 +4 # YB/4 PLATFORM COORDS
|
||||||
|
|
||||||
|
# YB = (-COSMCI + SOSI , COCM , COSMSI + SOCI )
|
||||||
|
|
||||||
|
UBY/2
|
||||||
|
VXM VSL2
|
||||||
|
REFSMMAT # .5 UNIT
|
||||||
|
STODL UBY/2 # YB/2 DONE REF COORDS
|
||||||
|
# Page 885
|
||||||
|
# CM /2 FROM PDL 2
|
||||||
|
VXSC VSL1
|
||||||
|
UBX/2
|
||||||
|
STODL UBX/2 # =( CMCI, NOISE, -CMSI)/2
|
||||||
|
STADR # SM /2 FROM PDL 0
|
||||||
|
STOVL UBX/2 +2 # SM /2 REPLACES NOISE
|
||||||
|
UBX/2 # XB/2 PLATFORM COORDS
|
||||||
|
|
||||||
|
# XB = ( CMCI , SM , -CMSI )
|
||||||
|
|
||||||
|
VXM VSL1
|
||||||
|
REFSMMAT # .5 UNIT
|
||||||
|
STORE UBX/2 # XB/2 DONE REF COORDS
|
||||||
|
|
||||||
|
VXV VSL1
|
||||||
|
UBY/2
|
||||||
|
STOVL UBZ/2 # ZB/2 DONE REF COORDS
|
||||||
|
|
||||||
|
# EQUIVALENT TO
|
||||||
|
# ZB = ( SOSMCI + COSI , -SOCM , -SOSMSI + COCI )
|
||||||
|
|
||||||
|
UXA/2 # -UVREL/2 = -UVA/2
|
||||||
|
VXV UNIT # GET UNIT(-UVREL*UBY)/2 = UL/2
|
||||||
|
UBY/2 # YB/2
|
||||||
|
PUSH DOT # UL/2 TO PDL 0,5
|
||||||
|
UZA/2 # UNA/2
|
||||||
|
STOVL COSTH # COS(ROLL)/4
|
||||||
|
0 # UL/2
|
||||||
|
|
||||||
|
DOT
|
||||||
|
UYA/2
|
||||||
|
STCALL SINTH # -SIN(ROLL)/4
|
||||||
|
ARCTRIG
|
||||||
|
STOVL 6D # -(ROLL/180) /2
|
||||||
|
UBY/2
|
||||||
|
DOT SL1 # -UVA.UBY = -SIN(BETA)
|
||||||
|
UXA/2 # -UVREL/2
|
||||||
|
ARCSIN
|
||||||
|
STOVL 7D # -(BETA/180) /2
|
||||||
|
UBX/2 # XB/2
|
||||||
|
DOT # UL.UBX = -SIN(ALFA)
|
||||||
|
0 # UL/2
|
||||||
|
STOVL SINTH # -SIN(ALFA)/4
|
||||||
|
DOT # UL/2 FROM PDL 0
|
||||||
|
UBZ/2
|
||||||
|
STCALL COSTH # COS(ALFA)/2
|
||||||
|
ARCTRIG
|
||||||
|
STOVL 8D # -(ALFA/180) /2
|
||||||
|
UNITR # UR/2 REF COORDS
|
||||||
|
DOT SL1
|
||||||
|
# Page 886
|
||||||
|
UZA/2 # MORE ACCURATE AT LARGE ARG.
|
||||||
|
ARCCOS
|
||||||
|
STORE 10D # (-GAMA/180)/2
|
||||||
|
|
||||||
|
TLOAD EXIT # ANGLES IN MPAC IN THE ORDER
|
||||||
|
# -( (ROLL, BETA, ALFA) /180)/2
|
||||||
|
6D # THESE VALUES CORRECT AT PIPUP TIME.
|
||||||
|
|
||||||
|
# Page 887
|
||||||
|
# BASIC SUBROUTINE TO UPDATE ATTITUDE ANGLES
|
||||||
|
|
||||||
|
EBANK= AOG
|
||||||
|
|
||||||
|
CM/ATUP CA EBAOG
|
||||||
|
TS EBANK
|
||||||
|
CMTR1 INDEX FIXLOC
|
||||||
|
CS 10D # (GAMA/180)/2
|
||||||
|
XCH GAMA
|
||||||
|
TS L
|
||||||
|
|
||||||
|
INHINT
|
||||||
|
# MUST REMAIN INHINTED UNTIL UPDATE OF BODY
|
||||||
|
# ANGLES, SO THAT GAMDIFSW IS VALID FIRST PASS
|
||||||
|
# INDICATOR.
|
||||||
|
|
||||||
|
CS CM/FLAGS
|
||||||
|
MASK BIT11 # GAMDIFSW=94D BIT11 INITLY=0
|
||||||
|
EXTEND # DON'T CALC GAMA DOT UNTIL HAVE FORMD
|
||||||
|
# ONE DIFFERENCE.
|
||||||
|
BZF DOGAMDOT # IS OK, GO ON.
|
||||||
|
ADS CM/FLAGS # KNOW BIT IS 0
|
||||||
|
TC NOGAMDOT # SET GAMDOT = 0
|
||||||
|
|
||||||
|
DOGAMDOT CS L
|
||||||
|
AD GAMA # DEL GAMA/360= T GAMDOT/360
|
||||||
|
EXTEND
|
||||||
|
MP TCDU # TCDU = .1 SEC, T = 2 SEC.
|
||||||
|
TS GAMDOT # GAMA DOT TCDU / 180
|
||||||
|
|
||||||
|
EXTEND # IGNORE GAMDOT IF LEQ .5 DEG/SEC
|
||||||
|
BZMF +2
|
||||||
|
COM
|
||||||
|
AD FIVE
|
||||||
|
EXTEND
|
||||||
|
BZMF +3 # SET GAMDOT=+0 AS TAG IF TOO SMALL.
|
||||||
|
|
||||||
|
NOGAMDOT CA ZERO # COME HERE INHINTED
|
||||||
|
TS GAMDOT
|
||||||
|
# FOR NOW LEAVE IN 2'S C
|
||||||
|
# UPDATE ANGLES BY CORRECTING EULER ANG
|
||||||
|
# FOR ACCRUED INCREMENT SINCE PIPUP
|
||||||
|
# R = R EUIL + R(NOW) - R(PIPUP)
|
||||||
|
CS MPAC # GET (R EUL/180) /2
|
||||||
|
DOUBLE # POSSIBLE OVERFLOW
|
||||||
|
TC CORANGOV # CORRECT FOR OVFL IF ANY
|
||||||
|
EXTEND
|
||||||
|
SU ROLL/PIP # GET INCR SINCE PIPUP
|
||||||
|
AD ROLL/180 # ONLY SINGLE OVFL POSSIBLE.
|
||||||
|
TC CORANGOV # CORRECT FOR OVFL IF ANY
|
||||||
|
# Page 888
|
||||||
|
TS TEMPROLL
|
||||||
|
|
||||||
|
CS MPAC +2 # GET (ALFA EUL/180) /2
|
||||||
|
DOUBLE # SAME AS FOR ROLL. NEEDED FOR EXT ATM DAP
|
||||||
|
TC CORANGOV # CORRECT FOR OVFL IF ANY
|
||||||
|
EXTEND
|
||||||
|
SU ALFA/PIP
|
||||||
|
AD ALFA/180
|
||||||
|
TC CORANGOV # CORRECT FOR OVFL IF ANY
|
||||||
|
TS TEMPALFA
|
||||||
|
|
||||||
|
CS MPAC +1 # GET (BETA EUL/180) /2
|
||||||
|
CMTR2 DOUBLE
|
||||||
|
EXTEND
|
||||||
|
SU BETA/PIP
|
||||||
|
AD BETA/180
|
||||||
|
XCH TEMPBETA # OVFL NOT EXPECTED.
|
||||||
|
|
||||||
|
CA EBANK3
|
||||||
|
TS EBANK
|
||||||
|
|
||||||
|
EBANK= PHSNAME5
|
||||||
|
EXTEND
|
||||||
|
DCA REPOSADR # THIS ASSUMES THAT THE TC PHASCHNG
|
||||||
|
DXCH PHSNAME5 # IS NOT CHANGED IN OCT 10035
|
||||||
|
# SERVICER.
|
||||||
|
|
||||||
|
CA EBAOG
|
||||||
|
TS EBANK
|
||||||
|
|
||||||
|
EBANK= AOG
|
||||||
|
REDOPOSE EXTEND # RE-STARTS COME HERE
|
||||||
|
DCA TEMPROLL
|
||||||
|
DXCH ROLL/180
|
||||||
|
CA TEMPBETA
|
||||||
|
TS BETA/180
|
||||||
|
|
||||||
|
RELINT
|
||||||
|
|
||||||
|
TC INTPRET # CAN'T TC DANZIG AFTER PHASCHNG.
|
||||||
|
CM/POSE3 VLOAD ABVAL # RETURN FROM CM/ATUP. (RESTART)
|
||||||
|
VN # 2(-7) M/CS
|
||||||
|
STORE VMAGI # FOR DISPLAY ON CALL.
|
||||||
|
|
||||||
|
GOTO
|
||||||
|
POSEXIT # ENDEXIT, STARTENT, OR SCALEPOP.
|
||||||
|
|
||||||
|
CORANGOV TS L
|
||||||
|
TC Q
|
||||||
|
INDEX A
|
||||||
|
# Page 889
|
||||||
|
CA LIMITS
|
||||||
|
ADS L
|
||||||
|
TC Q # COSTS 2 MCT TO USE. SEE ANGOVCOR.
|
||||||
|
|
||||||
|
-KVSCALE 2DEC -.81491944 # -12800/(2 VS .3048)
|
||||||
|
|
||||||
|
TCDU DEC .1 # TCDU = .1 SEC.
|
||||||
|
|
||||||
|
EBANK= AOG
|
||||||
|
REPOSADR 2CADR REDOPOSE
|
||||||
|
|
||||||
1474
LUNAR_LANDING_GUIDANCE_EQUATIONS.s
Normal file
1474
LUNAR_LANDING_GUIDANCE_EQUATIONS.s
Normal file
File diff suppressed because it is too large
Load Diff
Loading…
Reference in New Issue
Block a user