Source Code
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These source-code files were derived from scans of the
Colossus 237 (Apollo 8 Command Module) program listing from the private collection of original
AGC developer Fred Martin. Scanning was by Ron Burkey. Pre-existing Colossus 249
(Apollo 9 CM) source files were used as a template, and changes between Colossus 249
and Colossus 237 were manually transcribed by a team of volunteers. Note
that the page images
presented online are of reduced quality, and that additional images
are available. Report any conversion errors or legibility
problems in page images to info@sandroid.org.
Notations on the program listing read, in part:GAP: ASSEMBLE REVISION 237 OF AGC PROGRAM COLOSSUS BY NASA 2021111-031 1:17 AUG. 24, 1968Note that the date is the date of the printout, not the date of the program revision. |
021690,000002: ## Copyright: Public domain.
021691,000003: ## Filename: P76.agc
021692,000004: ## Purpose: Part of the source code for Colossus build 237.
021693,000005: ## This is for the Command Module's (CM) Apollo Guidance
021694,000006: ## Computer (AGC), for Apollo 8.
021695,000007: ## Assembler: yaYUL
021696,000008: ## Contact: Jim Lawton <jim DOT lawton AT gmail DOT com>
021697,000009: ## Website: www.ibiblio.org/apollo/index.html
021698,000010: ## Page Scans: www.ibiblio.org/apollo/ScansForConversion/Colossus237/
021699,000011: ## Mod history: 2011-02-05 JL Adapted from corresponding Colossus 249 file.
021700,000012: ## 2016-12-31 RSB Proofed comment text using octopus/ProoferComments,
021701,000013: ## and corrected errors found.
021702,000014:
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Page 500 |
021704,000016: # 1) PROGRAM NAME - TARGET DELTA V PROGRAM (P76).
021705,000017: # 2) FUNCTIONAL DESCRIPTION - UPON ENTRY BY ASTRONAUT ACTION, P76 FLASHES DSKY REQUESTS TO THE ASTRONAUT
021706,000018: # TO PROVIDE VIA DSKY (1) THE DELTA V TO BE APPLIED TO THE OTHER VEHICLE STATE VECTOR AND (2) THE
021707,000019: # TIME (TIG) AT WHICH THE OTHER VEHICLE VELOCITY WAS CHANGED BY EXECUTION OF A THRUSTING MANEUVER. THE
021708,000020: # OTHER VEHICLE STATE VECTOR IS INTEGRATED TO TIG AND UPDATED BY THE ADDITION OF DELTA V (DELTA V HAVING
021709,000021: # BEEN TRANSFORMED FROM LV TO REF COSYS). USING INTEGRVS, THE PROGRAM THEN INTEGRATES THE OTHER
021710,000022: # VEHICLE STATE VECTOR TO THE STATE VECTOR OF THIS VEHICLE, THUS INSURING THAT THE W-MATRIX AND BOTH VEHICLE
021711,000023: # STATES CORRESPOND TO THE SAME TIME.
021712,000024: # 3) ERASABLE INITIALIZATION REQUIRED - NONE.
021713,000025: # 4) CALLING SEQUENCES AND EXIT MODES - CALLED BY ASTRONAUT REQUEST THRU DSKY V 37 E 76 E.
021714,000026: # EXITS BY TCF ENDOFJOB.
021715,000027: # 5) OUTPUT - OTHER VEHICLE STATE VECTOR INTEGRATED TO TIG AND INCREMENTED BY DELTA V IN REF COSYS.
021716,000028: # THE PUSHLIST CONTAINS THE MATRIX BY WHICH THE INPUT DELTA V MUST BE POST-MULTIPLIED TO CONVERT FROM LV
021717,000029: # TO REF COSYS.
021718,000030: # 6) DEBRIS - OTHER VEHICLE STATE VECTOR.
021719,000031: # 7) SUBROUTINES CALLED - BANKCALL,GOXDSPF,CSMPREC (OR LEMPREC),ATOPCSM (OR ATOPLEM),INTSTALL,INTWAKE, PHASCHNG
021720,000032: # INTPRET, INTEGRVS, AND MINIRECT.
021721,000033:
021722,000034: # 8) FLAG USE - MOONFLAG,CMOONFLAG,INTYPFLG,RASFLAG, AND MARKCTR.
021723,000035:
021724,000036: 30,2000 BANK 30
021725,000037: 13,2000 SETLOC P76LOC
021726,000038: 13,2000 BANK
021727,000039:
021728,000040: 13,2036 COUNT* $$/P76
021729,000041:
021730,000042: 13,2036 E7,1412 EBANK= TIG
021731,000043:
021732,000044: 13,2036 05435 P76 TC UPFLAG
021733,000045: 13,2037 00031 ADRES TRACKFLG
021734,000046:
021735,000047: 13,2040 32163 CAF V06N84 # FLASH LAST DELTA V,
021736,000048: 13,2041 04555 TC BANKCALL # AND WAIT FOR KEYBOARD ACTION.
021737,000049: 13,2042 20624 CADR GOFLASH
021738,000050: 13,2043 12155 TCF ENDP76
021739,000051: 13,2044 02046 TC +2 # PROCEED
021740,000052: 13,2045 02040 TC -5 # STORE DATA AND REPEAT FLASHING
021741,000053: 13,2046 32164 CAF V06N84 +1 # FLASH VERB 06 NOUN 33, DISPLAY LAST TIG,
021742,000054: 13,2047 04555 TC BANKCALL # AND WAIT FOR KEYBOARD ACTION.
021743,000055: 13,2050 20624 CADR GOFLASH
021744,000056: 13,2051 12155 TCF ENDP76
021745,000057: 13,2052 02054 TC +2
021746,000058: 13,2053 02046 TC -5
021747,000059: 13,2054 06006 TC INTPRET # RETURN TO INTERPRETIVE CODE
021748,000060: 13,2055 77745 DLOAD # SET D(MPAC)=TIG IN CSEC B28
021749,000061: 13,2056 03413 TIG
021750,000062: 13,2057 34041 STCALL TDEC1 # SET TDEC1=TIG FOR ORBITAL INTEGRATION
021751,000063: 13,2060 27036 OTHPREC
021752,000064: 13,2061 53575 COMPMAT VLOAD UNIT
021753,000065: 13,2062 00001 RATT
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021755,000067: 13,2063 77676 VCOMP # U(-R)
021756,000068: 13,2064 00031 STORE 24D # U(-R) TO 24D
021757,000069: 13,2065 53435 VXV UNIT # U(-R)XV = U(VXR)
021758,000070: 13,2066 00007 VATT
021759,000071: 13,2067 00023 STORE 18D
021760,000072: 13,2070 53435 VXV UNIT # U(VXR)XU(-R) = U((RXV)XR)
021761,000073: 13,2071 00031 24D
021762,000074: 13,2072 24015 STOVL 12D
021763,000075: 13,2073 03540 DELVOV
021764,000076: 13,2074 76505 VXM VSL1 # V(MPAC)=DELTA V IN REFCOSYS
021765,000077: 13,2075 00015 12D
021766,000078: 13,2076 77655 VAD
021767,000079: 13,2077 00007 VATT
021768,000080: 13,2100 00007 STORE 6 # V(PD6)=VATT + DELTA V
021769,000081: 13,2101 77624 CALL # PREVENT WOULD-BE USER OF ORBITAL
021770,000082: 13,2102 27371 INTSTALL # INTEG FROM INTERFERING WITH UPDATING
021771,000083: 13,2103 77624 CALL
021772,000084: 13,2104 26165 P76SUB1
021773,000085: 13,2105 53775 VLOAD VSR*
021774,000086: 13,2106 00007 6
021775,000087: 13,2107 57176 0,2
021776,000088: 13,2110 25543 STOVL VCV
021777,000089: 13,2111 00001 RATT
021778,000090: 13,2112 77657 VSR*
021779,000091: 13,2113 57176 0,2
021780,000092: 13,2114 15535 STODL RCV
021781,000093: 13,2115 03413 TIG
021782,000094: 13,2116 01517 STORE TET
021783,000095: 13,2117 71214 CLEAR DLOAD
021784,000096: 13,2120 01673 INTYPFLG
021785,000097: 13,2121 01571 TETTHIS
021786,000098: 13,2122 34041 INTOTHIS STCALL TDEC1
021787,000099: 13,2123 27066 INTEGRVS
021788,000100: 13,2124 77624 CALL
021789,000101: 13,2125 27371 INTSTALL
021790,000102: 13,2126 77775 VLOAD
021791,000103: 13,2127 00017 RATT1
021792,000104: 13,2130 01503 STORE RRECT
021793,000105: 13,2131 15535 STODL RCV
021794,000106: 13,2132 00015 TAT
021795,000107: 13,2133 25517 STOVL TET
021796,000108: 13,2134 00025 VATT1
021797,000109: 13,2135 77624 CALL
021798,000110: 13,2136 23360 MINIRECT
021799,000111: 13,2137 77776 EXIT
021800,000112: 13,2140 05301 TC PHASCHNG
021801,000113: 13,2141 04024 OCT 04024
021802,000114:
021803,000115: 13,2142 05435 TC UPFLAG
021804,000116: 13,2143 00236 ADRES REINTFLG
021805,000117:
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021807,000119: 13,2144 06006 TC INTPRET
021808,000120: 13,2145 77624 CALL
021809,000121: 13,2146 26711 ATOPOTH
021810,000122: 13,2147 77531 SSP EXIT
021811,000123: 13,2150 00053 QPRET
021812,000124: 13,2151 26154 OUT
021813,000125: 13,2152 04555 TC BANKCALL # PERMIT USE OF ORBITAL INTEGRATION
021814,000126: 13,2153 27426 CADR INTWAKE1
021815,000127: 13,2154 77776 OUT EXIT
021816,000128: 13,2155 34714 ENDP76 CAF ZERO
021817,000129: 13,2156 55126 TS MARKCTR # CLEAR RR TRACKING MARK COUNTER
021818,000130: 13,2157 55125 TS VHFCNT
021819,000131:
021820,000132: 13,2160 37716 CAF NEGONE
021821,000133: 13,2161 55734 TS MRKBUF2 # INVALIDATE MARK BUFFER
021822,000134:
021823,000135: 13,2162 14106 TCF GOTOPOOH
021824,000136:
021825,000137: 13,2163 01524 V06N84 NV 0684
021826,000138: 13,2164 01441 NV 0633
021827,000139: 13,2165 43174 P76SUB1 AXT,2 SET
021828,000140: 13,2166 00002 2
021829,000141: 13,2167 00063 MOONFLAG # SET MEANS MOON IS SPHERE OF INFLUENCE.
021830,000142: 13,2170 77014 BON AXT,2
021831,000143: 13,2171 04303 CMOONFLG # SET MEANS PERM CM STATE IN LUNAR SPHERE.
021832,000144: 13,2172 00052 QPRET
021833,000145: 13,2173 00000 0
021834,000146: 13,2174 43414 CLEAR RVQ
021835,000147: 13,2175 00263 MOONFLAG
End of include-file P76.agc. Parent file is MAIN.agc