Source Code
These source-code files are part of a reconstructed copy of Luminary 163, the
first (unflown) release of the Apollo 14 Lunar Module (LM) Apollo Guidance
Computer (AGC) software.
The reconstruction began with reconstructed source code for Luminary 173. Changes between revision 163 and 173 were backed out, as described by Luminary memos 157 and 158. The reconstruction was verified by matching memory-bank checksums to those listed in drawing 2021152N. Note that page numbers in the reconstructed code match those for the baseline log section mentioned in each file's changelog; the page numbers for a real Luminary 163 listing would be different. Comments from the original source code are prefixed with a single '#' symbol, whereas comments added later are prefixed by "##" or "###". Report any errors noted by creating an issue report at the Virtual AGC project's GitHub repository. |
015735,000002: ## Copyright: Public domain.
015736,000003: ## Filename: GIMBAL_LOCK_AVOIDANCE.agc
015737,000004: ## Purpose: A section of Luminary revision 163.
015738,000005: ## It is part of the reconstructed source code for the first
015739,000006: ## (unflown) release of the flight software for the Lunar
015740,000007: ## Module's (LM) Apollo Guidance Computer (AGC) for Apollo 14.
015741,000008: ## The code has been recreated from a reconstructed copy of
015742,000009: ## Luminary 173, as well as Luminary memos 157 amd 158.
015743,000010: ## It has been adapted such that the resulting bugger words
015744,000011: ## exactly match those specified for Luminary 163 in NASA
015745,000012: ## drawing 2021152N, which gives relatively high confidence
015746,000013: ## that the reconstruction is correct.
015747,000014: ## Reference: p. 369
015748,000015: ## Assembler: yaYUL
015749,000016: ## Contact: Ron Burkey <info@sandroid.org>.
015750,000017: ## Website: www.ibiblio.org/apollo/index.html
015751,000018: ## Mod history: 2019-08-21 MAS Created from Luminary 173.
015752,000019:
Page 369 |
015754,000021: 15,2050 BANK 15
015755,000022:
015756,000023: 22,2000 SETLOC KALCMON1
015757,000024: 22,2000 BANK
015758,000025:
015759,000026:
015760,000027: # DETECTING GIMBAL LOCK
015761,000028: 22,2744 22,2744 LOCSKIRT EQUALS NOGIMLOC
015762,000029:
015763,000030: 22,2744 77614 NOGIMLOC SET
015764,000031: 22,2745 01074 CALCMAN3
015765,000032: 22,2746 70740 WCALC LXC,1 DLOAD*
015766,000033: 22,2747 01322 RATEINDX # CHOOSE THE DESIRED MANEUVER RATE
015767,000034: 22,2750 04772 ARATE,1 # FROM A LIST OF FOUR
015768,000035: 22,2751 45002 SR4 CALL # COMPUTE THE INCREMENTAL ROTATION MATRIX
015769,000036: 22,2752 44527 DELCOMP # DEL CORRESPONDING TO A 1 SEC ROTATION
015770,000037: # ABOUT COF
015771,000038: 22,2753 74343 DLOAD* VXSC
015772,000039: 22,2754 04772 ARATE,1
015773,000040: 22,2755 03270 COF
015774,000041: 22,2756 17325 STODL BRATE # COMPONENT MANEUVER RATES 45 DEG/SEC
015775,000042: 22,2757 03335 AM
015776,000043: 22,2760 55605 DMP DDV*
015777,000044: 22,2761 05002 ANGLTIME
015778,000045: 22,2762 04772 ARATE,1
015779,000046: 22,2763 77661 SR
015780,000047: 22,2764 20606 5
015781,000048: 22,2765 03333 STORE TM # MANEUVER EXECUTION TIME SCALED AS T2
015782,000049: 22,2766 77614 SETGO
015783,000050: 22,2767 01035 CALCMAN2 # 0(OFF) = CONTINUE MANEUVER
015784,000051: 22,2770 45010 NEWANGL +1 # 1(ON) = START MANEUVER
015785,000052: # THE FOUR SELECTABLE FREE FALL MANEUVER RATES SELECTED BY
015786,000053: # LOADING RATEINDX WITH 0,2,4,6, RESPECTIVELY
015787,000054:
015788,000055:
015789,000056: 22,2771 00221 24255 ARATE 2DEC .0088888888 # = 0.2 DEG/SEC $ 22.5 DEG/SEC
015790,000057: 22,2773 00554 02660 2DEC .0222222222 # = 0.5 DEG/SEC $ 22.5 DEG/SEC
015791,000058: 22,2775 02660 13301 2DEC .0888888888 # = 2.0 DEG/SEC $ 22.5 DEG/SEC
015792,000059: 22,2777 16161 30707 2DEC .4444444444 # = 10.0 DEG/SEC $ 22.5 DEG/SEC
015793,000060:
015794,000061: 22,3001 00003 04000 ANGLTIME 2DEC .0001907349 # = 100B-19 FUDGE FACTOR TO CONVERT
015795,000062: # MANEUVER ANGLE TO MANEUVER TIME
End of include-file GIMBAL_LOCK_AVOIDANCE.agc. Parent file is MAIN.agc