Source Code
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These source-code files are part of a reconstructed copy of Comanche 44, the
initial release (though not the final mission release) of the Apollo 10
Command Module (CM) Apollo Guidance Computer (AGC) software. Subsequent releases
were Comanche 45 and Comanche 45/2 (the flown release on Apollo 10). The reconstruction
is believed to be exactly accurate, but in the absence of an actual Apollo-era
listing of Comanche 44, some explanation of the reconstruction process is needed
to insure confidence in that accuracy.
The starting point was the source code of Comanche 51
(separately previously reconstructed from an Apollo-era listing of Comanche 55,
flown on Apollo 11). Comanche 51 source code was then modified
by undoing changes known to have been made between revisions 44 and 51. The now-reconstructed
Comanche 44 source code was verified by assembling it and checking that the assembled code had
the expected known-correct memory-bank checksums.
Note that page numbers in the reconstructed code match those on the Comanche 55 printout,
although the source code would likely have different page numbers in a contemporary
Comanche 44 listing.
Annotations that were not present in the contemporary source code have been added to the reconstructed
code to justify each change relative to Comanche 51. Here's a guide to the Apollo documentation referenced
in those annotations:
In most cases, only the titles (rather than the full texts) of PCRs are known. In addition to the
explanatory annotations, there is also
a step-by-step commentary about the reconstruction process.
Comments expected to have been present in 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.
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058480,000002: ## Copyright: Public domain.
058481,000003: ## Filename: POWERED_FLIGHT_SUBROUTINES.agc
058482,000004: ## Purpose: A section of Comanche revision 044.
058483,000005: ## It is part of the reconstructed source code for the
058484,000006: ## original release of the flight software for the Command
058485,000007: ## Module's (CM) Apollo Guidance Computer (AGC) for Apollo 10.
058486,000008: ## The code has been recreated from a copy of Comanche 055. It
058487,000009: ## has been adapted such that the resulting bugger words
058488,000010: ## exactly match those specified for Comanche 44 in NASA drawing
058489,000011: ## 2021153D, which gives relatively high confidence that the
058490,000012: ## reconstruction is correct.
058491,000013: ## Assembler: yaYUL
058492,000014: ## Contact: Ron Burkey <info@sandroid.org>.
058493,000015: ## Website: www.ibiblio.org/apollo/index.html
058494,000016: ## Mod history: 2020-12-03 MAS Created from Comanche 51.
058495,000017:
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Page 1365
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058497,000019: 14,3423 BANK 14 # SAME FBANK AS THE FINDCDUD SUB-PROGRAM
058498,000020: 23,2000 SETLOC POWFLITE
058499,000021: 23,2000 BANK
058500,000022:
058501,000023: 23,3477 0142 EBANK= DEXDEX
058502,000024: 23,3477 COUNT* $$/POWFL
058503,000025:
058504,000026: # CDUTRIG, CDUTRIG1, CDUTRIG2, AND CD*TR*GS ALL COMPUTE THE SINES AND
058505,000027: # COSINES OF THREE 2'S COMPLEMENT ANGLES AND PLACE THE RESULT, DOUBLE
058506,000028: # PRECISION, IN THE SAME ORDER AS THE INPUTS, AT SINCDU AND COSCDU. AN
058507,000029: # ADDITIONAL OUTPUT IS THE 1'S COMPLEMENT ANGLES AT CDUSPOT. THESE
058508,000030: # ROUTINES GO OUT OF THEIR WAY TO LEAVE THE MPAC AREA AS THEY FIND IT,
058509,000031: # EXCEPT FOR THE GENERALLY UNIMPORTANT MPAC +2. THEY DIFFER ONLY IN
058510,000032: # WHERE THEY GET THE ANGLES, AND IN METHOD OF CALLING.
058511,000033:
058512,000034: # CDUTRIG (AND CDUTRIG1, WHICH CAN BE CALLED IN BASIC) COMPUTE THE
058513,000035: # SINES AND COSINES FROM THE CURRENT CONTENTS OF THE CDU REGISTERS.
058514,000036: # THE CONTENTS OF CDUTEMP, ETC., ARE NOT TOUCHED SO THAT THEY MAY
058515,000037: # CONTINUE TO FORM A CONSISTENT SET WITH THE LATEST PIPA READINGS.
058516,000038:
058517,000039: # CDUTRIG1 IS LIKE CDUTRIG EXCEPT THAT IT CAN BE CALLED IN BASIC.
058518,000040:
058519,000041: # CD*TR*GS FINDS CDU VALUES IN CDUSPOT RATHER THAN IN CDUTEMP. THIS
058520,000042: # ALLOWS USERS TO MAKE TRANSFORMATIONS USING ARBITRARY ANGLES, OR REAL
058521,000043: # ANGLES IN AN ORDER OTHER THAN X Y Z. A CALL TO THIS ROUTINE IS
058522,000044: # NECESSARY IN PREPARATION FOR A CALL TO AX*SR*T IN EITHER OF ITS TWO
058523,000045: # MODES (SMNB OR NBSM). SINCE AX*SR*T EXPECTS TO FIND THE SINES AND
058524,000046: # COSINES IN THE ORDER Y Z X THE ANGLES MUST HAVE BEEN PLACED IN CDUSPOT
058525,000047: # IN THIS ORDER. CD*TR*GS NEED NOT BE REPEATED WHEN AX*SR*T IS CALLED
058526,000048: # MORE THAN ONCE, PROVIDED THE ANGLES HAVE NOT CHANGED. NOTE THAT SINCE
058527,000049: # IT CLOBBERS BUF2 (IN THE SINE AND COSINE ROUTINES) CD*TR*GS CANNOT BE
058528,000050: # CALLED USING BANKCALL. SORRY.
058529,000051:
058530,000052: # CD*TR*G IS LIKE CD*TR*GS EXCEPT THAT IT CAN BE CALLED IN
058531,000053: # INTERPRETIVE.
058532,000054:
058533,000055: 23,3477 77776 CDUTRIG EXIT
058534,000056: 23,3500 03507 TC CDUTRIGS
058535,000057: 23,3501 06006 TC INTPRET
058536,000058: 23,3502 77616 RVQ
058537,000059:
058538,000060: 23,3503 77776 CD*TR*G EXIT
058539,000061: 23,3504 03515 TC CD*TR*GS
058540,000062: 23,3505 06006 TC INTPRET
058541,000063: 23,3506 77616 RVQ
058542,000064:
058543,000065: 23,3507 30032 CDUTRIGS CA CDUX
058544,000066: 23,3510 54772 TS CDUSPOT +4
058545,000067: 23,3511 30033 CA CDUY
058546,000068: 23,3512 54766 TS CDUSPOT
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Page 1366
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058548,000070: 23,3513 30034 CA CDUZ
058549,000071: 23,3514 54770 TS CDUSPOT +2
058550,000072:
058551,000073: 23,3515 00006 CD*TR*GS EXTEND
058552,000074: 23,3516 22142 QXCH TEM2
058553,000075: 23,3517 35015 CAF FOUR
058554,000076: 23,3520 76211 TR*GL**P MASK SIX # MAKE IT EVEN AND SMALLER
058555,000077: 23,3521 54143 TS TEM3
058556,000078: 23,3522 50143 INDEX TEM3
058557,000079: 23,3523 30766 CA CDUSPOT
058558,000080: 23,3524 52155 DXCH MPAC # STORING 2'S COMP ANGLE, LOADING MPAC
058559,000081: 23,3525 52127 DXCH VBUF +4 # STORING MPAC FOR LATER RESTORATION
058560,000082: 23,3526 04757 TC USPRCADR
058561,000083: 23,3527 45513 CADR CDULOGIC
058562,000084: 23,3530 00006 EXTEND
058563,000085: 23,3531 30155 DCA MPAC
058564,000086: 23,3532 50143 INDEX TEM3
058565,000087: 23,3533 52767 DXCH CDUSPOT # STORING 1'S COMPLEMENT ANGLE
058566,000088: 23,3534 04757 TC USPRCADR
058567,000089: 23,3535 01516 CADR COSINE
058568,000090: 23,3536 52155 DXCH MPAC
058569,000091: 23,3537 50143 INDEX TEM3
058570,000092: 23,3540 52745 DXCH COSCDU # STORING COSINE
058571,000093: 23,3541 00006 EXTEND
058572,000094: 23,3542 50143 INDEX TEM3
058573,000095: 23,3543 30767 DCA CDUSPOT # LOADING 1'S COMPLEMENT ANGLE
058574,000096: 23,3544 04757 TC USPRCADR
058575,000097: 23,3545 01530 CADR SINE +1 # SINE +1 EXPECTS ARGUMENT IN A AND L
058576,000098: 23,3546 52127 DXCH VBUF +4 # BRINGING UP PRIOR MPAC TO BE RESTORED
058577,000099: 23,3547 52155 DXCH MPAC
058578,000100: 23,3550 50143 INDEX TEM3
058579,000101: 23,3551 52737 DXCH SINCDU
058580,000102: 23,3552 10143 CCS TEM3
058581,000103: 23,3553 13520 TCF TR*GL**P
058582,000104: 23,3554 00142 TC TEM2
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Page 1367
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058584,000106: # ****************************************************************************************************************
058585,000107: # QUICTRIG, INTENDED FOR GUIDANCE CYCLE USE WHERE TIME IS CRITICAL, IS A MUCH FASTER VERSION OF CD*TR*GS.
058586,000108: # QUICTRIG COMPUTES AND STORES THE SINES AND COSINES OF THE 2'S COMPLEMENT ANGLES AT CDUSPOT, CDUSPOT +2,
058587,000109: # AND CDUSPOT +4. UNLIKE CD*TR*GS, QUICTRIG DOES NOT LEAVE THE 1'S COMPLEMENT VERSIONS OF THE ANGLES IN
058588,000110: # CDUSPOT. QUICTRIG'S EXECUTION TIME IS 4.1 MS; THIS IS 10 TIMES AS FAST AS CD*TR*GS. QUICTRIG MAY BE
058589,000111: # CALLED FROM INTERPRETIVE AS AN RTB OP-CODE, OR FROM BASIC VIA BANKCALL OR IBNKCALL.
058590,000112:
058591,000113: 23,3555 00004 QUICTRIG INHINT # INHINT SINCE DAP USES THE SAME TEMPS
058592,000114: 23,3556 00006 EXTEND
058593,000115: 23,3557 22061 QXCH ITEMP1
058594,000116: 23,3560 35015 CAF FOUR
058595,000117: 23,3561 76211 +4 MASK SIX
058596,000118: 23,3562 54062 TS ITEMP2
058597,000119: 23,3563 50062 INDEX ITEMP2
058598,000120: 23,3564 30766 CA CDUSPOT
058599,000121: 23,3565 05075 TC SPSIN
058600,000122: 23,3566 00006 EXTEND
058601,000123: 23,3567 75002 MP BIT14 # SCALE DOWN TO MATCH INTERPRETER OUTPUTS
058602,000124: 23,3570 50062 INDEX ITEMP2
058603,000125: 23,3571 52737 DXCH SINCDU
058604,000126: 23,3572 50062 INDEX ITEMP2
058605,000127: 23,3573 30766 CA CDUSPOT
058606,000128: 23,3574 05074 TC SPCOS
058607,000129: 23,3575 00006 EXTEND
058608,000130: 23,3576 75002 MP BIT14
058609,000131: 23,3577 50062 INDEX ITEMP2
058610,000132: 23,3600 52745 DXCH COSCDU
058611,000133: 23,3601 10062 CCS ITEMP2
058612,000134: 23,3602 13561 TCF QUICTRIG +4
058613,000135: 23,3603 30061 CA ITEMP1
058614,000136: 23,3604 00003 RELINT
058615,000137: 23,3605 00000 TC A
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Page 1368
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058617,000139: # ****************************************************************************************************************
058618,000140: # THESE INTERFACE ROUTINES MAKE IT POSSIBLE TO CALL AX*SR*T, ETC., IN
058619,000141: # INTERPRETIVE. LATER, WHERE POSSIBLE, THEY WILL BE ELIMINATED.
058620,000142:
058621,000143: # NBSM WILL BE THE FIRST TO GO. IT SHOULD NOT BE USED.
058622,000144:
058623,000145: 23,3606 77620 NBSM STQ
058624,000146: 23,3607 00047 X2
058625,000147: 23,3610 76740 LXC,1 VLOAD*
058626,000148: 23,3611 00050 S1 # BASE ADDRESS OF THE CDU ANGLES IS IN S1
058627,000149: 23,3612 00001 0,1
058628,000150: 23,3613 24767 STOVL CDUSPOT
058629,000151: 23,3614 00041 32D # VECTOR TO BE TRANSFORMED IS IN 32D
058630,000152: 23,3615 77624 CALL
058631,000153: 23,3616 47637 TRG*NBSM
058632,000154: 23,3617 34041 STCALL 32D # SINCE THERE'S NO STGOTO
058633,000155: 23,3620 00047 X2
058634,000156:
058635,000157: # THESE INTERFACE ROUTINES ARE PERMANENT. ALL RESTORE USER'S EBANK
058636,000158: # SETTING. ALL ARE STRICT INTERPRETIVE SUBROUTINES, CALLED USING "CALL",
058637,000159: # RETURNING VIA QPRET. ALL EXPECT AND RETURN THE VECTOR TO BE TRANSFOR-
058638,000160: # MED INTERPRETER-STYLE IN MPAC; COMPONENTS AT MPAC, MPAC +3, AND MPAC +5.
058639,000161:
058640,000162: # TRG*SMNB AND TRG*NBSM BOTH EXPECT TO SEE THE 2'S COMPLEMENT ANGLES
058641,000163: # AT CDUSPOT (ORDER Y Z X, AT CDUSPOT, CDUSPOT +2, AND CDUSPOT +4; ODD
058642,000164: # LOCATIONS NEED NOT BE ZEROED). TRG*NBSM DOES THE NB TO SM TRANSFOR-
058643,000165: # MATION; TRG*SMNB, VICE VERSA.
058644,000166:
058645,000167: # CDU*NBSM DOES ITS TRANSFORMATION USING THE PRESENT CONTENTS OF
058646,000168: # THE CDU COUNTERS. OTHERWISE IT IS LIKE TRG*NBSM.
058647,000169:
058648,000170: # CDU*SMNB IS THE COMPLEMENT OF CDU*NBSM.
058649,000171:
058650,000172: 23,3621 77776 CDU*SMNB EXIT
058651,000173: 23,3622 03507 TC CDUTRIGS
058652,000174: 23,3623 13626 TCF C*MM*N1
058653,000175:
058654,000176: 23,3624 77776 TRG*SMNB EXIT
058655,000177: 23,3625 03515 TC CD*TR*GS
058656,000178: 23,3626 07501 C*MM*N1 TC MPACVBUF # AX*SR*T EXPECTS VECTOR IN VBUF
058657,000179: 23,3627 46214 CS THREE # SIGNAL FOR SM TO NB TRANSFORMATION
058658,000180: 23,3630 03650 C*MM*N2 TC AX*SR*T
058659,000181: 23,3631 06006 TC INTPRET
058660,000182: 23,3632 43575 VLOAD RVQ
058661,000183: 23,3633 00123 VBUF
058662,000184:
058663,000185: 23,3634 77776 CDU*NBSM EXIT
058664,000186: 23,3635 03507 TC CDUTRIGS
058665,000187:
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Page 1369
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058667,000189:
058668,000190: 23,3636 13641 TCF C*MM*N3
058669,000191:
058670,000192: 23,3637 77776 TRG*NBSM EXIT
058671,000193: 23,3640 03515 TC CD*TR*GS
058672,000194: 23,3641 07501 C*MM*N3 TC MPACVBUF # FOR AX*SR*T
058673,000195: 23,3642 36214 CA THREE # SIGNAL FOR NB TO SM TRANSFORMATION
058674,000196: 23,3643 13630 TCF C*MM*N2
058675,000197:
058676,000198: # *NBSM* AND *SMNB* EXPECT TO SEE THE SINES AND COSINES (AT SINCDU
058677,000199: # AND COSCDU) RATHER THAN THE ANGLES THEMSELVES. OTHERWISE THEY ARE
058678,000200: # LIKE TRG*NBSM AND TRG*SMNB.
058679,000201:
058680,000202: # NOTE THAT JUST AS CD*TR*GS NEED BE CALLED ONLY ONCE FOR EACH SERIES
058681,000203: # OF TRANSFORMATIONS USING THE SAME ANGLES, SO TOO ONLY ONE OF TRG*NBSM
058682,000204: # AND TRG*SMNB NEED BE CALLED FOR EACH SERIES. FOR SUBSEQUENT TRANSFOR-
058683,000205: # MATIONS USE *NBSM* AND *SMNB*.
058684,000206:
058685,000207: 23,3644 77776 *SMNB* EXIT
058686,000208: 23,3645 13626 TCF C*MM*N1
058687,000209:
058688,000210: 23,3646 77776 *NBSM* EXIT
058689,000211: 23,3647 13641 TCF C*MM*N3
058690,000212:
058691,000213: # AX*SR*T COMBINES THE OLD SMNB AND NBSM. FOR THE NB TO SM
058692,000214: # TRANSFORMATION, ENTER WITH +3 IN A. FOR SM TO NB, ENTER WITH -3.
058693,000215: # THE VECTOR TO BE TRANSFORMED ARRIVES, AND IS RETURNED, IN VBUF.
058694,000216: # AX*SR*T EXPECTS TO FIND THE SINES AND COSINES OF THE ANGLES OF ROTATION
058695,000217: # AT SINCDU AND COSCDU, IN THE ORDER Y Z X. A CALL TO CD*TR*GS, WITH
058696,000218: # THE 2'S COMPLEMENT ANGLES (ORDER Y Z X) AT CDUSPOT, WILL TAKE CARE OF
058697,000219: # THIS. HERE IS A SAMPLE CALLING SEQUENCE:-
058698,000220: # TC CDUTRIGS
058699,000221: # CS THREE ("CA THREE" FOR NBSM)
058700,000222: # TC AX*SR*T
058701,000223: # THE CALL TO CD*TR*GS NEED NOT BE REPEATED, WHEN AX*SR*T IS CALLED MORE
058702,000224: # THAN ONCE, UNLESS THE ANGLES HAVE CHANGED.
058703,000225:
058704,000226: # AX*SR*T IS GUARANTEED SAFE ONLY FOR VECTORS OF MAGNITUDE LESS THAN
058705,000227: # UNITY. A LOOK AT THE CASE IN WHICH A VECTOR OF GREATER MAGNITUDE
058706,000228: # HAPPENS TO LIE ALONG AN AXIS OF THE SYSTEM TO WHICH IT IS TO BE TRANS-
058707,000229: # FORMED CONVINCES ONE THAT THIS IS A RESTRICTION WHICH MUST BE ACCEPTED.
058708,000230:
058709,000231: 23,3650 54142 AX*SR*T TS DEXDEX # WHERE IT BECOMES THE INDEX OF INDEXES
058710,000232: 23,3651 00006 EXTEND
058711,000233: 23,3652 22145 QXCH RTNSAVER
058712,000234:
058713,000235: 23,3653 10142 R*TL**P CCS DEXDEX # +3 --> 0 -3 --> 2
058714,000236: 23,3654 40142 CS DEXDEX # THUS: +2 --> 1 -2 --> 1
058715,000237: 23,3655 66214 AD THREE # +1 --> 2 -1 --> 0
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Page 1370
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058717,000239: 23,3656 00006 EXTEND
058718,000240: 23,3657 50000 INDEX A
058719,000241: 23,3660 33737 DCA INDEXI
058720,000242: 23,3661 52144 DXCH DEXI
058721,000243:
058722,000244: 23,3662 35017 CA ONE
058723,000245: 23,3663 54130 TS BUF
058724,000246: 23,3664 00006 EXTEND
058725,000247: 23,3665 50143 INDEX DEX1
058726,000248: 23,3666 40123 DCS VBUF
058727,000249: 23,3667 13671 TCF LOOP1 # REALLY BE A SUBTRACT, AND VICE VERSA
058728,000250:
058729,000251: 23,3670 52131 LOOP2 DXCH BUF # LOADING VECTOR COMPONENT, STORING INDEX
058730,000252:
058731,000253: 23,3671 52155 LOOP1 DXCH MPAC
058732,000254: 23,3672 33735 CA SINESLOC
058733,000255: 23,3673 60143 AD DEX1
058734,000256: 23,3674 54116 TS ADDRWD
058735,000257:
058736,000258: 23,3675 07056 TC DMPSUB # MULTIPLY BY SIN(CDUANGLE)
058737,000259: 23,3676 10142 CCS DEXDEX
058738,000260: 23,3677 52155 DXCH MPAC # NBSM CASE
058739,000261: 23,3700 13703 TCF +3
058740,000262: 23,3701 00006 EXTEND # SMNB CASE
058741,000263: 23,3702 40155 DCS MPAC
058742,000264: 23,3703 52134 DXCH TERM1TMP
058743,000265:
058744,000266: 23,3704 36211 CA SIX # SINCDU AND COSCDU (EACH 6 WORDS) MUST
058745,000267: 23,3705 26116 ADS ADDRWD # BE CONSECUTIVE AND IN THAT ORDER
058746,000268:
058747,000269: 23,3706 00006 EXTEND
058748,000270: 23,3707 50130 INDEX BUF
058749,000271: 23,3710 50143 INDEX DEX1
058750,000272: 23,3711 30123 DCA VBUF
058751,000273: 23,3712 52155 DXCH MPAC
058752,000274: 23,3713 07056 TC DMPSUB # MULTIPLY BY COS(CDUANGLE)
058753,000275: 23,3714 52155 DXCH MPAC
058754,000276: 23,3715 20134 DAS TERM1TMP
058755,000277: 23,3716 52134 DXCH TERM1TMP
058756,000278: 23,3717 20001 DDOUBL
058757,000279: 23,3720 50130 INDEX BUF
058758,000280: 23,3721 50143 INDEX DEX1
058759,000281: 23,3722 52123 DXCH VBUF
058760,000282: 23,3723 52131 DXCH BUF # LOADING INDEX, STORING VECTOR COMPONENT
058761,000283: 23,3724 10000 CCS A # 'CAUSE THAT'S WHERE THE INDEX NOW IS
058762,000284: 23,3725 13670 TCF LOOP2
058763,000285:
058764,000286: 23,3726 00006 EXTEND
058765,000287: 23,3727 26142 DIM DEXDEX # DECREMENT MAGNITUDE PRESERVING SIGN
058766,000288:
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Page 1371
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058768,000290: 23,3730 10142 TSTPOINT CCS DEXDEX # ONLY THE BRANCHING FUNCTION IS USED
058769,000291: 23,3731 13653 TCF R*TL**P
058770,000292: 23,3732 00145 TC RTNSAVER
058771,000293: 23,3733 13653 TCF R*TL**P
058772,000294: 23,3734 00145 TC RTNSAVER
058773,000295:
058774,000296: 23,3735 00736 SINESLOC ADRES SINCDU # FOR USE IN SETTING ADDRWD
058775,000297:
058776,000298: 23,3736 00004 INDEXI DEC 4 B-14 # ********** DON'T **********
058777,000299: 23,3737 00002 DEC 2 B-14 # ********** TOUCH **********
058778,000300: 23,3740 00000 DEC 0 B-14 # ********** THESE **********
058779,000301: 23,3741 00004 DEC 4 B-14 # ********** CONSTANTS **********
058780,000302:
058781,000303: # ****************************************************************************************************************
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Page 1372
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058783,000305: # THIS SUBROUTINE COMPUTES INCREMENTAL CHANGES IN CDU(GIMBAL) ANGLES FROM INCREMENTAL CHANGES ABOUT SM AXES. IT
058784,000306: # REQUIRES SM INCREMENTS AS A DP VECTOR SCALED AT ONE REVOLUTION(DTHETASM,+2,+4). SIN,COS(CDUY,Z,X) ARE IN
058785,000307: # SINCDU,+2,+4 AND COSCDU,+2,+4 RESPECTIVELY, SCALED TO ONE HALF. CDU INCREENTS ARE PLACED IN DCDU,+2,+4 SCALED TO
058786,000308: # ONE REVOLUTION.
058787,000309:
058788,000310: # * COS(IGA)SEC(MGA) 0 -SIN(IGA)SEC(MGA) *
058789,000311: # * *
058790,000312: # * -COS(IGA)TAN(MGA) 1 SIN(IGA)TAN(MGA) *
058791,000313: # * *
058792,000314: # * SIN(IGA) 0 COS(IGA) *
058793,000315:
058794,000316: 14,3423 BANK 14
058795,000317: 23,2000 SETLOC POWFLIT1
058796,000318: 23,2000 BANK
058797,000319:
058798,000320: 23,3742 41345 SMCDURES DLOAD DMP
058799,000321: 23,3743 03212 DTHETASM
058800,000322: 23,3744 00745 COSCDUY
058801,000323:
058802,000324: 23,3745 41325 PDDL DMP
058803,000325: 23,3746 03216 DTHETASM +4
058804,000326: 23,3747 00737 SINCDUY
058805,000327:
058806,000328: 23,3750 77621 BDSU
058807,000329: 23,3751 77671 DDV
058808,000330: 23,3752 00747 COSCDUZ
058809,000331: 23,3753 03204 STORE DCDU
058810,000332:
058811,000333: 23,3754 72405 DMP SL1 # SCALE
058812,000334: 23,3755 00741 SINCDUZ
058813,000335: 23,3756 77621 BDSU
058814,000336:
058815,000337: 23,3757 03214 DTHETASM +2
058816,000338: 23,3760 17206 STODL DCDU +2
058817,000339: 23,3761 03212 DTHETASM
058818,000340:
058819,000341: 23,3762 65205 DMP PDDL
058820,000342: 23,3763 00737 SINCDUY
058821,000343: 23,3764 03216 DTHETASM +4
058822,000344:
058823,000345: 23,3765 43205 DMP DAD
058824,000346: 23,3766 00745 COSCDUY
058825,000347: 23,3767 77752 SL1
058826,000348: 23,3770 03210 STORE DCDU +4
058827,000349: 23,3771 77616 RVQ
058828,000350:
End of include-file POWERED_FLIGHT_SUBROUTINES.agc. Parent file is MAIN.agc