Source Code
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These source-code files are part of a reconstructed copy of Comanche 45, the
second release, though not the final mission release, of the Apollo 10
Command Module (CM) Apollo Guidance Computer (AGC) software. Comanche 45 was
preceded by Comanche 44 and followed by Comanche 45/2 (the flown release). The reconstruction
is believed to be exactly accurate, but in the absence of an actual Apollo-era
listing of Comanche 45, some explanation of the reconstruction process is needed
to insure confidence in that accuracy.
The starting point was the source code of Comanche 44 (itself previously accurately
reconstructed). Comanche 44 source code was then modified
by incorporating changes known from contemporary documentation to have been
made between revisions 44 and 45. The now-reconstructed Comanche 45 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 tend to match those in the Comanche 55, the
most-similar revision of Comanche for which we have access to an actual non-reconstructed hardcopy;
the source code would likely have different page numbers in a contemporary
Comanche 45 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 44. Here's a guide to the Apollo documentation referenced
in those annotations:
There is also
a detailed 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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057968,000002: ## Copyright: Public domain.
057969,000003: ## Filename: POWERED_FLIGHT_SUBROUTINES.agc
057970,000004: ## Purpose: A section of Comanche revision 045.
057971,000005: ## It is part of the reconstructed source code for the
057972,000006: ## second release of the flight software for the Command
057973,000007: ## Module's (CM) Apollo Guidance Computer (AGC) for Apollo 10.
057974,000008: ## The code has been recreated from a copy of Comanche 055. It
057975,000009: ## has been adapted such that the resulting bugger words
057976,000010: ## exactly match those specified for Comanche 45 in NASA drawing
057977,000011: ## 2021153D, which gives relatively high confidence that the
057978,000012: ## reconstruction is correct.
057979,000013: ## Assembler: yaYUL
057980,000014: ## Contact: Ron Burkey <info@sandroid.org>.
057981,000015: ## Website: www.ibiblio.org/apollo/index.html
057982,000016: ## Mod history: 2020-12-06 MAS Created from Comanche 44.
057983,000017:
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Page 1365
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057985,000019: 14,3423 BANK 14 # SAME FBANK AS THE FINDCDUD SUB-PROGRAM
057986,000020: 23,2000 SETLOC POWFLITE
057987,000021: 23,2000 BANK
057988,000022:
057989,000023: 23,3477 0142 EBANK= DEXDEX
057990,000024: 23,3477 COUNT* $$/POWFL
057991,000025:
057992,000026: # CDUTRIG, CDUTRIG1, CDUTRIG2, AND CD*TR*GS ALL COMPUTE THE SINES AND
057993,000027: # COSINES OF THREE 2'S COMPLEMENT ANGLES AND PLACE THE RESULT, DOUBLE
057994,000028: # PRECISION, IN THE SAME ORDER AS THE INPUTS, AT SINCDU AND COSCDU. AN
057995,000029: # ADDITIONAL OUTPUT IS THE 1'S COMPLEMENT ANGLES AT CDUSPOT. THESE
057996,000030: # ROUTINES GO OUT OF THEIR WAY TO LEAVE THE MPAC AREA AS THEY FIND IT,
057997,000031: # EXCEPT FOR THE GENERALLY UNIMPORTANT MPAC +2. THEY DIFFER ONLY IN
057998,000032: # WHERE THEY GET THE ANGLES, AND IN METHOD OF CALLING.
057999,000033:
058000,000034: # CDUTRIG (AND CDUTRIG1, WHICH CAN BE CALLED IN BASIC) COMPUTE THE
058001,000035: # SINES AND COSINES FROM THE CURRENT CONTENTS OF THE CDU REGISTERS.
058002,000036: # THE CONTENTS OF CDUTEMP, ETC., ARE NOT TOUCHED SO THAT THEY MAY
058003,000037: # CONTINUE TO FORM A CONSISTENT SET WITH THE LATEST PIPA READINGS.
058004,000038:
058005,000039: # CDUTRIG1 IS LIKE CDUTRIG EXCEPT THAT IT CAN BE CALLED IN BASIC.
058006,000040:
058007,000041: # CD*TR*GS FINDS CDU VALUES IN CDUSPOT RATHER THAN IN CDUTEMP. THIS
058008,000042: # ALLOWS USERS TO MAKE TRANSFORMATIONS USING ARBITRARY ANGLES, OR REAL
058009,000043: # ANGLES IN AN ORDER OTHER THAN X Y Z. A CALL TO THIS ROUTINE IS
058010,000044: # NECESSARY IN PREPARATION FOR A CALL TO AX*SR*T IN EITHER OF ITS TWO
058011,000045: # MODES (SMNB OR NBSM). SINCE AX*SR*T EXPECTS TO FIND THE SINES AND
058012,000046: # COSINES IN THE ORDER Y Z X THE ANGLES MUST HAVE BEEN PLACED IN CDUSPOT
058013,000047: # IN THIS ORDER. CD*TR*GS NEED NOT BE REPEATED WHEN AX*SR*T IS CALLED
058014,000048: # MORE THAN ONCE, PROVIDED THE ANGLES HAVE NOT CHANGED. NOTE THAT SINCE
058015,000049: # IT CLOBBERS BUF2 (IN THE SINE AND COSINE ROUTINES) CD*TR*GS CANNOT BE
058016,000050: # CALLED USING BANKCALL. SORRY.
058017,000051:
058018,000052: # CD*TR*G IS LIKE CD*TR*GS EXCEPT THAT IT CAN BE CALLED IN
058019,000053: # INTERPRETIVE.
058020,000054:
058021,000055: 23,3477 77776 CDUTRIG EXIT
058022,000056: 23,3500 03507 TC CDUTRIGS
058023,000057: 23,3501 06006 TC INTPRET
058024,000058: 23,3502 77616 RVQ
058025,000059:
058026,000060: 23,3503 77776 CD*TR*G EXIT
058027,000061: 23,3504 03515 TC CD*TR*GS
058028,000062: 23,3505 06006 TC INTPRET
058029,000063: 23,3506 77616 RVQ
058030,000064:
058031,000065: 23,3507 30032 CDUTRIGS CA CDUX
058032,000066: 23,3510 54772 TS CDUSPOT +4
058033,000067: 23,3511 30033 CA CDUY
058034,000068: 23,3512 54766 TS CDUSPOT
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Page 1366
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058036,000070: 23,3513 30034 CA CDUZ
058037,000071: 23,3514 54770 TS CDUSPOT +2
058038,000072:
058039,000073: 23,3515 00006 CD*TR*GS EXTEND
058040,000074: 23,3516 22142 QXCH TEM2
058041,000075: 23,3517 35015 CAF FOUR
058042,000076: 23,3520 76211 TR*GL**P MASK SIX # MAKE IT EVEN AND SMALLER
058043,000077: 23,3521 54143 TS TEM3
058044,000078: 23,3522 50143 INDEX TEM3
058045,000079: 23,3523 30766 CA CDUSPOT
058046,000080: 23,3524 52155 DXCH MPAC # STORING 2'S COMP ANGLE, LOADING MPAC
058047,000081: 23,3525 52127 DXCH VBUF +4 # STORING MPAC FOR LATER RESTORATION
058048,000082: 23,3526 04757 TC USPRCADR
058049,000083: 23,3527 45513 CADR CDULOGIC
058050,000084: 23,3530 00006 EXTEND
058051,000085: 23,3531 30155 DCA MPAC
058052,000086: 23,3532 50143 INDEX TEM3
058053,000087: 23,3533 52767 DXCH CDUSPOT # STORING 1'S COMPLEMENT ANGLE
058054,000088: 23,3534 04757 TC USPRCADR
058055,000089: 23,3535 01516 CADR COSINE
058056,000090: 23,3536 52155 DXCH MPAC
058057,000091: 23,3537 50143 INDEX TEM3
058058,000092: 23,3540 52745 DXCH COSCDU # STORING COSINE
058059,000093: 23,3541 00006 EXTEND
058060,000094: 23,3542 50143 INDEX TEM3
058061,000095: 23,3543 30767 DCA CDUSPOT # LOADING 1'S COMPLEMENT ANGLE
058062,000096: 23,3544 04757 TC USPRCADR
058063,000097: 23,3545 01530 CADR SINE +1 # SINE +1 EXPECTS ARGUMENT IN A AND L
058064,000098: 23,3546 52127 DXCH VBUF +4 # BRINGING UP PRIOR MPAC TO BE RESTORED
058065,000099: 23,3547 52155 DXCH MPAC
058066,000100: 23,3550 50143 INDEX TEM3
058067,000101: 23,3551 52737 DXCH SINCDU
058068,000102: 23,3552 10143 CCS TEM3
058069,000103: 23,3553 13520 TCF TR*GL**P
058070,000104: 23,3554 00142 TC TEM2
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Page 1367
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058072,000106: # ****************************************************************************************************************
058073,000107: # QUICTRIG, INTENDED FOR GUIDANCE CYCLE USE WHERE TIME IS CRITICAL, IS A MUCH FASTER VERSION OF CD*TR*GS.
058074,000108: # QUICTRIG COMPUTES AND STORES THE SINES AND COSINES OF THE 2'S COMPLEMENT ANGLES AT CDUSPOT, CDUSPOT +2,
058075,000109: # AND CDUSPOT +4. UNLIKE CD*TR*GS, QUICTRIG DOES NOT LEAVE THE 1'S COMPLEMENT VERSIONS OF THE ANGLES IN
058076,000110: # CDUSPOT. QUICTRIG'S EXECUTION TIME IS 4.1 MS; THIS IS 10 TIMES AS FAST AS CD*TR*GS. QUICTRIG MAY BE
058077,000111: # CALLED FROM INTERPRETIVE AS AN RTB OP-CODE, OR FROM BASIC VIA BANKCALL OR IBNKCALL.
058078,000112:
058079,000113: 23,3555 00004 QUICTRIG INHINT # INHINT SINCE DAP USES THE SAME TEMPS
058080,000114: 23,3556 00006 EXTEND
058081,000115: 23,3557 22061 QXCH ITEMP1
058082,000116: 23,3560 35015 CAF FOUR
058083,000117: 23,3561 76211 +4 MASK SIX
058084,000118: 23,3562 54062 TS ITEMP2
058085,000119: 23,3563 50062 INDEX ITEMP2
058086,000120: 23,3564 30766 CA CDUSPOT
058087,000121: 23,3565 05075 TC SPSIN
058088,000122: 23,3566 00006 EXTEND
058089,000123: 23,3567 75002 MP BIT14 # SCALE DOWN TO MATCH INTERPRETER OUTPUTS
058090,000124: 23,3570 50062 INDEX ITEMP2
058091,000125: 23,3571 52737 DXCH SINCDU
058092,000126: 23,3572 50062 INDEX ITEMP2
058093,000127: 23,3573 30766 CA CDUSPOT
058094,000128: 23,3574 05074 TC SPCOS
058095,000129: 23,3575 00006 EXTEND
058096,000130: 23,3576 75002 MP BIT14
058097,000131: 23,3577 50062 INDEX ITEMP2
058098,000132: 23,3600 52745 DXCH COSCDU
058099,000133: 23,3601 10062 CCS ITEMP2
058100,000134: 23,3602 13561 TCF QUICTRIG +4
058101,000135: 23,3603 30061 CA ITEMP1
058102,000136: 23,3604 00003 RELINT
058103,000137: 23,3605 00000 TC A
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Page 1368
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058105,000139: # ****************************************************************************************************************
058106,000140: # THESE INTERFACE ROUTINES MAKE IT POSSIBLE TO CALL AX*SR*T, ETC., IN
058107,000141: # INTERPRETIVE. LATER, WHERE POSSIBLE, THEY WILL BE ELIMINATED.
058108,000142:
058109,000143: # NBSM WILL BE THE FIRST TO GO. IT SHOULD NOT BE USED.
058110,000144:
058111,000145: 23,3606 77620 NBSM STQ
058112,000146: 23,3607 00047 X2
058113,000147: 23,3610 76740 LXC,1 VLOAD*
058114,000148: 23,3611 00050 S1 # BASE ADDRESS OF THE CDU ANGLES IS IN S1
058115,000149: 23,3612 00001 0,1
058116,000150: 23,3613 24767 STOVL CDUSPOT
058117,000151: 23,3614 00041 32D # VECTOR TO BE TRANSFORMED IS IN 32D
058118,000152: 23,3615 77624 CALL
058119,000153: 23,3616 47637 TRG*NBSM
058120,000154: 23,3617 34041 STCALL 32D # SINCE THERE'S NO STGOTO
058121,000155: 23,3620 00047 X2
058122,000156:
058123,000157: # THESE INTERFACE ROUTINES ARE PERMANENT. ALL RESTORE USER'S EBANK
058124,000158: # SETTING. ALL ARE STRICT INTERPRETIVE SUBROUTINES, CALLED USING "CALL",
058125,000159: # RETURNING VIA QPRET. ALL EXPECT AND RETURN THE VECTOR TO BE TRANSFOR-
058126,000160: # MED INTERPRETER-STYLE IN MPAC; COMPONENTS AT MPAC, MPAC +3, AND MPAC +5.
058127,000161:
058128,000162: # TRG*SMNB AND TRG*NBSM BOTH EXPECT TO SEE THE 2'S COMPLEMENT ANGLES
058129,000163: # AT CDUSPOT (ORDER Y Z X, AT CDUSPOT, CDUSPOT +2, AND CDUSPOT +4; ODD
058130,000164: # LOCATIONS NEED NOT BE ZEROED). TRG*NBSM DOES THE NB TO SM TRANSFOR-
058131,000165: # MATION; TRG*SMNB, VICE VERSA.
058132,000166:
058133,000167: # CDU*NBSM DOES ITS TRANSFORMATION USING THE PRESENT CONTENTS OF
058134,000168: # THE CDU COUNTERS. OTHERWISE IT IS LIKE TRG*NBSM.
058135,000169:
058136,000170: # CDU*SMNB IS THE COMPLEMENT OF CDU*NBSM.
058137,000171:
058138,000172: 23,3621 77776 CDU*SMNB EXIT
058139,000173: 23,3622 03507 TC CDUTRIGS
058140,000174: 23,3623 13626 TCF C*MM*N1
058141,000175:
058142,000176: 23,3624 77776 TRG*SMNB EXIT
058143,000177: 23,3625 03515 TC CD*TR*GS
058144,000178: 23,3626 07501 C*MM*N1 TC MPACVBUF # AX*SR*T EXPECTS VECTOR IN VBUF
058145,000179: 23,3627 46214 CS THREE # SIGNAL FOR SM TO NB TRANSFORMATION
058146,000180: 23,3630 03650 C*MM*N2 TC AX*SR*T
058147,000181: 23,3631 06006 TC INTPRET
058148,000182: 23,3632 43575 VLOAD RVQ
058149,000183: 23,3633 00123 VBUF
058150,000184:
058151,000185: 23,3634 77776 CDU*NBSM EXIT
058152,000186: 23,3635 03507 TC CDUTRIGS
058153,000187:
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Page 1369
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058155,000189:
058156,000190: 23,3636 13641 TCF C*MM*N3
058157,000191:
058158,000192: 23,3637 77776 TRG*NBSM EXIT
058159,000193: 23,3640 03515 TC CD*TR*GS
058160,000194: 23,3641 07501 C*MM*N3 TC MPACVBUF # FOR AX*SR*T
058161,000195: 23,3642 36214 CA THREE # SIGNAL FOR NB TO SM TRANSFORMATION
058162,000196: 23,3643 13630 TCF C*MM*N2
058163,000197:
058164,000198: # *NBSM* AND *SMNB* EXPECT TO SEE THE SINES AND COSINES (AT SINCDU
058165,000199: # AND COSCDU) RATHER THAN THE ANGLES THEMSELVES. OTHERWISE THEY ARE
058166,000200: # LIKE TRG*NBSM AND TRG*SMNB.
058167,000201:
058168,000202: # NOTE THAT JUST AS CD*TR*GS NEED BE CALLED ONLY ONCE FOR EACH SERIES
058169,000203: # OF TRANSFORMATIONS USING THE SAME ANGLES, SO TOO ONLY ONE OF TRG*NBSM
058170,000204: # AND TRG*SMNB NEED BE CALLED FOR EACH SERIES. FOR SUBSEQUENT TRANSFOR-
058171,000205: # MATIONS USE *NBSM* AND *SMNB*.
058172,000206:
058173,000207: 23,3644 77776 *SMNB* EXIT
058174,000208: 23,3645 13626 TCF C*MM*N1
058175,000209:
058176,000210: 23,3646 77776 *NBSM* EXIT
058177,000211: 23,3647 13641 TCF C*MM*N3
058178,000212:
058179,000213: # AX*SR*T COMBINES THE OLD SMNB AND NBSM. FOR THE NB TO SM
058180,000214: # TRANSFORMATION, ENTER WITH +3 IN A. FOR SM TO NB, ENTER WITH -3.
058181,000215: # THE VECTOR TO BE TRANSFORMED ARRIVES, AND IS RETURNED, IN VBUF.
058182,000216: # AX*SR*T EXPECTS TO FIND THE SINES AND COSINES OF THE ANGLES OF ROTATION
058183,000217: # AT SINCDU AND COSCDU, IN THE ORDER Y Z X. A CALL TO CD*TR*GS, WITH
058184,000218: # THE 2'S COMPLEMENT ANGLES (ORDER Y Z X) AT CDUSPOT, WILL TAKE CARE OF
058185,000219: # THIS. HERE IS A SAMPLE CALLING SEQUENCE:-
058186,000220: # TC CDUTRIGS
058187,000221: # CS THREE ("CA THREE" FOR NBSM)
058188,000222: # TC AX*SR*T
058189,000223: # THE CALL TO CD*TR*GS NEED NOT BE REPEATED, WHEN AX*SR*T IS CALLED MORE
058190,000224: # THAN ONCE, UNLESS THE ANGLES HAVE CHANGED.
058191,000225:
058192,000226: # AX*SR*T IS GUARANTEED SAFE ONLY FOR VECTORS OF MAGNITUDE LESS THAN
058193,000227: # UNITY. A LOOK AT THE CASE IN WHICH A VECTOR OF GREATER MAGNITUDE
058194,000228: # HAPPENS TO LIE ALONG AN AXIS OF THE SYSTEM TO WHICH IT IS TO BE TRANS-
058195,000229: # FORMED CONVINCES ONE THAT THIS IS A RESTRICTION WHICH MUST BE ACCEPTED.
058196,000230:
058197,000231: 23,3650 54142 AX*SR*T TS DEXDEX # WHERE IT BECOMES THE INDEX OF INDEXES
058198,000232: 23,3651 00006 EXTEND
058199,000233: 23,3652 22145 QXCH RTNSAVER
058200,000234:
058201,000235: 23,3653 10142 R*TL**P CCS DEXDEX # +3 --> 0 -3 --> 2
058202,000236: 23,3654 40142 CS DEXDEX # THUS: +2 --> 1 -2 --> 1
058203,000237: 23,3655 66214 AD THREE # +1 --> 2 -1 --> 0
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Page 1370
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058205,000239: 23,3656 00006 EXTEND
058206,000240: 23,3657 50000 INDEX A
058207,000241: 23,3660 33737 DCA INDEXI
058208,000242: 23,3661 52144 DXCH DEXI
058209,000243:
058210,000244: 23,3662 35017 CA ONE
058211,000245: 23,3663 54130 TS BUF
058212,000246: 23,3664 00006 EXTEND
058213,000247: 23,3665 50143 INDEX DEX1
058214,000248: 23,3666 40123 DCS VBUF
058215,000249: 23,3667 13671 TCF LOOP1 # REALLY BE A SUBTRACT, AND VICE VERSA
058216,000250:
058217,000251: 23,3670 52131 LOOP2 DXCH BUF # LOADING VECTOR COMPONENT, STORING INDEX
058218,000252:
058219,000253: 23,3671 52155 LOOP1 DXCH MPAC
058220,000254: 23,3672 33735 CA SINESLOC
058221,000255: 23,3673 60143 AD DEX1
058222,000256: 23,3674 54116 TS ADDRWD
058223,000257:
058224,000258: 23,3675 07056 TC DMPSUB # MULTIPLY BY SIN(CDUANGLE)
058225,000259: 23,3676 10142 CCS DEXDEX
058226,000260: 23,3677 52155 DXCH MPAC # NBSM CASE
058227,000261: 23,3700 13703 TCF +3
058228,000262: 23,3701 00006 EXTEND # SMNB CASE
058229,000263: 23,3702 40155 DCS MPAC
058230,000264: 23,3703 52134 DXCH TERM1TMP
058231,000265:
058232,000266: 23,3704 36211 CA SIX # SINCDU AND COSCDU (EACH 6 WORDS) MUST
058233,000267: 23,3705 26116 ADS ADDRWD # BE CONSECUTIVE AND IN THAT ORDER
058234,000268:
058235,000269: 23,3706 00006 EXTEND
058236,000270: 23,3707 50130 INDEX BUF
058237,000271: 23,3710 50143 INDEX DEX1
058238,000272: 23,3711 30123 DCA VBUF
058239,000273: 23,3712 52155 DXCH MPAC
058240,000274: 23,3713 07056 TC DMPSUB # MULTIPLY BY COS(CDUANGLE)
058241,000275: 23,3714 52155 DXCH MPAC
058242,000276: 23,3715 20134 DAS TERM1TMP
058243,000277: 23,3716 52134 DXCH TERM1TMP
058244,000278: 23,3717 20001 DDOUBL
058245,000279: 23,3720 50130 INDEX BUF
058246,000280: 23,3721 50143 INDEX DEX1
058247,000281: 23,3722 52123 DXCH VBUF
058248,000282: 23,3723 52131 DXCH BUF # LOADING INDEX, STORING VECTOR COMPONENT
058249,000283: 23,3724 10000 CCS A # 'CAUSE THAT'S WHERE THE INDEX NOW IS
058250,000284: 23,3725 13670 TCF LOOP2
058251,000285:
058252,000286: 23,3726 00006 EXTEND
058253,000287: 23,3727 26142 DIM DEXDEX # DECREMENT MAGNITUDE PRESERVING SIGN
058254,000288:
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Page 1371
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058256,000290: 23,3730 10142 TSTPOINT CCS DEXDEX # ONLY THE BRANCHING FUNCTION IS USED
058257,000291: 23,3731 13653 TCF R*TL**P
058258,000292: 23,3732 00145 TC RTNSAVER
058259,000293: 23,3733 13653 TCF R*TL**P
058260,000294: 23,3734 00145 TC RTNSAVER
058261,000295:
058262,000296: 23,3735 00736 SINESLOC ADRES SINCDU # FOR USE IN SETTING ADDRWD
058263,000297:
058264,000298: 23,3736 00004 INDEXI DEC 4 B-14 # ********** DON'T **********
058265,000299: 23,3737 00002 DEC 2 B-14 # ********** TOUCH **********
058266,000300: 23,3740 00000 DEC 0 B-14 # ********** THESE **********
058267,000301: 23,3741 00004 DEC 4 B-14 # ********** CONSTANTS **********
058268,000302:
058269,000303: # ****************************************************************************************************************
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Page 1372
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058271,000305: # THIS SUBROUTINE COMPUTES INCREMENTAL CHANGES IN CDU(GIMBAL) ANGLES FROM INCREMENTAL CHANGES ABOUT SM AXES. IT
058272,000306: # REQUIRES SM INCREMENTS AS A DP VECTOR SCALED AT ONE REVOLUTION(DTHETASM,+2,+4). SIN,COS(CDUY,Z,X) ARE IN
058273,000307: # SINCDU,+2,+4 AND COSCDU,+2,+4 RESPECTIVELY, SCALED TO ONE HALF. CDU INCREENTS ARE PLACED IN DCDU,+2,+4 SCALED TO
058274,000308: # ONE REVOLUTION.
058275,000309:
058276,000310: # * COS(IGA)SEC(MGA) 0 -SIN(IGA)SEC(MGA) *
058277,000311: # * *
058278,000312: # * -COS(IGA)TAN(MGA) 1 SIN(IGA)TAN(MGA) *
058279,000313: # * *
058280,000314: # * SIN(IGA) 0 COS(IGA) *
058281,000315:
058282,000316: 14,3423 BANK 14
058283,000317: 23,2000 SETLOC POWFLIT1
058284,000318: 23,2000 BANK
058285,000319:
058286,000320: 23,3742 41345 SMCDURES DLOAD DMP
058287,000321: 23,3743 03212 DTHETASM
058288,000322: 23,3744 00745 COSCDUY
058289,000323:
058290,000324: 23,3745 41325 PDDL DMP
058291,000325: 23,3746 03216 DTHETASM +4
058292,000326: 23,3747 00737 SINCDUY
058293,000327:
058294,000328: 23,3750 77621 BDSU
058295,000329: 23,3751 77671 DDV
058296,000330: 23,3752 00747 COSCDUZ
058297,000331: 23,3753 03204 STORE DCDU
058298,000332:
058299,000333: 23,3754 72405 DMP SL1 # SCALE
058300,000334: 23,3755 00741 SINCDUZ
058301,000335: 23,3756 77621 BDSU
058302,000336:
058303,000337: 23,3757 03214 DTHETASM +2
058304,000338: 23,3760 17206 STODL DCDU +2
058305,000339: 23,3761 03212 DTHETASM
058306,000340:
058307,000341: 23,3762 65205 DMP PDDL
058308,000342: 23,3763 00737 SINCDUY
058309,000343: 23,3764 03216 DTHETASM +4
058310,000344:
058311,000345: 23,3765 43205 DMP DAD
058312,000346: 23,3766 00745 COSCDUY
058313,000347: 23,3767 77752 SL1
058314,000348: 23,3770 03210 STORE DCDU +4
058315,000349: 23,3771 77616 RVQ
058316,000350:
End of include-file POWERED_FLIGHT_SUBROUTINES.agc. Parent file is MAIN.agc