Source Code
|
These source-code files were obtained by digitally photographing
an Artemis 72 program listing from a private collection and then
modifying pre-existing Comanche 55 (Apollo 11) source files to
incorporate changes. Note that the page images
presented online are of reduced quality, and that additional images
may be 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 072 OF AGC PROGRAM ARTEMIS BY NASA 2021114-011 11:40 FEB. 26, 1971 THIS AGC PROGRAM SHALL ALSO BE REFERRED TO AS COLOSSUS 3 THIS PROGRAM IS INTENDED FOR USE IN THE CM AS SPECIFIED IN REPORT R-577. THIS PROGRAM WAS PREPARED UNDER OSR PROJECT 55-23890, SPONSORED BY THE MANNED SPACECRAFT CENTER OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION THROUGH CONTRACT NAS 9-4065 WITH THE CHARLES STARK DRAPER LABORATORY, MASSACHUSETTS INSTITUTE OF TECHNOLOGY, CAMBRIDGE, MASS. |
052999,000002: # Copyright: Public domain.
053000,000003: # Filename: PLANETARY_INERTIAL_ORIENTATION.agc
053001,000004: # Purpose: Part of the source code for Artemis (i.e., Colossus 3),
053002,000005: # build 072. This is for the Command Module's (CM)
053003,000006: # Apollo Guidance Computer (AGC), we believe for
053004,000007: # Apollo 15-17.
053005,000008: # Assembler: yaYUL
053006,000009: # Contact: Sergio Navarro <sergionavarrog@gmail.com>
053007,000010: # Website: www.ibiblio.org/apollo/index.html
053008,000011: # Page scans: www.ibiblio.org/apollo/ScansForConversion/Artemis072/
053009,000012: # Mod history: 2009-09-03 SN Adapted from corresponding Comanche 055 file.
053010,000013: # 2009-09-05 JL Fix typos. Remove code not in Artemis072.
053011,000014: # 2010-02-20 RSB Un-##'d this header.
053012,000015:
|
|
Page 1243 |
053014,000017: # PLANETARY INERTIAL ORIENTATION
053015,000018:
053016,000019: # ..... RP-TO-R SUBROUTINE .....
053017,000020: # SUBROUTINE TO CONVERT RP (VECTOR IN PLANETARY COORDINATE SYSTEM, EITHER
053018,000021: # EARTH-FIXED OR MOON-FIXED) TO R (SAME VECTOR IN BASIC REF. SYSTEM)
053019,000022:
053020,000023: # R = MT(T) * (RP + LP X RP) MT = M MATRIX TRANSPOSE
053021,000024:
053022,000025: # CALLING SEQUENCE
053023,000026: # L CALL
053024,000027: # L+1 RP-TO-R
053025,000028:
053026,000029: # SUBROUTINES USED
053027,000030: # EARTHMX, MOONMX, EARTHL
053028,000031:
053029,000032: # ITEMS AVAILABLE FROM LAUNCH DATA
053030,000033: # 504LM = THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL, EXPRESSED
053031,000034: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
053032,000035:
053033,000036: # ITEMS NECESSARY FOR SUBR. USED (SEE DESCRIPTION OF SUBR.)
053034,000037:
053035,000038: # INPUT
053036,000039: # MPAC = 0 FOR EARTH, NON-ZERO FOR MOON
053037,000040: # 0-5D = RP VECTOR
053038,000041: # 6-7D = TIME
053039,000042:
053040,000043: # OUTPUT
053041,000044: # MPAC = R VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
053042,000045:
053043,000046: 26,2000 SETLOC PLANTIN
053044,000047: 26,2000 BANK
053045,000048:
053046,000049: 26,3345 COUNT* $$/LUROT
053047,000050:
053048,000051: 26,3345 46020 RP-TO-R STQ BHIZ
053049,000052: 26,3346 00050 RPREXIT
053050,000053: 26,3347 55362 RPTORA
053051,000054: 26,3350 77624 CALL # COMPUTE M MATRIX FOR MOON
053052,000055: 26,3351 55416 MOONMX # LP=LM FOR MOON RADIANS B0
053053,000056: 26,3352 77775 VLOAD
053054,000057: 26,3353 02012 504LM
053055,000058: 26,3354 53235 RPTORB VXV VAD
053056,000059: 26,3355 00001 504RPR
053057,000060: 26,3356 00001 504RPR
053058,000061: 26,3357 52105 VXM GOTO
053059,000062: 26,3360 00025 MMATRIX # MPAC=R=MT(T)*(RP+LPXRP)
053060,000063: 26,3361 55406 RPRPXXXX # RESET PUSHLOC TO 0 BEFORE EXITING
053061,000064: 26,3362 77624 RPTORA CALL # EARTH COMPUTATIONS
053062,000065: 26,3363 55567 EARTHMX # M MATRIX B-1
053063,000066: # AND L VECTOR RADIANS B0
053064,000067: 26,3364 76521 MXV VSL1 # LP=M(T)*L RAD B-0
053065,000068: 26,3365 00025 MMATRIX
053066,000069: 26,3366 77650 GOTO
|
|
Page 1244 |
053068,000071: 26,3367 55354 RPTORB
053069,000072:
|
|
Page 1245 |
053071,000074: # ..... R-TO-RP SUBROUTINE .....
053072,000075: # SUBROUTINE TO CONVERT R (VECTOR IN REFERENCE COORD. SYSTEM) TO RP
053073,000076: # (VECTOR IN PLANETARY COORD SYSTEM) EITHER EARTH-FIXED OR MOON-FIXED
053074,000077:
053075,000078: # RP = M(T) * (R - L X R)
053076,000079:
053077,000080: # CALLING SEQUENCE
053078,000081: # L CALL
053079,000082: # L+1 R-TO-RP
053080,000083:
053081,000084: # SUBROUTINES USED
053082,000085: # EARTHMX, MOONMX, EARTHL
053083,000086:
053084,000087: # INPUT
053085,000088: # MPAC = 0 FOR EARTH, NON-ZERO FOR MOON
053086,000089: # 0-5D = R VECTOR
053087,000090: # 6-7D = TIME
053088,000091:
053089,000092: # ITEMS AVAILABLE FROM LAUNCH DATA
053090,000093: # 504LM = THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL, EXPRESSED
053091,000094: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
053092,000095:
053093,000096: # ITEMS NECESSARY FOR SUBROUTINES USED (SEE DESCRIPTION OF SUBR.)
053094,000097:
053095,000098: # OUTPUT
053096,000099: # MPAC = RP VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
053097,000100:
053098,000101: 26,3370 46020 R-TO-RP STQ BHIZ
053099,000102: 26,3371 00050 RPREXIT
053100,000103: 26,3372 55412 RTORPA
053101,000104: 26,3373 77624 CALL
053102,000105: 26,3374 55416 MOONMX
053103,000106: 26,3375 61375 VLOAD VXM
053104,000107: 26,3376 02012 504LM # LP=LM
053105,000108: 26,3377 00025 MMATRIX
053106,000109: 26,3400 77772 VSL1 # L = MT(T)*LP RADIANS B0
053107,000110: 26,3401 51235 RTORPB VXV BVSU
053108,000111: 26,3402 00001 504RPR
053109,000112: 26,3403 00001 504RPR
053110,000113: 26,3404 77721 MXV # M(T)*(R-LXR) B-2
053111,000114: 26,3405 00025 MMATRIX
053112,000115: 26,3406 40372 RPRPXXXX VSL1 SETPD
053113,000116: 26,3407 00001 0D
053114,000117: 26,3410 77650 GOTO
053115,000118: 26,3411 00050 RPREXIT
053116,000119: 26,3412 77624 RTORPA CALL # EARTH COMPUTATIONS
053117,000120: 26,3413 55567 EARTHMX
053118,000121: 26,3414 77650 GOTO # MPAC=L=(-AX,-AY,0) RAD B-0
053119,000122: 26,3415 55401 RTORPB
053120,000123:
|
|
Page 1246 |
053122,000125: # ..... MOONMX SUBROUTINE .....
053123,000126: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE MOON
053124,000127:
053125,000128: # CALLING SEQUENCE
053126,000129: # L CALL
053127,000130: # L+1 MOONMX
053128,000131:
053129,000132: # SUBROUTINES USED
053130,000133: # NEWANGLE
053131,000134:
053132,000135: # INPUT
053133,000136: # 6-7D = TIME
053134,000137:
053135,000138: # ITEMS AVAILABLE FROM LAUNCH DATA
053136,000139: # BSUBO, BDOT
053137,000140: # TIMSUBO, NODIO, NODDOT, FSUBO, FDOT
053138,000141: # COSI = COS(I) B-1
053139,000142: # SINI = SIN(I) B-1
053140,000143: # I IS THE ANGLE BETWEEN THE MEAN LUNAR EQUATORIAL PLANE AND THE
053141,000144: # PLANE OF THE ECLIPTIC (1 DEGREE 32.1 MINUTES)
053142,000145:
053143,000146: # OUTPUT
053144,000147: # MMATRIX = 3X3 M MATRIX B-1 (STORED IN VAC AREA)
053145,000148:
053146,000149: 26,3416 40220 MOONMX STQ SETPD
053147,000150: 26,3417 00051 EARTHMXX
053148,000151: 26,3420 00011 8D
053149,000152: 26,3421 77770 AXT,1 # B REQUIRES SL 0, SL 5 IN NEWANGLE
053150,000153: 26,3422 00005 5
053151,000154: 26,3423 65345 DLOAD PDDL # PD 10D 8-9D=BSUBO
053152,000155: 26,3424 15647 BSUBO # 10-11D=BDOT
053153,000156: 26,3425 15641 BDOT
053154,000157: 26,3426 45006 PUSH CALL # PD 12D
053155,000158: 26,3427 55543 NEWANGLE # EXIT WITH PD 8D AND MPAC= B REVS B0
053156,000159: 26,3430 71406 PUSH COS # PD 10D
053157,000160: 26,3431 14041 STODL COB # PD 8D COS(B) B-1
053158,000161: 26,3432 77756 SIN # SIN(B) B-1
053159,000162: 26,3433 14043 STODL SOB # SETUP INPUT FOR NEWANGLE
053160,000163: 26,3434 15645 FSUBO # 8-9D=FSUBO
053161,000164: 26,3435 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=FDOT
053162,000165: 26,3436 15637 FDOT
053163,000166: 26,3437 45170 AXT,1 CALL # F REQUIRES SL 1, SL 6 IN NEWANGLE
053164,000167: 26,3440 00004 4
053165,000168: 26,3441 55543 NEWANGLE # EXIT WITH PD 8D AND MPAC= F REVS B0
053166,000169: 26,3442 14027 STODL AVECTR +2 # SAVE F TEMP
053167,000170: 26,3443 15643 NODIO # 8-9D=NODIO
053168,000171: 26,3444 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=NODDOT
053169,000172: 26,3445 15635 NODDOT # MPAC=T
053170,000173: 26,3446 45170 AXT,1 CALL # NODE REQUIRES SL 0, SL 5 IN NEWANGLE
053171,000174: 26,3447 00005 5
053172,000175: 26,3450 55543 NEWANGLE # EXIT WITH PD 8D AND MPAC= NODI REVS B0
|
|
Page 1247 |
053174,000177: 26,3451 71406 PUSH COS # PD 10D 8-9D= NODI REVS B0
053175,000178: 26,3452 77606 PUSH # PD 12D 10-11D= COS(NODI) B-1
053176,000179: 26,3453 00025 STORE AVECTR
053177,000180: 26,3454 76405 DMP SL1R
053178,000181: 26,3455 00041 COB # COS(NODI) B-1
053179,000182: 26,3456 14035 STODL BVECTR +2 # PD 10D 20-25D=AVECTR= COB*SIN(NODI)
053180,000183: 26,3457 76405 DMP SL1R # SOB*SIN(NODI)
053181,000184: 26,3460 00043 SOB
053182,000185: 26,3461 14037 STODL BVECTR +4 # PD 8D
053183,000186: 26,3462 41556 SIN PUSH # PD 10D -SIN(NODI) B-1
053184,000187: 26,3463 77676 DCOMP # 26-31D=BVECTR= COB*COS(NODI)
053185,000188: 26,3464 14033 STODL BVECTR # PD 8D SOB*COS(NODI)
053186,000189: 26,3465 00027 AVECTR +2 # MOVE F FROM TEMP LOC. TO 504F
053187,000190: 26,3466 14007 STODL 504F
053188,000191: 26,3467 76405 DMP SL1R
053189,000192: 26,3470 00041 COB
053190,000193: 26,3471 14027 STODL AVECTR +2
053191,000194: 26,3472 00011 SINNODI # 8-9D=SIN(NODI) B-1
053192,000195: 26,3473 76405 DMP SL1R
053193,000196: 26,3474 00043 SOB
053194,000197: 26,3475 14031 STODL AVECTR +4 # 0
053195,000198: 26,3476 15336 HI6ZEROS # 8-13D= CVECTR= -SOB B-1
053196,000199: 26,3477 57525 PDDL DCOMP # PD 10D COB
053197,000200: 26,3500 00043 SOB
053198,000201: 26,3501 63325 PDDL PDVL # PD 12D THEN PD 14D
053199,000202: 26,3502 00041 COB
053200,000203: 26,3503 00033 BVECTR
053201,000204: 26,3504 63361 VXSC PDVL # PD 20D BVECTR*SINI B-2
053202,000205: 26,3505 15633 SINI
053203,000206: 26,3506 00011 CVECTR
053204,000207: 26,3507 53361 VXSC VAD # PD 14D CVECTR*COSI B-2
053205,000208: 26,3510 15631 COSI
053206,000209: 26,3511 77772 VSL1
053207,000210: 26,3512 24041 STOVL MMATRIX +12D # PD 8D M2=BVECTR*SINI+CVECTR*COSI B-1
053208,000211: 26,3513 63361 VXSC PDVL # PD 14D
053209,000212: 26,3514 15633 SINI # CVECTR*SINI B-2
053210,000213: 26,3515 00033 BVECTR
053211,000214: 26,3516 52361 VXSC VSU # PD 8D BVECTR*COSI B-2
053212,000215: 26,3517 15631 COSI
053213,000216: 26,3520 65372 VSL1 PDDL # PD 14D
053214,000217: 26,3521 00007 504F # 8-13D=DVECTR=BVECTR*COSI-CVECTR*SINI B-1
053215,000218: 26,3522 74346 COS VXSC
053216,000219: 26,3523 00011 DVECTR
053217,000220: 26,3524 73525 PDDL SIN # PD 20D 14-19D= DVECTR*COSF B-2
053218,000221: 26,3525 00007 504F
053219,000222: 26,3526 52361 VXSC VSU # PD 14D AVECTR*SINF B-2
053220,000223: 26,3527 00025 AVECTR
053221,000224: 26,3530 77772 VSL1
053222,000225: 26,3531 14033 STODL MMATRIX +6 # M1= AVECTR*SINF-DVECTR*COSF B-1
053223,000226: 26,3532 00007 504F
|
|
Page 1248 |
053225,000228: 26,3533 74356 SIN VXSC # PD 8D
053226,000229: 26,3534 71525 PDDL COS # PD 14D 8-13D=DVECTR*SINF B-2
053227,000230: 26,3535 00007 504F
053228,000231: 26,3536 53361 VXSC VAD # PD 8D AVECTR*COSF B-2
053229,000232: 26,3537 00025 AVECTR
053230,000233: 26,3540 57572 VSL1 VCOMP
053231,000234: 26,3541 34025 STCALL MMATRIX # M0= -(AVECTR*COSF+DVECTR*SINF) B-1
053232,000235: 26,3542 00051 EARTHMXX
053233,000236:
053234,000237: # COMPUTE X=X0+(XDOT)(T+T0)
053235,000238: # 8-9D= X0 (REVS B-0), PUSHLOC SET AT 12D
053236,000239: # 10-11D=XDOT (REVS/CSEC) SCALED B+23 FOR WEARTH,B+28 FOR NODDOT AND BDOT
053237,000240: # AND B+27 FOR FDOT
053238,000241: # X1=DIFFERENCE IN 23 AND SCALING OF XDOT, =0 FOR WEARTH, 5 FOR NDDOT AND
053239,000242: # BDOT AND 4 FOR FDOT
053240,000243: # 6-7D=T (CSEC B-28), TIMSUBO= (CSEC B-42 TRIPLE PREC.)
053241,000244:
053242,000245: 26,3543 54345 NEWANGLE DLOAD SR # ENTER PD 12D
053243,000246: 26,3544 00007 6D
053244,000247: 26,3545 20617 14D
053245,000248: 26,3546 72371 TAD TLOAD # CHANGE MODE TO TP
053246,000249: 26,3547 01707 TIMSUBO
053247,000250: 26,3550 00155 MPAC
053248,000251: 26,3551 14017 STODL TIMSUBM # T+T0 CSEC B-42
053249,000252: 26,3552 00020 TIMSUBM +1
053250,000253: 26,3553 77605 DMP # PD 10D MULT BY XDOT IN 10-11D
053251,000254: 26,3554 43257 SL* DAD # PD 8D ADD X0 IN 8-9D AFTER SHIFTING
053252,000255: 26,3555 20206 5,1 # SUCH THAT SCALING IS B-0
053253,000256: 26,3556 67206 PUSH SLOAD # PD 10D SAVE PARTIAL (X0+XDOT*T) IN 8-9D
053254,000257: 26,3557 00017 TIMSUBM
053255,000258: 26,3560 41261 SL DMP
053256,000259: 26,3561 20212 9D
053257,000260: 26,3562 00013 10D # XDOT
053258,000261: 26,3563 43257 SL* DAD # PD 8D SHIFT SUCH THAT THIS PART OF X
053259,000262: 26,3564 20213 10D,1 # IS SCALED REVS/CSEC B-0
053260,000263: 26,3565 43400 HERE BOV RVQ # TURN OFF OVERFLOW IF SET BY SHIFT
053261,000264: 26,3566 55565 HERE # INSTRUCTION BEFORE EXITING.
053262,000265: # MPAC=X=X0+(XDOT)(T+T0) REVS B0
053263,000266:
|
|
Page 1249 |
053265,000268: # ..... EARTHMX SUBROUTINE .....
053266,000269: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE EARTH
053267,000270:
053268,000271: # CALLING SEQUENCE
053269,000272: # L CALL
053270,000273: # L+1 EARTHMX
053271,000274:
053272,000275: # SUBROUTINE USED
053273,000276: # NEWANGLE
053274,000277:
053275,000278: # INPUT
053276,000279: # INPUT AVAILABLE FROM LAUNCH DATA AZO REVS B-0
053277,000280: # TEPHEM CSEC B-42
053278,000281: # 6-7D= TIME CSEC B-28
053279,000282:
053280,000283: # OUTPUT
053281,000284: # MMATRIX= 3X3 M MATRIX B-1 (STORED IN VAC AREA)
053282,000285:
053283,000286: 26,3567 40220 EARTHMX STQ SETPD # SET 8-9D=AZO
053284,000287: 26,3570 00051 EARTHMXX
053285,000288: 26,3571 00011 8D # 10-11D=WEARTH
053286,000289: 26,3572 77770 AXT,1 # FOR SL 5, AND SL 10 IN NEWANGLE
053287,000290: 26,3573 00000 0
053288,000291: 26,3574 65345 DLOAD PDDL # LEAVING PD SET AT 12D FOR NEWANGLE
053289,000292: 26,3575 15653 AZO
053290,000293: 26,3576 15651 WEARTH
053291,000294: 26,3577 45006 PUSH CALL
053292,000295: 26,3600 55543 NEWANGLE
053293,000296: 26,3601 41401 SETPD PUSH # 18-19D=504AZ
053294,000297: 26,3602 00023 18D # COS(AZ) SIN(AZ) 0
053295,000298: 26,3603 65346 COS PDDL # 20-37D= MMATRIX= -SIN(AZ) COS(AZ) 0 B-1
053296,000299: 26,3604 00023 504AZ # 0 0 1
053297,000300: 26,3605 65356 SIN PDDL
053298,000301: 26,3606 15336 HI6ZEROS
053299,000302: 26,3607 73525 PDDL SIN
053300,000303: 26,3610 00023 504AZ
053301,000304: 26,3611 65276 DCOMP PDDL
053302,000305: 26,3612 00023 504AZ
053303,000306: 26,3613 63346 COS PDVL
053304,000307: 26,3614 15336 HI6ZEROS
053305,000308: 26,3615 41525 PDDL PUSH
053306,000309: 26,3616 15334 HIDPHALF
|
|
Page 1250 |
053308,000311: # ..... EARTHL SUBROUTINE .....
053309,000312: # SUBROUTINE TO COMPUTE L VECTOR FOR EARTH
053310,000313:
053311,000314: # CALLING SEQUENCE
053312,000315: # L CALL
053313,000316: # L+1 EARTHL
053314,000317:
053315,000318: # INPUT
053316,000319: # AXO,AYO SET AT LAUNCH TIME WITH AYO IMMEDIATELY FOLLOWING AXO IN CORE
053317,000320:
053318,000321: # OUTPUT
053319,000322: # -AX
053320,000323: # MPAC= -AY RADIANS B-0
053321,000324: # 0
053322,000325:
053323,000326: 26,3617 71201 EARTHL SETPD DLOAD
053324,000327: 26,3620 00017 14D
053325,000328: 26,3621 15336 HI6ZEROS
053326,000329: 26,3622 65325 PDDL PDDL
053327,000330: 26,3623 01712 -AYO
053328,000331: 26,3624 01714 AXO
053329,000332: 26,3625 55476 DCOMP VDEF
053330,000333: 26,3626 77650 GOTO
053331,000334: 26,3627 00051 EARTHMXX
053332,000335:
|
|
Page 1251 |
053334,000337: # CONSTANTS AND ERASABLE ASSIGNMENTS
053335,000338:
053336,000339: 26,3630 04,3757 1B1 = DP1/2 # 1 SCALED B-1
053337,000340: 26,3630 17775 02052 COSI 2DEC* 9.996417320 E-1 B-1* # COS(5521.5 SEC.)
053338,000341: 26,3632 00333 10374 SINI 2DEC* 2.676579050 E-2 B-1* # SIN(5521.5 SEC.)
053339,000342: 26,3634 0000050 RPREXIT = S1 # R-TO-RP AND RP-TO-R SUBR EXIT
053340,000343: 26,3634 0000051 EARTHMXX = S2 # EARTHMX,MOONMX SUBR. EXITS
053341,000344: 26,3634 504RPR = 0D # 6 REGS R OR RP VECTOR
053342,000345: 26,3634 SINNODI = 8D # 2 SIN(NODI)
053343,000346: 26,3634 DVECTR = 8D # 6 D VECTOR MOON
053344,000347: 26,3634 CVECTR = 8D # 6 C VECTR MOON
053345,000348: 26,3634 504AZ = 18D # 2 AZ
053346,000349: 26,3634 TIMSUBM = 14D # 3 TIME SUB M (MOON) T+T0 IN GETAZ
053347,000350: 26,3634 504LPL = 14D # 6 L OR LP VECTOR
053348,000351: 26,3634 AVECTR = 20D # 6 A VECTOR (MOON)
053349,000352: 26,3634 BVECTR = 26D # 6 B VECTOR (MOON)
053350,000353: 26,3634 MMATRIX = 20D # 18 M MATRIX
053351,000354: 26,3634 COB = 32D # 2 COS(B) B-1
053352,000355: 26,3634 SOB = 34D # 2 SIN(B) B-1
053353,000356: 26,3634 504F = 6D # 2 F (MOON)
053354,000357: 26,3634 77665 42175 NODDOT 2DEC* -1.703706128 E-11 B28* # REVS/CS.
053355,000358: 26,3636 22211 00636 FDOT 2DEC* +4.253263471 E-9 B27* # REVS/CS.
053356,000359: 26,3640 77777 77767 BDOT 2DEC* -1.145531390 E-16 B28* # REVS/CS.
053357,000360: 26,3642 34076 30363 NODIO 2DEC* +8.788308600 E-1 B # REV.
053358,000361: 26,3644 24760 00133 FSUBO 2DEC* +6.552737750 E-1 B # REV.
053359,000362: 26,3646 02052 35250 BSUBO 2DEC* +6.511941688 E-2 B # REV.
053360,000363: 26,3650 37116 32631 WEARTH 2DEC* +1.160576171 E-7 B23* # REV/CS.
053361,000364: 26,3652 30576 10326 AZO 2DEC* +7.733314844 E-1 B # REVS.
End of include-file PLANETARY_INERTIAL_ORIENTATION.agc. Parent file is MAIN.agc