Source Code
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These source-code files are part of a reconstructed copy of Comanche 67, the
Apollo Guidance Computer (AGC) Command Module (CM) software for Apollo 12.
They have been adapted from sources files for Comanche 55, and updated via
disassembly of binary dumps of original core rope memory modules, part numbers
2003972-1081, 2003972-1091, 2003972-1111, 2003972-1121, 2003972-1131, and 2003972-1141.
Since only binary dumps (rather than listings) of Comanche 67 are available as source material,
all comments and labels are approximate.
They have been taken from other AGC programs where possible, or, in some places, written
from scratch to match what we believe would have been in the original listing.
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011887,000002: ## Copyright: Public domain.
011888,000003: ## Filename: CSM_GEOMETRY.agc
011889,000004: ## Purpose: A section of Comanche revision 067.
011890,000005: ## It is part of the reconstructed source code for the flight
011891,000006: ## software for the Command Module's (CM) Apollo Guidance Computer
011892,000007: ## (AGC) for Apollo 12. No original listings of this program are
011893,000008: ## available; instead, this file was created via dissassembly of
011894,000009: ## dumps of Comanche 067 core rope modules and comparison with
011895,000010: ## other AGC programs.
011896,000011: ## Assembler: yaYUL
011897,000012: ## Contact: Ron Burkey <info@sandroid.org>.
011898,000013: ## Website: www.ibiblio.org/apollo/index.html
011899,000014: ## Mod history: 2023-08-16 MAS Created from Comanche 055.
011900,000015:
011901,000016: 22,2000 BANK 22
011902,000017: 23,2000 SETLOC COMGEOM1
011903,000018: 23,2000 BANK
011904,000019:
011905,000020: # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT
011906,000021: # VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WITH THE SEXTANT LINE OF SIGHT.
011907,000022:
011908,000023: # THE INPUTS ARE 1) THE SEXTANT SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE
011909,000024: # MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR
011910,000025: # JOB VAC AREA.
011911,000026:
011912,000027: # THE OUTPUT IS A HALF-UNIT VECTOR IN NAVIGATION BASE COORDINATES AND STORED AT LOCATION 32D OF THE VAC AREA. THE
011913,000028: # OUTPUT IS ALSO AVAILABLE AT MPAC.
011914,000029:
011915,000030: 23,2000 COUNT 23/GEOM
011916,000031:
011917,000032: 23,2000 47133 SXTNB SLOAD* RTB # PUSHDOWN 00,02,04,(17D-19D),32D-36D
011918,000033: 23,2001 00006 5,1 # TRUNNION = TA
011919,000034: 23,2002 45513 CDULOGIC
011920,000035: 23,2003 41434 RTB PUSH
011921,000036: 23,2004 46027 SXTLOGIC
011922,000037: 23,2005 72556 SIN SL1
011923,000038: 23,2006 66606 PUSH SLOAD* # PD2 = SIN(TA)
011924,000039: 23,2007 00004 3,1 # SHAFT = SA
011925,000040: 23,2010 41434 RTB PUSH # PD4 = SA
011926,000041: 23,2011 45513 CDULOGIC
011927,000042:
011928,000043: 23,2012 41346 COS DMP
011929,000044: 23,2013 00003 2
011930,000045: 23,2014 14041 STODL STARM # COS(SA)SIN(TA)
011931,000046:
011932,000047: 23,2015 41356 SIN DMP
011933,000048: 23,2016 77626 STADR
011934,000049: 23,2017 63734 STODL STARM +2 # SIN(SA)SIN(TA)
011935,000050:
011936,000051: 23,2020 77746 COS
011937,000052: 23,2021 24045 STOVL STARM +4
011938,000053: 23,2022 00041 STARM # STARM = 32D
011939,000054: 23,2023 76521 MXV VSL1
011940,000055: 23,2024 06302 NB1NB2
011941,000056: 23,2025 00041 STORE 32D
011942,000057: 23,2026 77616 RVQ
011943,000058:
011944,000059: 23,2027 32323 SXTLOGIC CAF 10DEGS- # CORRECT FOR 19.775 DEGREE OFFSET
011945,000060: 23,2030 26154 ADS MPAC
011946,000061: 23,2031 35017 CAF QUARTER
011947,000062: 23,2032 07256 TC SHORTMP
011948,000063: 23,2033 06030 TC DANZIG
011949,000064:
011950,000065: # CALCSXA COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-
011951,000066: # OF-SIGHT LIES ALONG THE STAR VECTOR. THE ROUTINE TAKES THE GIVEN STAR VECTOR AND EXPRESSES IT AS A VECTOR REF-
011952,000067: # ERENCED TO THE OPTICS COORDINATE SYSTEM. IN ADDITION IT SETS UP THREE UNIT VECTORS DEFINING THE X, Y, AND Z AXES
011953,000068: # REFERENCED TO THE OPTICS COORDINATE SYSTEM.
011954,000069:
011955,000070: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO PRESENT STABLE MEMBER COORDINATES STORED AT STAR. 2) SAME ANGLE
011956,000071: # INPUT AS *SMNB*, I.E. SINES AND COSINES OF THE CDU ANGLES, IN THE ORDER Y Z X, AT SINCDU AND COSCDU. A CALL
011957,000072: # TO CDUTRIG WILL PROVIDE THIS INPUT.
011958,000073:
011959,000074: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
011960,000075: # EQUAL TO ZERO).
011961,000076:
011962,000077: 23,2034 77220 CALCSXA ITA VLOAD # PUSHDOWN 00-26D, 28D, 30D, 32D-36D
011963,000078: 23,2035 00034 28D
011964,000079: 23,2036 02766 STAR
011965,000080: 23,2037 77624 CALL
011966,000081: 23,2040 47646 *SMNB*
011967,000082: 23,2041 76521 MXV VSL1
011968,000083: 23,2042 06260 NB2NB1
011969,000084: 23,2043 26766 STOVL STAR
011970,000085: 23,2044 15332 HIUNITX
011971,000086: 23,2045 26555 STOVL XNB1
011972,000087: 23,2046 15330 HIUNITY
011973,000088: 23,2047 26563 STOVL YNB1
011974,000089: 23,2050 15326 HIUNITZ
011975,000090: 23,2051 36571 STCALL ZNB1
011976,000091: 23,2052 46076 SXTANG1
011977,000092:
011978,000093: # SXTANG COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-OF-
011979,000094: # SIGHT LIES ALONG THE STAR VECTOR.
011980,000095:
011981,000096: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO ANY COORDINATE SYSTEM STORED AT STAR. 2) THE NAVIGATION BASE
011982,000097: # COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STORED AT XNB, YNB,AND
011983,000098: # ZNB.
011984,000099:
011985,000100: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
011986,000101: # EQUAL TO ZERO).
011987,000102:
011988,000103: 23,2053 47020 SXTANG ITA RTB # PUSHDOWN 16D,18D,22D-26D,28D
011989,000104: 23,2054 00034 28D
011990,000105: 23,2055 45662 TRANSP1 # EREF WRT NB2
011991,000106: 23,2056 64375 VLOAD MXV
011992,000107: 23,2057 02714 XNB
011993,000108: 23,2060 06260 NB2NB1
011994,000109: 23,2061 77772 VSL1
011995,000110: 23,2062 26555 STOVL XNB1
011996,000111: 23,2063 02722 YNB
011997,000112: 23,2064 76521 MXV VSL1
011998,000113: 23,2065 06260 NB2NB1
011999,000114: 23,2066 26563 STOVL YNB1
012000,000115: 23,2067 02730 ZNB
012001,000116: 23,2070 76521 MXV VSL1
012002,000117: 23,2071 06260 NB2NB1
012003,000118: 23,2072 02571 STORE ZNB1
012004,000119:
012005,000120: 23,2073 47034 RTB RTB
012006,000121: 23,2074 45662 TRANSP1
012007,000122: 23,2075 45676 TRANSP2
012008,000123:
012009,000124: 23,2076 47375 SXTANG1 VLOAD VXV
012010,000125: 23,2077 02571 ZNB1
012011,000126: 23,2100 02766 STAR
012012,000127: 23,2101 77600 BOV
012013,000128: 23,2102 46103 +1
012014,000129: 23,2103 40056 UNIT BOV
012015,000130: 23,2104 46145 ZNB=S1
012016,000131: 23,2105 00027 STORE PDA # PDA = UNIT(ZNB X S)
012017,000132:
012018,000133: 23,2106 57441 DOT DCOMP
012019,000134: 23,2107 02555 XNB1
012020,000135: 23,2110 24023 STOVL SINTH # SIN(SA) = PDA . -XNB
012021,000136: 23,2111 00027 PDA
012022,000137:
012023,000138: 23,2112 77641 DOT
012024,000139: 23,2113 02563 YNB1
012025,000140: 23,2114 34021 STCALL COSTH # COS(SA) = PDA . YNB
012026,000141: 23,2115 47260 ARCTRIG
012027,000142: 23,2116 77634 RTB
012028,000143: 23,2117 45546 1STO2S
012029,000144: 23,2120 26774 STOVL SAC
012030,000145: 23,2121 02766 STAR
012031,000146: 23,2122 77600 BOV
012032,000147: 23,2123 46124 +1
012033,000148: 23,2124 72441 DOT SL1
012034,000149: 23,2125 02571 ZNB1
012035,000150: 23,2126 77726 ACOS
012036,000151: 23,2127 62440 BMN SL2
012037,000152: 23,2130 46142 SXTALARM # TRUNNION ANGLE NEGATIVE
012038,000153: 23,2131 45200 BOV DSU
012039,000154: 23,2132 46142 SXTALARM # TRUNNION ANGLE GREATER THAN 90 DEGREES
012040,000155: 23,2133 06331 20DEG-
012041,000156: 23,2134 77634 RTB
012042,000157: 23,2135 45546 1STO2S
012043,000158: 23,2136 02776 STORE PAC # FOR FLIGHT USE, CULTFLAG IS ON IF
012044,000159: 23,2137 77614 CLRGO # TRUNION IS GREATER THAN 90 DEG
012045,000160: 23,2140 01630 CULTFLAG
012046,000161: 23,2141 00034 28D
012047,000162: 23,2142 77614 SXTALARM SETGO # ALARM HAS BEEN REMOVED FROM THIS
012048,000163: 23,2143 01430 CULTFLAG
012049,000164: 23,2144 00034 28D # SUBROUTINE, ALARM WILL BE SET BY MPI
012050,000165: 23,2145 77745 ZNB=S1 DLOAD
012051,000166: 23,2146 06325 270DEG
012052,000167: 23,2147 16774 STODL SAC
012053,000168: 23,2150 06327 20DEGS-
012054,000169: 23,2151 02776 STORE PAC
012055,000170: 23,2152 77614 CLRGO
012056,000171: 23,2153 01630 CULTFLAG
012057,000172: 23,2154 00034 28D
012058,000173:
012059,000174: # THESE TWO ROUTINES COMPUTE THE ACTUAL STATE VECTOR FOR LM, CSM BY ADDING
012060,000175: # THE CONIC R,V AND THE DEVIATIONS R,V. THE STATE VECTORS ARE CONVERTED TO
012061,000176: # METERS B-29 AND METERS/CSEC B-7 AND STORED APPROPRIATELY IN RN,VN OR
012062,000177: # R-OTHER, V-OTHER FOR DOWNLINK. THE ROUTINES NAMES ARE SWITCHED IN THE
012063,000178: # OTHER VEHICLES COMPUTER.
012064,000179:
012065,000180: # INPUT
012066,000181: # STATE VECTOR IN TEMPORARY STORAGE AREA
012067,000182: # IF STATE VECTOR IS SCALED POS B27 AND VEL B5
012068,000183: # SET X2 TO +2
012069,000184: # IF STATE VECTOR IS SCALED POS B29 AND VEL B7
012070,000185: # SET X2 TO 0
012071,000186:
012072,000187: # OUTPUT
012073,000188: # R(T) IN RN, V(T) IN VN, T IN PIPTIME
012074,000189: # OR
012075,000190: # R(T) IN R-OTHER, V(T) IN V-OTHER (T IS DEFINED BY T-OTHER)
012076,000191:
012077,000192: 23,2155 BANK 23
012078,000193: 10,2000 SETLOC COMGEOM2
012079,000194: 10,2000 BANK
012080,000195: 10,2237 COUNT 10/GEOM
012081,000196: 10,2237 43414 SVDWN1 BOF RVQ # SW=1=AVETOMID DOING W-MATRIX INTEG
012082,000197: 10,2240 04756 AVEMIDSW
012083,000198: 10,2241 20242 +1
012084,000199: 10,2242 53775 VLOAD VSL*
012085,000200: 10,2243 01521 TDELTAV
012086,000201: 10,2244 57605 0 -7,2
012087,000202: 10,2245 53655 VAD VSL*
012088,000203: 10,2246 01535 RCV
012089,000204: 10,2247 57576 0,2
012090,000205: 10,2250 25171 STOVL RN
012091,000206: 10,2251 01527 TNUV
012092,000207: 10,2252 53257 VSL* VAD
012093,000208: 10,2253 57602 0 -4,2
012094,000209: 10,2254 01543 VCV
012095,000210: 10,2255 77657 VSL*
012096,000211: 10,2256 57576 0,2
012097,000212: 10,2257 15177 STODL VN
012098,000213: 10,2260 01517 TET
012099,000214: 10,2261 01205 STORE PIPTIME
012100,000215: 10,2262 77616 RVQ
012101,000216:
012102,000217: 10,2263 53775 SVDWN2 VLOAD VSL*
012103,000218: 10,2264 01521 TDELTAV
012104,000219: 10,2265 57605 0 -7,2
012105,000220: 10,2266 53655 VAD VSL*
012106,000221: 10,2267 01535 RCV
012107,000222: 10,2270 57576 0,2
012108,000223: 10,2271 25722 STOVL R-OTHER
012109,000224: 10,2272 01527 TNUV
012110,000225: 10,2273 53257 VSL* VAD
012111,000226: 10,2274 57602 0 -4,2
012112,000227: 10,2275 01543 VCV
012113,000228: 10,2276 77657 VSL*
012114,000229: 10,2277 57576 0,2
012115,000230: 10,2300 01730 STORE V-OTHER
012116,000231: 10,2301 77616 RVQ
012117,000232:
012118,000233: # SUBROUTINE TO COMPUTE THE NATURAL LOG OF C(MPAC, MPAC +1).
012119,000234:
012120,000235: # ENTRY: CALL
012121,000236: # LOG
012122,000237:
012123,000238: # SUBROUTINE RETURNS WITH -LOG IN DP MPAC.
012124,000239:
012125,000240: # EBANK IS ARBITRARY..
012126,000241:
012127,000242: 14,2000 BANK 14
012128,000243: 23,2000 SETLOC POWFLIT2
012129,000244: 23,2000 BANK
012130,000245: 23,2155 COUNT 23/GEOM
012131,000246:
012132,000247: 23,2155 44301 LOG NORM BDSU # GENERATES LOG BY SHIFTING ARG
012133,000248: 23,2156 00160 MPAC +3 # UNTIL IT LIES BETWEEN .5 AND 1.
012134,000249: 23,2157 06212 NEARLY1 # THE LOG OF THIS PART IS FOUND AND THE
012135,000250: 23,2160 77776 EXIT # LOG OF THE SHIFTED PART IS COMPUTED
012136,000251: 23,2161 07171 TC POLY # AND ADDED IN. SHIFT COUNT STORED
012137,000252: 23,2162 00002 DEC 2 B-14 # (N-1, SUPPLIED BY SMERZH)
012138,000253: 23,2163 00000 00000 2DEC 0 B-28 # IN MPAC +3.
012139,000254: 23,2165 01001 14636 2DEC .031335467
012140,000255: 23,2167 00325 07310 2DEC .0130145859
012141,000256: 23,2171 00541 16735 2DEC .0215738898
012142,000257:
012143,000258: 23,2173 35035 CAF ZERO
012144,000259: 23,2174 54156 TS MPAC +2
012145,000260: 23,2175 00006 EXTEND
012146,000261: 23,2176 32214 DCA CLOG2/32
012147,000262: 23,2177 52155 DXCH MPAC
012148,000263: 23,2200 52160 DXCH MPAC +3
012149,000264: 23,2201 40000 COM # LOAD POSITIVE SHIFT COUNT IN A.
012150,000265: 23,2202 07256 TC SHORTMP # MULTIPLY BY SHIFT COUNT.
012151,000266:
012152,000267: 23,2203 52156 DXCH MPAC +1
012153,000268: 23,2204 52155 DXCH MPAC
012154,000269: 23,2205 52160 DXCH MPAC +3
012155,000270: 23,2206 20155 DAS MPAC
012156,000271: 23,2207 06006 TC INTPRET # RESULT IN MPAC, MPAC +1
012157,000272:
012158,000273: 23,2210 77616 RVQ
012159,000274:
012160,000275: 23,2211 37777 37777 NEARLY1 2DEC .999999999
012161,000276:
012162,000277: 23,2213 00542 34414 CLOG2/32 2DEC .0216608494
012163,000278:
012164,000279: # SUBROUTINE NAME: EARTH ROTATOR (EARROT1 OR EARROT2) DATE: 15 FEB 67
012165,000280: # MOD NO: N +1 LOG SECTION: POWERED FLIGHT SUBROS
012166,000281: # MOD BY: ENTRY GROUP (BAIRNSFATHER)
012167,000282:
012168,000283: # FUNCTIONAL DESCRIPTION: THIS ROUTINE PROJECTS THE INITIAL EARTH TARGET VECTOR RTINIT AHEAD THROUGH
012169,000284: # THE ESTIMATED TIME OF FLIGHT. INITIAL CALL RESOLVES THE INITIAL TARGET VECTOR RTINIT INTO EASTERLY
012170,000285: # AND NORMAL COMPONENTS RTEAST AND RTNORM. INITIAL AND SUBSEQUENT CALLS ROTATE THIS VECTOR
012171,000286: # ABOUT THE (FULL) UNIT POLAR AXIS UNITW THROUGH THE ANGLE WIE DTEAROT TO OBTAIN THE ROTATED
012172,000287: # TARGET VECTOR RT. ALL VECTORS EXCEPT UNITW ARE HALF UNIT.
012173,000288: # THE EQUATIONS ARE
012174,000289: # - - - -
012175,000290: # RT = RTINIT + RTNORM (COS(WT) - 1) + RTEAST SIN(WT)
012176,000291:
012177,000292: # WHERE WT = WIE DTEAROT
012178,000293:
012179,000294: # RTINIT = INITIAL TARGET VECTOR
012180,000295: # - - -
012181,000296: # RTEAST = UNITW * RTINIT
012182,000297: # - - -
012183,000298: # RTNORM = RTEAST * UNITW
012184,000299:
012185,000300: # FOR CONTINUOUS UPDATING, ONLY ONE ENTRY TO EARROT1 IS REQUIRED, WITH SUBSEQUENT ENTRIES AT EARROT2.
012186,000301: #
012187,000302: # CALLING SEQUENCE: FIRST CALL SUBSEQUENT CALL
012188,000303: # STCALL DTEAROT STCALL DTEAROT
012189,000304: # EARROT1 EARROT2
012190,000305: # C(MPAC) UNSPECIFIED C(MPAC) = DTEAROT
012191,000306: # PUSHLOC = PDL+0, ARBITRARY. 6 LOCATIONS USED.
012192,000307:
012193,000308: # SUBROUTINES USED: NONE
012194,000309:
012195,000310: # NORMAL EXIT MODES: RVQ
012196,000311:
012197,000312: # ALARMS: NONE
012198,000313:
012199,000314: # OUTPUT: RTEAST (-1) .5 UNIT VECTOR EAST, COMPNT OF RTINIT LEFT BY FIRST CALL
012200,000315: # RTNORM (-1) .5 UNIT VECTOR NORML, COMPNT OF RTINIT LEFT BY FIRST CALL
012201,000316: # RT (-1) .5 UNIT TARGET VECTOR, ROTATED LEFT BY ALL CALLS
012202,000317: # DTEAROT (-28) CS MAY BE CHANGED BY EARROT2, IF OVER 1 DAY
012203,000318:
012204,000319: # ERASABLE INITIALIZATION REQUIRED:
012205,000320: # UNITW (0) UNIT POLAR VECTOR PAD LOADED
012206,000321: # RTINIT (-1) .5 UNIT INITIAL TARGET VECTOR LEFT BY ENTRY
012207,000322: # DTEAROT (-28) CS TIME OF FLIGHT LEFT BY CALLER
012208,000323:
012209,000324: # DEBRIS: QPRET, PDL+0 ... PDL+5
012210,000325: 23,2215 E7,1451 EBANK= RTINIT
012211,000326:
012212,000327: 23,2215 47375 EARROT1 VLOAD VXV
012213,000328: 23,2216 01714 UNITW # FULL UNIT VECTOR
012214,000329: 23,2217 03452 RTINIT # .5 UNIT
012215,000330: 23,2220 03460 STORE RTEAST # .5 UNIT
012216,000331:
012217,000332: 23,2221 77635 VXV
012218,000333: 23,2222 01714 UNITW # FULL UNIT
012219,000334: 23,2223 17466 STODL RTNORM # .5 UNIT
012220,000335: 23,2224 03606 DTEAROT # (-28) CS
012221,000336:
012222,000337: 23,2225 56204 EARROT2 BOVB DDV
012223,000338: 23,2226 57353 TCDANZIG # RESET OVFIND, IF ON
012224,000339: 23,2227 06256 1/WIE
012225,000340: 23,2230 41400 BOV PUSH
012226,000341: 23,2231 46245 OVERADAY
012227,000342: 23,2232 45346 COS DSU
012228,000343: 23,2233 15332 HIDPHALF
012229,000344: 23,2234 65361 VXSC PDDL # XCH W PUSH LIST
012230,000345: 23,2235 03466 RTNORM # .5 UNIT
012231,000346: 23,2236 74356 SIN VXSC
012232,000347: 23,2237 03460 RTEAST # .5 UNIT
012233,000348: 23,2240 76455 VAD VSL1
012234,000349: 23,2241 53455 VAD UNIT # INSURE THAT RT IS 'UNIT'.
012235,000350: 23,2242 03452 RTINIT # .5 UNIT
012236,000351: 23,2243 03474 STORE RT # .5 UNIT TARGET VECTOR
012237,000352:
012238,000353: 23,2244 77616 RVQ
012239,000354:
012240,000355: 23,2245 75345 OVERADAY DLOAD SIGN
012241,000356: 23,2246 06256 1/WIE
012242,000357: 23,2247 03606 DTEAROT
012243,000358: 23,2250 77621 BDSU
012244,000359: 23,2251 03606 DTEAROT
012245,000360: 23,2252 03606 STORE DTEAROT
012246,000361:
012247,000362: 23,2253 77650 GOTO
012248,000363: 23,2254 46225 EARROT2
012249,000364:
012250,000365: # WIE 2DEC .1901487997
012251,000366: 23,2255 01015 34732 1/WIE 2DEC 8616410 B-28
012252,000367: 23,2257 15373 11346 NB2NB1 2DEC +.8431756920 B-1
012253,000368: 23,2261 00000 00000 2DEC 0 B-28
012254,000369: 23,2263 67313 65307 2DEC -.5376381241 B-1
012255,000370: 23,2265 00000 00000 ZERINFLT 2DEC 0 B-28
012256,000371: 23,2267 20000 00000 HALFNFLT 2DEC .5
012257,000372: 23,2271 00000 00000 2DEC 0 B-28
012258,000373: 23,2273 10464 12470 2DEC +.5376381241 B-1
012259,000374: 23,2275 00000 00000 2DEC 0 B-28
012260,000375: 23,2277 15373 11346 2DEC +.8431756920 B-1
012261,000376: 23,2301 15373 11346 NB1NB2 2DEC +.8431756920 B-1
012262,000377: 23,2303 00000 00000 2DEC 0 B-28
012263,000378: 23,2305 10464 12470 2DEC +.5376381241 B-1
012264,000379: 23,2307 00000 00000 2DEC 0 B-28
012265,000380: 23,2311 20000 00000 2DEC .5
012266,000381: 23,2313 00000 00000 2DEC 0 B-28
012267,000382: 23,2315 67313 65307 2DEC -.5376381241 B-1
012268,000383: 23,2317 00000 00000 2DEC 0 B-28
012269,000384: 23,2321 15373 11346 2DEC +.8431756920 B-1
012270,000385: 23,2323 07020 10DEGS- DEC 3600 B-14
012271,000386: 23,2324 60000 270DEG OCT 60000 # SHAFT 270 DEGREES 2S COMP.
012272,000387: 23,2325 00000 OCT 00000
012273,000388: 23,2326 61740 20DEGS- DEC -07199 B-14
012274,000389: 23,2327 77777 DEC -00000 B-14
012275,000390: 23,2330 07020 20DEG- DEC 03600 B-14
012276,000391: 23,2331 00000 DEC 00000 B-14
012277,000392:
End of include-file CSM_GEOMETRY.agc. Parent file is MAIN.agc