Source Code
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These source-code files are part of a reconstructed copy of Comanche 72, the
first release of the Apollo Guidance Computer (AGC) Command Module (CM) software
for Apollo 13.
They have been adapted from sources files created from a listing of Comanche 55.
These source files were updated to match binary dumps of a set of Comanche 67 rope modules.
They were then further modified by applying known changes between Comanche 67 and Comanche 72.
A binary dump of module B2 of Comanche 72, part number 2010802-021, was also used
to validate changes made to banks 05-13. The resulting code assembles to have identical
memory-bank checksums as those specified in NASA drawing 2021153G; this gives reasonably
high confidence that the changes that have been made are correct. In places where
ambiguity exists, this ambiguity is discussed in "## Reconstruction:" comments.
Since no contemporary listings of Comanche 72 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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011994,000002: ## Copyright: Public domain.
011995,000003: ## Filename: CSM_GEOMETRY.agc
011996,000004: ## Purpose: A section of Comanche revision 072.
011997,000005: ## It is part of the reconstructed source code for the first
011998,000006: ## release of the software for the Command Module's (CM) Apollo
011999,000007: ## Guidance Computer (AGC) for Apollo 13. No original listings
012000,000008: ## of this program are available; instead, this file was recreated
012001,000009: ## from a printout of Comanche 055, binary dumps of a set of
012002,000010: ## Comanche 067 rope modules, and changelogs between Comanche 067
012003,000011: ## and 072. It has been adapted such that the resulting bugger words
012004,000012: ## exactly match those specified for Comanche 072 in NASA drawing
012005,000013: ## 2021153G, which gives relatively high confidence that the
012006,000014: ## reconstruction is correct.
012007,000015: ## Assembler: yaYUL
012008,000016: ## Contact: Ron Burkey <info@sandroid.org>.
012009,000017: ## Website: www.ibiblio.org/apollo/index.html
012010,000018: ## Mod history: 2024-05-13 MAS Created from Comanche 067.
012011,000019:
012012,000020: 22,2000 BANK 22
012013,000021: 23,2000 SETLOC COMGEOM1
012014,000022: 23,2000 BANK
012015,000023:
012016,000024: # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT
012017,000025: # VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WITH THE SEXTANT LINE OF SIGHT.
012018,000026:
012019,000027: # THE INPUTS ARE 1) THE SEXTANT SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE
012020,000028: # MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR
012021,000029: # JOB VAC AREA.
012022,000030:
012023,000031: # THE OUTPUT IS A HALF-UNIT VECTOR IN NAVIGATION BASE COORDINATES AND STORED AT LOCATION 32D OF THE VAC AREA. THE
012024,000032: # OUTPUT IS ALSO AVAILABLE AT MPAC.
012025,000033:
012026,000034: 23,2000 COUNT 23/GEOM
012027,000035:
012028,000036: 23,2000 47133 SXTNB SLOAD* RTB # PUSHDOWN 00,02,04,(17D-19D),32D-36D
012029,000037: 23,2001 00006 5,1 # TRUNNION = TA
012030,000038: 23,2002 45513 CDULOGIC
012031,000039: 23,2003 41434 RTB PUSH
012032,000040: 23,2004 46027 SXTLOGIC
012033,000041: 23,2005 72556 SIN SL1
012034,000042: 23,2006 66606 PUSH SLOAD* # PD2 = SIN(TA)
012035,000043: 23,2007 00004 3,1 # SHAFT = SA
012036,000044: 23,2010 41434 RTB PUSH # PD4 = SA
012037,000045: 23,2011 45513 CDULOGIC
012038,000046:
012039,000047: 23,2012 41346 COS DMP
012040,000048: 23,2013 00003 2
012041,000049: 23,2014 14041 STODL STARM # COS(SA)SIN(TA)
012042,000050:
012043,000051: 23,2015 41356 SIN DMP
012044,000052: 23,2016 77626 STADR
012045,000053: 23,2017 63734 STODL STARM +2 # SIN(SA)SIN(TA)
012046,000054:
012047,000055: 23,2020 77746 COS
012048,000056: 23,2021 24045 STOVL STARM +4
012049,000057: 23,2022 00041 STARM # STARM = 32D
012050,000058: 23,2023 76521 MXV VSL1
012051,000059: 23,2024 06302 NB1NB2
012052,000060: 23,2025 00041 STORE 32D
012053,000061: 23,2026 77616 RVQ
012054,000062:
012055,000063: 23,2027 32323 SXTLOGIC CAF 10DEGS- # CORRECT FOR 19.775 DEGREE OFFSET
012056,000064: 23,2030 26154 ADS MPAC
012057,000065: 23,2031 35017 CAF QUARTER
012058,000066: 23,2032 07256 TC SHORTMP
012059,000067: 23,2033 06030 TC DANZIG
012060,000068:
012061,000069: # CALCSXA COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-
012062,000070: # OF-SIGHT LIES ALONG THE STAR VECTOR. THE ROUTINE TAKES THE GIVEN STAR VECTOR AND EXPRESSES IT AS A VECTOR REF-
012063,000071: # ERENCED TO THE OPTICS COORDINATE SYSTEM. IN ADDITION IT SETS UP THREE UNIT VECTORS DEFINING THE X, Y, AND Z AXES
012064,000072: # REFERENCED TO THE OPTICS COORDINATE SYSTEM.
012065,000073:
012066,000074: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO PRESENT STABLE MEMBER COORDINATES STORED AT STAR. 2) SAME ANGLE
012067,000075: # INPUT AS *SMNB*, I.E. SINES AND COSINES OF THE CDU ANGLES, IN THE ORDER Y Z X, AT SINCDU AND COSCDU. A CALL
012068,000076: # TO CDUTRIG WILL PROVIDE THIS INPUT.
012069,000077:
012070,000078: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012071,000079: # EQUAL TO ZERO).
012072,000080:
012073,000081: 23,2034 77220 CALCSXA ITA VLOAD # PUSHDOWN 00-26D, 28D, 30D, 32D-36D
012074,000082: 23,2035 00034 28D
012075,000083: 23,2036 02766 STAR
012076,000084: 23,2037 77624 CALL
012077,000085: 23,2040 47646 *SMNB*
012078,000086: 23,2041 76521 MXV VSL1
012079,000087: 23,2042 06260 NB2NB1
012080,000088: 23,2043 26766 STOVL STAR
012081,000089: 23,2044 15332 HIUNITX
012082,000090: 23,2045 26555 STOVL XNB1
012083,000091: 23,2046 15330 HIUNITY
012084,000092: 23,2047 26563 STOVL YNB1
012085,000093: 23,2050 15326 HIUNITZ
012086,000094: 23,2051 36571 STCALL ZNB1
012087,000095: 23,2052 46076 SXTANG1
012088,000096:
012089,000097: # SXTANG COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-OF-
012090,000098: # SIGHT LIES ALONG THE STAR VECTOR.
012091,000099:
012092,000100: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO ANY COORDINATE SYSTEM STORED AT STAR. 2) THE NAVIGATION BASE
012093,000101: # COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STORED AT XNB, YNB,AND
012094,000102: # ZNB.
012095,000103:
012096,000104: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012097,000105: # EQUAL TO ZERO).
012098,000106:
012099,000107: 23,2053 47020 SXTANG ITA RTB # PUSHDOWN 16D,18D,22D-26D,28D
012100,000108: 23,2054 00034 28D
012101,000109: 23,2055 45662 TRANSP1 # EREF WRT NB2
012102,000110: 23,2056 64375 VLOAD MXV
012103,000111: 23,2057 02714 XNB
012104,000112: 23,2060 06260 NB2NB1
012105,000113: 23,2061 77772 VSL1
012106,000114: 23,2062 26555 STOVL XNB1
012107,000115: 23,2063 02722 YNB
012108,000116: 23,2064 76521 MXV VSL1
012109,000117: 23,2065 06260 NB2NB1
012110,000118: 23,2066 26563 STOVL YNB1
012111,000119: 23,2067 02730 ZNB
012112,000120: 23,2070 76521 MXV VSL1
012113,000121: 23,2071 06260 NB2NB1
012114,000122: 23,2072 02571 STORE ZNB1
012115,000123:
012116,000124: 23,2073 47034 RTB RTB
012117,000125: 23,2074 45662 TRANSP1
012118,000126: 23,2075 45676 TRANSP2
012119,000127:
012120,000128: 23,2076 47375 SXTANG1 VLOAD VXV
012121,000129: 23,2077 02571 ZNB1
012122,000130: 23,2100 02766 STAR
012123,000131: 23,2101 77600 BOV
012124,000132: 23,2102 46103 +1
012125,000133: 23,2103 40056 UNIT BOV
012126,000134: 23,2104 46145 ZNB=S1
012127,000135: 23,2105 00027 STORE PDA # PDA = UNIT(ZNB X S)
012128,000136:
012129,000137: 23,2106 57441 DOT DCOMP
012130,000138: 23,2107 02555 XNB1
012131,000139: 23,2110 24023 STOVL SINTH # SIN(SA) = PDA . -XNB
012132,000140: 23,2111 00027 PDA
012133,000141:
012134,000142: 23,2112 77641 DOT
012135,000143: 23,2113 02563 YNB1
012136,000144: 23,2114 34021 STCALL COSTH # COS(SA) = PDA . YNB
012137,000145: 23,2115 47260 ARCTRIG
012138,000146: 23,2116 77634 RTB
012139,000147: 23,2117 45546 1STO2S
012140,000148: 23,2120 26774 STOVL SAC
012141,000149: 23,2121 02766 STAR
012142,000150: 23,2122 77600 BOV
012143,000151: 23,2123 46124 +1
012144,000152: 23,2124 72441 DOT SL1
012145,000153: 23,2125 02571 ZNB1
012146,000154: 23,2126 77726 ACOS
012147,000155: 23,2127 62440 BMN SL2
012148,000156: 23,2130 46142 SXTALARM # TRUNNION ANGLE NEGATIVE
012149,000157: 23,2131 45200 BOV DSU
012150,000158: 23,2132 46142 SXTALARM # TRUNNION ANGLE GREATER THAN 90 DEGREES
012151,000159: 23,2133 06331 20DEG-
012152,000160: 23,2134 77634 RTB
012153,000161: 23,2135 45546 1STO2S
012154,000162: 23,2136 02776 STORE PAC # FOR FLIGHT USE, CULTFLAG IS ON IF
012155,000163: 23,2137 77614 CLRGO # TRUNION IS GREATER THAN 90 DEG
012156,000164: 23,2140 01630 CULTFLAG
012157,000165: 23,2141 00034 28D
012158,000166: 23,2142 77614 SXTALARM SETGO # ALARM HAS BEEN REMOVED FROM THIS
012159,000167: 23,2143 01430 CULTFLAG
012160,000168: 23,2144 00034 28D # SUBROUTINE, ALARM WILL BE SET BY MPI
012161,000169: 23,2145 77745 ZNB=S1 DLOAD
012162,000170: 23,2146 06325 270DEG
012163,000171: 23,2147 16774 STODL SAC
012164,000172: 23,2150 06327 20DEGS-
012165,000173: 23,2151 02776 STORE PAC
012166,000174: 23,2152 77614 CLRGO
012167,000175: 23,2153 01630 CULTFLAG
012168,000176: 23,2154 00034 28D
012169,000177:
012170,000178: # THESE TWO ROUTINES COMPUTE THE ACTUAL STATE VECTOR FOR LM, CSM BY ADDING
012171,000179: # THE CONIC R,V AND THE DEVIATIONS R,V. THE STATE VECTORS ARE CONVERTED TO
012172,000180: # METERS B-29 AND METERS/CSEC B-7 AND STORED APPROPRIATELY IN RN,VN OR
012173,000181: # R-OTHER, V-OTHER FOR DOWNLINK. THE ROUTINES NAMES ARE SWITCHED IN THE
012174,000182: # OTHER VEHICLES COMPUTER.
012175,000183:
012176,000184: # INPUT
012177,000185: # STATE VECTOR IN TEMPORARY STORAGE AREA
012178,000186: # IF STATE VECTOR IS SCALED POS B27 AND VEL B5
012179,000187: # SET X2 TO +2
012180,000188: # IF STATE VECTOR IS SCALED POS B29 AND VEL B7
012181,000189: # SET X2 TO 0
012182,000190:
012183,000191: # OUTPUT
012184,000192: # R(T) IN RN, V(T) IN VN, T IN PIPTIME
012185,000193: # OR
012186,000194: # R(T) IN R-OTHER, V(T) IN V-OTHER (T IS DEFINED BY T-OTHER)
012187,000195:
012188,000196: 23,2155 BANK 23
012189,000197: 10,2000 SETLOC COMGEOM2
012190,000198: 10,2000 BANK
012191,000199: 10,2237 COUNT 10/GEOM
012192,000200: 10,2237 43414 SVDWN1 BOF RVQ # SW=1=AVETOMID DOING W-MATRIX INTEG
012193,000201: 10,2240 04756 AVEMIDSW
012194,000202: 10,2241 20242 +1
012195,000203: 10,2242 53775 VLOAD VSL*
012196,000204: 10,2243 01521 TDELTAV
012197,000205: 10,2244 57605 0 -7,2
012198,000206: 10,2245 53655 VAD VSL*
012199,000207: 10,2246 01535 RCV
012200,000208: 10,2247 57576 0,2
012201,000209: 10,2250 25171 STOVL RN
012202,000210: 10,2251 01527 TNUV
012203,000211: 10,2252 53257 VSL* VAD
012204,000212: 10,2253 57602 0 -4,2
012205,000213: 10,2254 01543 VCV
012206,000214: 10,2255 77657 VSL*
012207,000215: 10,2256 57576 0,2
012208,000216: 10,2257 15177 STODL VN
012209,000217: 10,2260 01517 TET
012210,000218: 10,2261 01205 STORE PIPTIME
012211,000219: 10,2262 77616 RVQ
012212,000220:
012213,000221: 10,2263 53775 SVDWN2 VLOAD VSL*
012214,000222: 10,2264 01521 TDELTAV
012215,000223: 10,2265 57605 0 -7,2
012216,000224: 10,2266 53655 VAD VSL*
012217,000225: 10,2267 01535 RCV
012218,000226: 10,2270 57576 0,2
012219,000227: 10,2271 25722 STOVL R-OTHER
012220,000228: 10,2272 01527 TNUV
012221,000229: 10,2273 53257 VSL* VAD
012222,000230: 10,2274 57602 0 -4,2
012223,000231: 10,2275 01543 VCV
012224,000232: 10,2276 77657 VSL*
012225,000233: 10,2277 57576 0,2
012226,000234: 10,2300 01730 STORE V-OTHER
012227,000235: 10,2301 77616 RVQ
012228,000236:
012229,000237: # SUBROUTINE TO COMPUTE THE NATURAL LOG OF C(MPAC, MPAC +1).
012230,000238:
012231,000239: # ENTRY: CALL
012232,000240: # LOG
012233,000241:
012234,000242: # SUBROUTINE RETURNS WITH -LOG IN DP MPAC.
012235,000243:
012236,000244: # EBANK IS ARBITRARY..
012237,000245:
012238,000246: 14,2000 BANK 14
012239,000247: 23,2000 SETLOC POWFLIT2
012240,000248: 23,2000 BANK
012241,000249: 23,2155 COUNT 23/GEOM
012242,000250:
012243,000251: 23,2155 44301 LOG NORM BDSU # GENERATES LOG BY SHIFTING ARG
012244,000252: 23,2156 00160 MPAC +3 # UNTIL IT LIES BETWEEN .5 AND 1.
012245,000253: 23,2157 06212 NEARLY1 # THE LOG OF THIS PART IS FOUND AND THE
012246,000254: 23,2160 77776 EXIT # LOG OF THE SHIFTED PART IS COMPUTED
012247,000255: 23,2161 07171 TC POLY # AND ADDED IN. SHIFT COUNT STORED
012248,000256: 23,2162 00002 DEC 2 B-14 # (N-1, SUPPLIED BY SMERZH)
012249,000257: 23,2163 00000 00000 2DEC 0 B-28 # IN MPAC +3.
012250,000258: 23,2165 01001 14636 2DEC .031335467
012251,000259: 23,2167 00325 07310 2DEC .0130145859
012252,000260: 23,2171 00541 16735 2DEC .0215738898
012253,000261:
012254,000262: 23,2173 35035 CAF ZERO
012255,000263: 23,2174 54156 TS MPAC +2
012256,000264: 23,2175 00006 EXTEND
012257,000265: 23,2176 32214 DCA CLOG2/32
012258,000266: 23,2177 52155 DXCH MPAC
012259,000267: 23,2200 52160 DXCH MPAC +3
012260,000268: 23,2201 40000 COM # LOAD POSITIVE SHIFT COUNT IN A.
012261,000269: 23,2202 07256 TC SHORTMP # MULTIPLY BY SHIFT COUNT.
012262,000270:
012263,000271: 23,2203 52156 DXCH MPAC +1
012264,000272: 23,2204 52155 DXCH MPAC
012265,000273: 23,2205 52160 DXCH MPAC +3
012266,000274: 23,2206 20155 DAS MPAC
012267,000275: 23,2207 06006 TC INTPRET # RESULT IN MPAC, MPAC +1
012268,000276:
012269,000277: 23,2210 77616 RVQ
012270,000278:
012271,000279: 23,2211 37777 37777 NEARLY1 2DEC .999999999
012272,000280:
012273,000281: 23,2213 00542 34414 CLOG2/32 2DEC .0216608494
012274,000282:
012275,000283: # SUBROUTINE NAME: EARTH ROTATOR (EARROT1 OR EARROT2) DATE: 15 FEB 67
012276,000284: # MOD NO: N +1 LOG SECTION: POWERED FLIGHT SUBROS
012277,000285: # MOD BY: ENTRY GROUP (BAIRNSFATHER)
012278,000286:
012279,000287: # FUNCTIONAL DESCRIPTION: THIS ROUTINE PROJECTS THE INITIAL EARTH TARGET VECTOR RTINIT AHEAD THROUGH
012280,000288: # THE ESTIMATED TIME OF FLIGHT. INITIAL CALL RESOLVES THE INITIAL TARGET VECTOR RTINIT INTO EASTERLY
012281,000289: # AND NORMAL COMPONENTS RTEAST AND RTNORM. INITIAL AND SUBSEQUENT CALLS ROTATE THIS VECTOR
012282,000290: # ABOUT THE (FULL) UNIT POLAR AXIS UNITW THROUGH THE ANGLE WIE DTEAROT TO OBTAIN THE ROTATED
012283,000291: # TARGET VECTOR RT. ALL VECTORS EXCEPT UNITW ARE HALF UNIT.
012284,000292: # THE EQUATIONS ARE
012285,000293: # - - - -
012286,000294: # RT = RTINIT + RTNORM (COS(WT) - 1) + RTEAST SIN(WT)
012287,000295:
012288,000296: # WHERE WT = WIE DTEAROT
012289,000297:
012290,000298: # RTINIT = INITIAL TARGET VECTOR
012291,000299: # - - -
012292,000300: # RTEAST = UNITW * RTINIT
012293,000301: # - - -
012294,000302: # RTNORM = RTEAST * UNITW
012295,000303:
012296,000304: # FOR CONTINUOUS UPDATING, ONLY ONE ENTRY TO EARROT1 IS REQUIRED, WITH SUBSEQUENT ENTRIES AT EARROT2.
012297,000305: #
012298,000306: # CALLING SEQUENCE: FIRST CALL SUBSEQUENT CALL
012299,000307: # STCALL DTEAROT STCALL DTEAROT
012300,000308: # EARROT1 EARROT2
012301,000309: # C(MPAC) UNSPECIFIED C(MPAC) = DTEAROT
012302,000310: # PUSHLOC = PDL+0, ARBITRARY. 6 LOCATIONS USED.
012303,000311:
012304,000312: # SUBROUTINES USED: NONE
012305,000313:
012306,000314: # NORMAL EXIT MODES: RVQ
012307,000315:
012308,000316: # ALARMS: NONE
012309,000317:
012310,000318: # OUTPUT: RTEAST (-1) .5 UNIT VECTOR EAST, COMPNT OF RTINIT LEFT BY FIRST CALL
012311,000319: # RTNORM (-1) .5 UNIT VECTOR NORML, COMPNT OF RTINIT LEFT BY FIRST CALL
012312,000320: # RT (-1) .5 UNIT TARGET VECTOR, ROTATED LEFT BY ALL CALLS
012313,000321: # DTEAROT (-28) CS MAY BE CHANGED BY EARROT2, IF OVER 1 DAY
012314,000322:
012315,000323: # ERASABLE INITIALIZATION REQUIRED:
012316,000324: # UNITW (0) UNIT POLAR VECTOR PAD LOADED
012317,000325: # RTINIT (-1) .5 UNIT INITIAL TARGET VECTOR LEFT BY ENTRY
012318,000326: # DTEAROT (-28) CS TIME OF FLIGHT LEFT BY CALLER
012319,000327:
012320,000328: # DEBRIS: QPRET, PDL+0 ... PDL+5
012321,000329: 23,2215 E7,1451 EBANK= RTINIT
012322,000330:
012323,000331: 23,2215 47375 EARROT1 VLOAD VXV
012324,000332: 23,2216 01714 UNITW # FULL UNIT VECTOR
012325,000333: 23,2217 03452 RTINIT # .5 UNIT
012326,000334: 23,2220 03460 STORE RTEAST # .5 UNIT
012327,000335:
012328,000336: 23,2221 77635 VXV
012329,000337: 23,2222 01714 UNITW # FULL UNIT
012330,000338: 23,2223 17466 STODL RTNORM # .5 UNIT
012331,000339: 23,2224 03606 DTEAROT # (-28) CS
012332,000340:
012333,000341: 23,2225 56204 EARROT2 BOVB DDV
012334,000342: 23,2226 57353 TCDANZIG # RESET OVFIND, IF ON
012335,000343: 23,2227 06256 1/WIE
012336,000344: 23,2230 41400 BOV PUSH
012337,000345: 23,2231 46245 OVERADAY
012338,000346: 23,2232 45346 COS DSU
012339,000347: 23,2233 15332 HIDPHALF
012340,000348: 23,2234 65361 VXSC PDDL # XCH W PUSH LIST
012341,000349: 23,2235 03466 RTNORM # .5 UNIT
012342,000350: 23,2236 74356 SIN VXSC
012343,000351: 23,2237 03460 RTEAST # .5 UNIT
012344,000352: 23,2240 76455 VAD VSL1
012345,000353: 23,2241 53455 VAD UNIT # INSURE THAT RT IS 'UNIT'.
012346,000354: 23,2242 03452 RTINIT # .5 UNIT
012347,000355: 23,2243 03474 STORE RT # .5 UNIT TARGET VECTOR
012348,000356:
012349,000357: 23,2244 77616 RVQ
012350,000358:
012351,000359: 23,2245 75345 OVERADAY DLOAD SIGN
012352,000360: 23,2246 06256 1/WIE
012353,000361: 23,2247 03606 DTEAROT
012354,000362: 23,2250 77621 BDSU
012355,000363: 23,2251 03606 DTEAROT
012356,000364: 23,2252 03606 STORE DTEAROT
012357,000365:
012358,000366: 23,2253 77650 GOTO
012359,000367: 23,2254 46225 EARROT2
012360,000368:
012361,000369: # WIE 2DEC .1901487997
012362,000370: 23,2255 01015 34732 1/WIE 2DEC 8616410 B-28
012363,000371: 23,2257 15373 11346 NB2NB1 2DEC +.8431756920 B-1
012364,000372: 23,2261 00000 00000 2DEC 0 B-28
012365,000373: 23,2263 67313 65307 2DEC -.5376381241 B-1
012366,000374: 23,2265 00000 00000 ZERINFLT 2DEC 0 B-28
012367,000375: 23,2267 20000 00000 HALFNFLT 2DEC .5
012368,000376: 23,2271 00000 00000 2DEC 0 B-28
012369,000377: 23,2273 10464 12470 2DEC +.5376381241 B-1
012370,000378: 23,2275 00000 00000 2DEC 0 B-28
012371,000379: 23,2277 15373 11346 2DEC +.8431756920 B-1
012372,000380: 23,2301 15373 11346 NB1NB2 2DEC +.8431756920 B-1
012373,000381: 23,2303 00000 00000 2DEC 0 B-28
012374,000382: 23,2305 10464 12470 2DEC +.5376381241 B-1
012375,000383: 23,2307 00000 00000 2DEC 0 B-28
012376,000384: 23,2311 20000 00000 2DEC .5
012377,000385: 23,2313 00000 00000 2DEC 0 B-28
012378,000386: 23,2315 67313 65307 2DEC -.5376381241 B-1
012379,000387: 23,2317 00000 00000 2DEC 0 B-28
012380,000388: 23,2321 15373 11346 2DEC +.8431756920 B-1
012381,000389: 23,2323 07020 10DEGS- DEC 3600 B-14
012382,000390: 23,2324 60000 270DEG OCT 60000 # SHAFT 270 DEGREES 2S COMP.
012383,000391: 23,2325 00000 OCT 00000
012384,000392: 23,2326 61740 20DEGS- DEC -07199 B-14
012385,000393: 23,2327 77777 DEC -00000 B-14
012386,000394: 23,2330 07020 20DEG- DEC 03600 B-14
012387,000395: 23,2331 00000 DEC 00000 B-14
012388,000396:
End of include-file CSM_GEOMETRY.agc. Parent file is MAIN.agc