Source Code
012056,000001: # Copyright: Public domain.
012057,000002: # Filename: CSM_GEOMETRY.agc
012058,000003: # Purpose: Part of the source code for Colossus, build 249.
012059,000004: # It is part of the source code for the Command Module's (CM)
012060,000005: # Apollo Guidance Computer (AGC), possibly for Apollo 8 and 9.
012061,000006: # Assembler: yaYUL
012062,000007: # Reference: pp. 282-293 of 1701.pdf.
012063,000008: # Contact: Ron Burkey <info@sandroid.org>.
012064,000009: # Website: www.ibiblio.org/apollo.
012065,000010: # Mod history: 08/08/04 RSB. Began transcribing.
012066,000011:
012067,000012: # The contents of the "Colossus249" files, in general, are transcribed
012068,000013: # from a scanned document obtained from MIT's website,
012069,000014: # http://hrst.mit.edu/hrs/apollo/public/archive/1701.pdf. Notations on this
012070,000015: # document read, in part:
012071,000016:
012072,000017: # Assemble revision 249 of AGC program Colossus by NASA
012073,000018: # 2021111-041. October 28, 1968.
012074,000019:
012075,000020: # This AGC program shall also be referred to as
012076,000021: # Colossus 1A
012077,000022:
012078,000023: # Prepared by
012079,000024: # Massachusetts Institute of Technology
012080,000025: # 75 Cambridge Parkway
012081,000026: # Cambridge, Massachusetts
012082,000027: # under NASA contract NAS 9-4065.
012083,000028:
012084,000029: # Refer directly to the online document mentioned above for further information.
012085,000030: # Please report any errors (relative to 1701.pdf) to info@sandroid.org.
012086,000031:
012087,000032: # In some cases, where the source code for Luminary 131 overlaps that of
012088,000033: # Colossus 249, this code is instead copied from the corresponding Luminary 131
012089,000034: # source file, and then is proofed to incorporate any changes.
012090,000035:
012091,000036: # Page 282
012092,000037: 22,2000 BANK 22
012093,000038: 23,2000 SETLOC COMGEOM1
012094,000039: 23,2000 BANK
012095,000040:
012096,000041: # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT
012097,000042: # VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WTIH THE SEXTAND LINE OF SIGHT.
012098,000043:
012099,000044: # THE INPUTS ARE: 1) THE SEXTAND SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE
012100,000045: # MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR
012101,000046: # JOB VAC AREA.
012102,000047:
012103,000048: # THE OUTPUT IS A HALF-UNIT VECTOR IN NAVIGATION BASE COORDINATES AND STORED AT LOCATION 32D OF THE VAC AREA. THE
012104,000049: # OUTPUT IS ALSO AVAILABLE AT MPAC.
012105,000050:
012106,000051: 23,2000 COUNT 23/GEOM
012107,000052:
012108,000053: 23,2000 47133 SXTNB SLOAD* RTB # PUSHDOWN 00,02,04,(17D-19D),32D-36D
012109,000054: 23,2001 00006 5,1 # TRUNNION = TA
012110,000055: 23,2002 45510 CDULOGIC
012111,000056: 23,2003 41434 RTB PUSH
012112,000057: 23,2004 46027 SXTLOGIC
012113,000058: 23,2005 72556 SIN SL1
012114,000059: 23,2006 66606 PUSH SLOAD* # PD2 = SIN(TA)
012115,000060: 23,2007 00004 3,1 # SHAFT = SA
012116,000061: 23,2010 41434 RTB PUSH # PD4 = SA
012117,000062: 23,2011 45510 CDULOGIC
012118,000063:
012119,000064: 23,2012 41346 COS DMP
012120,000065: 23,2013 00003 2
012121,000066: 23,2014 14041 STODL STARM # COS(SA)SIN(TA)
012122,000067:
012123,000068: 23,2015 41356 SIN DMP
012124,000069: 23,2016 77626 STADR
012125,000070: 23,2017 63734 STODL STARM +2 # SIN(SA)SIN(TA)
012126,000071:
012127,000072: 23,2020 77746 COS
012128,000073: 23,2021 24045 STOVL STARM +4
012129,000074: 23,2022 00041 STARM # STARM = 32D
012130,000075: 23,2023 76521 MXV VSL1
012131,000076: 23,2024 06302 NB1NB2
012132,000077: 23,2025 00041 STORE 32D
012133,000078: 23,2026 77616 RVQ
012134,000079: 23,2027 32323 SXTLOGIC CAF 10DEGS- # CORRECT FOR 19.775 DEGREE OFFSET
012135,000080: 23,2030 26154 ADS MPAC
012136,000081: 23,2031 34676 CAF QUARTER
012137,000082: 23,2032 07256 TC SHORTMP
012138,000083: 23,2033 06030 TC DANZIG
012139,000084:
012140,000085: # Page 283
012141,000086: # CALCSXA COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-
012142,000087: # OF-SIGHT LIES ALONG THE STAR FECTOR. THE ROUTINE TAKES THE GIVEN STAR VECTOR AND EXPRESSES IT AS A VECTOR REF-
012143,000088: # ERENECED TO THE OPTICS COORDINATE SYSTEM. IN ADDITION IT SETS UP THREE UNIT VECTORS DEFINING THE X, Y, AND Z AXES
012144,000089: # REFERENCED TO THE OPTICS COORDINATE SYSTEM.
012145,000090:
012146,000091: # THE INPUTS ARE: 1) THE STAR VECTOR REFERRED TO THE PRESENT STABLE MEMMBER COORDINATES STORED AT STAR. 2) SAME ANGLE
012147,000092: # INPUT AS *SMNB*, I.E., SINES AND COSINES OF THE CDU ANGLES, IN THE ORDER Y Z X, AT SINCDU AND COSCDU. A CALL
012148,000093: # TO CDUTRIG WILL PROVIDE THIS INPUT.
012149,000094:
012150,000095: # THE OUTPUT ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012151,000096: # EQUAL TO ZERO).
012152,000097:
012153,000098: 23,2034 77220 CALCSXA ITA VLOAD # PUSHDOWN 00-26D, 28D, 30D, 32D-36D
012154,000099: 23,2035 00034 28D
012155,000100: 23,2036 02766 STAR
012156,000101: 23,2037 77624 CALL
012157,000102: 23,2040 47577 *SMNB*
012158,000103: 23,2041 76521 MXV VSL1
012159,000104: 23,2042 06260 NB2NB1
012160,000105: 23,2043 26766 STOVL STAR
012161,000106: 23,2044 15330 HIUNITX
012162,000107: 23,2045 26555 STOVL XNB1
012163,000108: 23,2046 15326 HIUNITY
012164,000109: 23,2047 26563 STOVL YNB1
012165,000110: 23,2050 15324 HIUNITZ
012166,000111: 23,2051 36571 STCALL ZNB1
012167,000112: 23,2052 46076 SXTANG1
012168,000113:
012169,000114: # Page 284
012170,000115: # SXTANG COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-OF-
012171,000116: # SIGHT LIES ALONG THE STAR VECTOR.
012172,000117:
012173,000118: # THE INPUTS ARE: 1) THE STAR VECTOR REFERRED TO ANY COORDINATE SYSTEM STORED AT STAR. 2) THE NAVIGATION BASE
012174,000119: # COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STROED AT XNB, YNB,AND
012175,000120: # ZNB.
012176,000121:
012177,000122: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012178,000123: # EQUAL TO ZERO).
012179,000124:
012180,000125: 23,2053 47020 SXTANG ITA RTB # PUSHDOWN 16D,18D,22D-26D,28D
012181,000126: 23,2054 00034 28D
012182,000127: 23,2055 45657 TRANSP1 # EREF WRT NB2
012183,000128: 23,2056 64375 VLOAD MXV
012184,000129: 23,2057 02714 XNB
012185,000130: 23,2060 06260 NB2NB1
012186,000131: 23,2061 77772 VSL1
012187,000132: 23,2062 26555 STOVL XNB1
012188,000133: 23,2063 02722 YNB
012189,000134: 23,2064 76521 MXV VSL1
012190,000135: 23,2065 06260 NB2NB1
012191,000136: 23,2066 26563 STOVL YNB1
012192,000137: 23,2067 02730 ZNB
012193,000138: 23,2070 76521 MXV VSL1
012194,000139: 23,2071 06260 NB2NB1
012195,000140: 23,2072 02571 STORE ZNB1
012196,000141:
012197,000142: 23,2073 47034 RTB RTB
012198,000143: 23,2074 45657 TRANSP1
012199,000144: 23,2075 45673 TRANSP2
012200,000145:
012201,000146: 23,2076 47375 SXTANG1 VLOAD VXV
012202,000147: 23,2077 02571 ZNB1
012203,000148: 23,2100 02766 STAR
012204,000149: 23,2101 77600 BOV
012205,000150: 23,2102 46103 +1
012206,000151: 23,2103 40056 UNIT BOV
012207,000152: 23,2104 46145 ZNB=S1
012208,000153: 23,2105 00027 STORE PDA # PDA = UNIT(ZNB X S)
012209,000154:
012210,000155: 23,2106 57441 DOT DCOMP
012211,000156: 23,2107 02555 XNB1
012212,000157: 23,2110 24023 STOVL SINTH # SIN(SA) = PDA . -XNB
012213,000158: 23,2111 00027 PDA
012214,000159:
012215,000160: 23,2112 77641 DOT
012216,000161: 23,2113 02563 YNB1
012217,000162: 23,2114 34021 STCALL COSTH # COS(SA) = PDA . YNB
012218,000163: 23,2115 47211 ARCTRIG
012219,000164: # Page 285
012220,000165: 23,2116 77634 RTB
012221,000166: 23,2117 45543 1STO2S
012222,000167: 23,2120 26774 STOVL SAC
012223,000168: 23,2121 02766 STAR
012224,000169: 23,2122 77600 BOV
012225,000170: 23,2123 46124 +1
012226,000171: 23,2124 72441 DOT SL1
012227,000172: 23,2125 02571 ZNB1
012228,000173: 23,2126 77726 ACOS
012229,000174: 23,2127 62440 BMN SL2
012230,000175: 23,2130 46142 SXTALARM # TRUNNION ANGLE NEGATIVE
012231,000176: 23,2131 45200 BOV DSU
012232,000177: 23,2132 46142 SXTALARM # TRUNNION ANGLE GREATER THAN 90 DEGREES
012233,000178: 23,2133 06331 20DEG-
012234,000179: 23,2134 77634 RTB
012235,000180: 23,2135 45543 1STO2S
012236,000181: 23,2136 02776 STORE PAC # FOR FLIGHT USE, CULTFLAG IS ON IF
012237,000182: 23,2137 77614 CLRGO # TRUNION IS GREATER THAN 90 DEGR
012238,000183: 23,2140 01630 CULTFLAG
012239,000184: 23,2141 00034 28D
012240,000185: 23,2142 77614 SXTALARM SETGO # ALARM HAS BEEN REMOVED FROM THIS
012241,000186: 23,2143 01430 CULTFLAG
012242,000187: 23,2144 00034 28D # SUBROUTINE, ALARM WILL BE SET BY MPI
012243,000188: 23,2145 77745 ZNB=S1 DLOAD
012244,000189: 23,2146 06325 270DEG
012245,000190: 23,2147 16774 STODL SAC
012246,000191: 23,2150 06327 20DEGS-
012247,000192: 23,2151 02776 STORE PAC
012248,000193: 23,2152 77614 CLRGO
012249,000194: 23,2153 01630 CULTFLAG
012250,000195: 23,2154 00034 28D
012251,000196:
012252,000197: # Page 286
012253,000198: # THESE TWO ROUTINES COMPUTE THE ACTUAL STATE VECTOR FOR LM, CSM BY ADDING
012254,000199: # THE CONIC R,V AND THE DEVIATIONS R,V. THE STATE VECTORS ARE CONVERTED TO
012255,000200: # METERS B-29 AND METERS/CSEC B-7 AND STORED APPROPIRATELY IN RN,VN OR
012256,000201: # R-OTHER, V-OTHER FOR DOWNLINK. THE ROUTINES NAMES ARE SWITCHED IN THE
012257,000202: # OTHER VEHICLES COMPUTER.
012258,000203:
012259,000204: # INPUT
012260,000205: # STATE VECTOR IN TEMPORARY STORAGE AREA
012261,000206: # IF STATE VECTOR IS SCALED POS B27 AND VEL B5
012262,000207: # SET X2 TO +2
012263,000208: # IF STATE VECTOR IS SCALED POS B29 AND VEL B7
012264,000209: # SET X2 TO 0
012265,000210:
012266,000211: # OUTPUT
012267,000212: # R(T) IN RN, V(T) IN VN, T IN PIPTIME
012268,000213: # OR
012269,000214: # R(T) IN R-OTHER, V(T) IN V-OTHER (T IS DEFINED BY T-OTHER)
012270,000215:
012271,000216: 23,2155 BANK 23
012272,000217: 10,2000 SETLOC COMGEOM2
012273,000218: 10,2000 BANK
012274,000219: 10,2237 COUNT 10/GEOM
012275,000220: 10,2237 43414 SVDWN1 BOF RVQ # SW=1=AVETOMID DOING W-MATRIX INTEG
012276,000221: 10,2240 04756 AVEMIDSW
012277,000222: 10,2241 20242 +1
012278,000223: 10,2242 53775 VLOAD VSL*
012279,000224: 10,2243 01521 TDELTAV
012280,000225: 10,2244 57605 0 -7,2
012281,000226: 10,2245 53655 VAD VSL*
012282,000227: 10,2246 01535 RCV
012283,000228: 10,2247 57576 0,2
012284,000229: 10,2250 25171 STOVL RN
012285,000230: 10,2251 01527 TNUV
012286,000231: 10,2252 53257 VSL* VAD
012287,000232: 10,2253 57602 0 -4,2
012288,000233: 10,2254 01543 VCV
012289,000234: 10,2255 77657 VSL*
012290,000235: 10,2256 57576 0,2
012291,000236: 10,2257 15177 STODL VN
012292,000237: 10,2260 01517 TET
012293,000238: 10,2261 01205 STORE PIPTIME
012294,000239: 10,2262 77616 RVQ
012295,000240: 10,2263 53775 SVDWN2 VLOAD VSL*
012296,000241: 10,2264 01521 TDELTAV
012297,000242: 10,2265 57605 0 -7,2
012298,000243: 10,2266 53655 VAD VSL*
012299,000244: 10,2267 01535 RCV
012300,000245: # Page 287
012301,000246: 10,2270 57576 0,2
012302,000247: 10,2271 25722 STOVL R-OTHER
012303,000248: 10,2272 01527 TNUV
012304,000249: 10,2273 53257 VSL* VAD
012305,000250: 10,2274 57602 0 -4,2
012306,000251: 10,2275 01543 VCV
012307,000252: 10,2276 77657 VSL*
012308,000253: 10,2277 57576 0,2
012309,000254: 10,2300 01730 STORE V-OTHER
012310,000255: 10,2301 77616 RVQ
012311,000256:
012312,000257: # Page 288
012313,000258: # SUBROUTINE TO COMPUTE THE NATURAL LOG OF C(MPAC, MPAC +1).
012314,000259:
012315,000260: # ENTRY: CALL
012316,000261: # LOG
012317,000262:
012318,000263: # SUBROUTINE RETURNS WITH -LOG IN DP MPAC.
012319,000264:
012320,000265: # EBANK IS ARBITRARY.
012321,000266:
012322,000267: 14,2000 BANK 14
012323,000268: 23,2000 SETLOC POWFLIT2
012324,000269: 23,2000 BANK
012325,000270: 23,2155 COUNT 23/GEOM
012326,000271:
012327,000272: 23,2155 44301 LOG NORM BDSU # GENERATES LOG BY SHIFTING ARG
012328,000273: 23,2156 00160 MPAC +3 # UNTIL IT LIES BETWEEN .5 AND 1.
012329,000274: 23,2157 06212 NEARLY1 # THE LOG OF THIS PART IS FOUND AND THE
012330,000275: 23,2160 77776 EXIT # LOG OF THE SHIFTED PART IS COMPUTED
012331,000276: 23,2161 07171 TC POLY # AND ADDED IN. SHIFT COUNT STORED
012332,000277: 23,2162 00002 DEC 2 B-14 # (N-1, SUPPLIED BY SMERZH)
012333,000278: 23,2163 00000 00000 2DEC 0 B-28 # IN MPAC +3.
012334,000279: 23,2165 01001 14636 2DEC .031335467
012335,000280: 23,2167 00325 07310 2DEC .0130145859
012336,000281: 23,2171 00541 16735 2DEC .0215738898
012337,000282:
012338,000283: 23,2173 34714 CAF ZERO
012339,000284: 23,2174 54156 TS MPAC +2
012340,000285: 23,2175 00006 EXTEND
012341,000286: 23,2176 32214 DCA CLOG2/32
012342,000287: 23,2177 52155 DXCH MPAC
012343,000288: 23,2200 52160 DXCH MPAC +3
012344,000289: 23,2201 40000 COM # LOAD POSITIVE SHIFT COUNT IN A.
012345,000290: 23,2202 07256 TC SHORTMP # MULTIPLY BY SHIFT COUNT.
012346,000291:
012347,000292: 23,2203 52156 DXCH MPAC +1
012348,000293: 23,2204 52155 DXCH MPAC
012349,000294: 23,2205 52160 DXCH MPAC +3
012350,000295: 23,2206 20155 DAS MPAC
012351,000296: 23,2207 06006 TC INTPRET # RESULT IN MPAC, MPAC +1
012352,000297:
012353,000298: 23,2210 77616 RVQ
012354,000299:
012355,000300: 23,2211 37777 37777 NEARLY1 2DEC .999999999
012356,000301:
012357,000302: # Page 289
012358,000303: 23,2213 00542 34414 CLOG2/32 2DEC .0216608494
012359,000304:
012360,000305: # Page 290
012361,000306: # SUBROUTINE NAME: EARTH ROTATOR (EARROT1 OR EARROT2) DATE: 15 FEB 67
012362,000307: # MOD NO: N +1 LOG SECTION: POWERED FLIGHT SUBROS
012363,000308: # MOD BY: ENTRY GROUP (BAIRNSFATHER)
012364,000309:
012365,000310: # FUNCTIONAL DESCRIPTION: THIS ROUTINE PROJECTS THE INITIAL EARTH TARGET VECTOR RTINIT AHEAD THROUGH
012366,000311: # THE ESTIMATED TIME OF FLIGHT. INITIAL CALL RESOLVES THE INITIAL TARGET VECTOR RTINIT INTO EASTERLY
012367,000312: # AND NORMAL COMPONENTS RTEAST AND RTNORM. INITIAL AND SUBSEQUENT CALLS ROTATE THIS VECTOR
012368,000313: # ABOUT THE (FULL) UNIT POLAR AXIS UNITW THROUGH THE ANGLE WIE DTEAROT TO OBTAIN THE ROTATED
012369,000314: # TARGET VECTOR RT. ALL VECTORS EXCEPT UNITW ARE HALF UNIT.
012370,000315: # THE EQUATIONS ARE:
012371,000316: # _ _ _ _
012372,000317: # RT = RTINIT + RTNORM (COS(WT) - 1) + RTEAST SIN(WT)
012373,000318:
012374,000319: # WHERE WT = WIE DTEAROT
012375,000320:
012376,000321: # RTINIT = INITIAL TARGET VECTOR
012377,000322: # _ _ _
012378,000323: # RTEAST = UNITW * RTINIT
012379,000324: # _ _ _
012380,000325: # RTNORM = RTEAST * UNITW
012381,000326:
012382,000327: # FOR CONTINUOUS UPDATING, ONLY ONE ENTRY TO EARROT1 IS REQUIRED, WITH SUBSEQUENT ENTRIES AT EARROT2.
012383,000328: #
012384,000329: # CALLING SEQUENCE: FIRST CALL SUBSEQUENT CALL
012385,000330: # STCALL DTEAROT STCALL DTEAROT
012386,000331: # EARROT1 EARROT2
012387,000332: # C(MPAC) UNSPECIFIED C(MPAC) = DTEAROT
012388,000333: # PUSHLOC = PDL+0, ARBITRARY. 6 LOCATIONS USED.
012389,000334:
012390,000335: # SUBROUTINES USED: NONE
012391,000336:
012392,000337: # NORMAL EXIT MODES: RVQ
012393,000338:
012394,000339: # ALARMS: NONE
012395,000340:
012396,000341: # OUTPUT: RTEAST (-1) .5 UNIT VECTOR EAST, COMPNT OF RTINIT LEFT BY FIRST CALL
012397,000342: # RTNORM (-1) .5 UNIT VECTOR NORML, COMPNT OF RTINIT LEFT BY FIRST CALL
012398,000343: # RT (-1) .5 UNIT TARGET VECTOR, ROTATED LEFT BY ALL CALLS
012399,000344: # DTEAROT (-28) CS MAY BE CHANGED BY EARROT2, IF OVER 1 DAY
012400,000345:
012401,000346: # ERASABLE INITIALIZATION REQUIRED:
012402,000347: # UNITW (0) UNIT POLAR VECTOR PAD LOADED
012403,000348: # RTINIT (-1) .5 UNIT INITIAL TARGET VECTOR LEFT BY ENTRY
012404,000349: # DTEAROT (-26) CS TIME OF FLIGHT LEFT BY CALLER
012405,000350:
012406,000351: # DEBRIS: QPRET, PDL+0 ... PDL+5
012407,000352: # Page 291
012408,000353: 23,2215 E7,1451 EBANK= RTINIT
012409,000354:
012410,000355: 23,2215 47375 EARROT1 VLOAD VXV
012411,000356: 23,2216 01714 UNITW # FULL UNIT VECTOR
012412,000357: 23,2217 03452 RTINIT # .5 UNIT
012413,000358: 23,2220 03460 STORE RTEAST # .5 UNIT
012414,000359:
012415,000360: 23,2221 77635 VXV
012416,000361: 23,2222 01714 UNITW # FULL UNIT
012417,000362: 23,2223 17466 STODL RTNORM # .5 UNIT
012418,000363: 23,2224 03606 DTEAROT # (-28) CS
012419,000364:
012420,000365: 23,2225 56204 EARROT2 BOVB DDV
012421,000366: 23,2226 57343 TCDANZIG # RESET OVFIND, IF ON
012422,000367: 23,2227 06256 1/WIE
012423,000368: 23,2230 41400 BOV PUSH
012424,000369: 23,2231 46245 OVERADAY
012425,000370: 23,2232 45346 COS DSU
012426,000371: 23,2233 15330 HIDPHALF
012427,000372: 23,2234 65361 VXSC PDDL # XCH W PUSH LIST
012428,000373: 23,2235 03466 RTNORM # .5 UNIT
012429,000374: 23,2236 74356 SIN VXSC
012430,000375: 23,2237 03460 RTEAST # .5 UNIT
012431,000376: 23,2240 76455 VAD VSL1
012432,000377: 23,2241 53455 VAD UNIT # INSURE THAT RT IS "UNIT".
012433,000378: 23,2242 03452 RTINIT # .5 UNIT
012434,000379: 23,2243 03474 STORE RT # .5 UNIT TARGET VECTOR
012435,000380:
012436,000381: 23,2244 77616 RVQ
012437,000382:
012438,000383: 23,2245 75345 OVERADAY DLOAD SIGN
012439,000384: 23,2246 06256 1/WIE
012440,000385: 23,2247 03606 DTEAROT
012441,000386: 23,2250 77621 BDSU
012442,000387: 23,2251 03606 DTEAROT
012443,000388: 23,2252 03606 STORE DTEAROT
012444,000389:
012445,000390: 23,2253 77650 GOTO
012446,000391: 23,2254 46225 EARROT2
012447,000392:
012448,000393: # WIE 2DEC .1901487997
012449,000394: 23,2255 01015 34732 1/WIE 2DEC 8616410 B-28
012450,000395: 23,2257 15373 11346 NB2NB1 2DEC +.8431756920 B-1
012451,000396: 23,2261 00000 00000 2DEC 0 B-28
012452,000397: 23,2263 67313 65307 2DEC -.5376381241 B-1
012453,000398: # Page 292
012454,000399: 23,2265 00000 00000 ZERINFLT 2DEC 0 B-28
012455,000400: 23,2267 20000 00000 HALFNFLT 2DEC .5
012456,000401: 23,2271 00000 00000 2DEC 0 B-28
012457,000402: 23,2273 10464 12470 2DEC +.5376381241 B-1
012458,000403: 23,2275 00000 00000 2DEC 0 B-28
012459,000404: 23,2277 15373 11346 2DEC +.8431756920 B-1
012460,000405: 23,2301 15373 11346 NB1NB2 2DEC +.8431756920 B-1
012461,000406: 23,2303 00000 00000 2DEC 0 B-28
012462,000407: 23,2305 10464 12470 2DEC +.5376381241 B-1
012463,000408: 23,2307 00000 00000 2DEC 0 B-28
012464,000409: 23,2311 20000 00000 2DEC .5
012465,000410: 23,2313 00000 00000 2DEC 0 B-28
012466,000411: 23,2315 67313 65307 2DEC -.5376381241 B-1
012467,000412: 23,2317 00000 00000 2DEC 0 B-28
012468,000413: 23,2321 15373 11346 2DEC +.8431756920 B-1
012469,000414: # Page 293
012470,000415: 23,2323 07020 10DEGS- DEC 3600 B-14
012471,000416: 23,2324 60000 270DEG OCT 60000 # SHAFT 270 DEGREES 25 COMP.
012472,000417: 23,2325 00000 OCT 00000
012473,000418: 23,2326 61740 20DEGS- DEC -07199 B-14
012474,000419: 23,2327 77777 DEC -00000 B-14
012475,000420: 23,2330 07020 20DEG- DEC 03600 B-14
012476,000421: 23,2331 00000 DEC 00000 B-14
012477,000422:
End of include-file CSM_GEOMETRY.agc. Parent file is MAIN.agc