Source Code
012360,000001: # Copyright: Public domain.
012361,000002: # Filename: CSM_GEOMETRY.agc
012362,000003: # Purpose: Part of the source code for Colossus 2A, AKA Comanche 055.
012363,000004: # It is part of the source code for the Command Module's (CM)
012364,000005: # Apollo Guidance Computer (AGC), for Apollo 11.
012365,000006: # Assembler: yaYUL
012366,000007: # Contact: Ron Burkey <info@sandroid.org>.
012367,000008: # Website: www.ibiblio.org/apollo.
012368,000009: # Pages: 285-296
012369,000010: # Mod history: 2009-05-08 RSB Adapted from the Colossus249/ file of the
012370,000011: # same name, using Comanche055 page images.
012371,000012:
012372,000013: # This source code has been transcribed or otherwise adapted from digitized
012373,000014: # images of a hardcopy from the MIT Museum. The digitization was performed
012374,000015: # by Paul Fjeld, and arranged for by Deborah Douglas of the Museum. Many
012375,000016: # thanks to both. The images (with suitable reduction in storage size and
012376,000017: # consequent reduction in image quality as well) are available online at
012377,000018: # www.ibiblio.org/apollo. If for some reason you find that the images are
012378,000019: # illegible, contact me at info@sandroid.org about getting access to the
012379,000020: # (much) higher-quality images which Paul actually created.
012380,000021:
012381,000022: # Notations on the hardcopy document read, in part:
012382,000023:
012383,000024: # Assemble revision 055 of AGC program Comanche by NASA
012384,000025: # 2021113-051. 10:28 APR. 1, 1969
012385,000026:
012386,000027: # This AGC program shall also be referred to as
012387,000028: # Colossus 2A
012388,000029:
012389,000030: # Page 285
012390,000031: 22,2000 BANK 22
012391,000032: 23,2000 SETLOC COMGEOM1
012392,000033: 23,2000 BANK
012393,000034:
012394,000035: # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT
012395,000036: # VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WTIH THE SEXTANT LINE OF SIGHT.
012396,000037:
012397,000038: # THE INPUTS ARE: 1) THE SEXTAND SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE
012398,000039: # MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR
012399,000040: # JOB VAC AREA.
012400,000041:
012401,000042: # THE OUTPUT IS A HALF-UNIT VECTOR IN NAVIGATION BASE COORDINATES AND STORED AT LOCATION 32D OF THE VAC AREA. THE
012402,000043: # OUTPUT IS ALSO AVAILABLE AT MPAC.
012403,000044:
012404,000045: 23,2000 COUNT 23/GEOM
012405,000046:
012406,000047: 23,2000 47133 SXTNB SLOAD* RTB # PUSHDOWN 00,02,04,(17D-19D),32D-36D
012407,000048: 23,2001 00006 5,1 # TRUNNION = TA
012408,000049: 23,2002 45513 CDULOGIC
012409,000050: 23,2003 41434 RTB PUSH
012410,000051: 23,2004 46027 SXTLOGIC
012411,000052: 23,2005 72556 SIN SL1
012412,000053: 23,2006 66606 PUSH SLOAD* # PD2 = SIN(TA)
012413,000054: 23,2007 00004 3,1 # SHAFT = SA
012414,000055: 23,2010 41434 RTB PUSH # PD4 = SA
012415,000056: 23,2011 45513 CDULOGIC
012416,000057:
012417,000058: 23,2012 41346 COS DMP
012418,000059: 23,2013 00003 2
012419,000060: 23,2014 14041 STODL STARM # COS(SA)SIN(TA)
012420,000061:
012421,000062: 23,2015 41356 SIN DMP
012422,000063: 23,2016 77626 STADR
012423,000064: 23,2017 63734 STODL STARM +2 # SIN(SA)SIN(TA)
012424,000065:
012425,000066: 23,2020 77746 COS
012426,000067: 23,2021 24045 STOVL STARM +4
012427,000068: 23,2022 00041 STARM # STARM = 32D
012428,000069: 23,2023 76521 MXV VSL1
012429,000070: 23,2024 06302 NB1NB2
012430,000071: 23,2025 00041 STORE 32D
012431,000072: 23,2026 77616 RVQ
012432,000073:
012433,000074: 23,2027 32323 SXTLOGIC CAF 10DEGS- # CORRECT FOR 19.775 DEGREE OFFSET
012434,000075: 23,2030 26154 ADS MPAC
012435,000076: 23,2031 35003 CAF QUARTER
012436,000077: 23,2032 07256 TC SHORTMP
012437,000078: 23,2033 06030 TC DANZIG
012438,000079:
012439,000080: # Page 286
012440,000081: # CALCSXA COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-
012441,000082: # OF-SIGHT LIES ALONG THE STAR VECTOR. THE ROUTINE TAKES THE GIVEN STAR VECTOR AND EXPRESSES IT AS A VECTOR REF-
012442,000083: # ERENECED TO THE OPTICS COORDINATE SYSTEM. IN ADDITION IT SETS UP THREE UNIT VECTORS DEFINING THE X, Y, AND Z AXES
012443,000084: # REFERENCED TO THE OPTICS COORDINATE SYSTEM.
012444,000085:
012445,000086: # THE INPUTS ARE: 1) THE STAR VECTOR REFERRED TO THE PRESENT STABLE MEMMBER COORDINATES STORED AT STAR. 2) SAME ANGLE
012446,000087: # INPUT AS *SMNB*, I.E., SINES AND COSINES OF THE CDU ANGLES, IN THE ORDER Y Z X, AT SINCDU AND COSCDU. A CALL
012447,000088: # TO CDUTRIG WILL PROVIDE THIS INPUT.
012448,000089:
012449,000090: # THE OUTPUT ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012450,000091: # EQUAL TO ZERO).
012451,000092:
012452,000093: 23,2034 77220 CALCSXA ITA VLOAD # PUSHDOWN 00-26D, 28D, 30D, 32D-36D
012453,000094: 23,2035 00034 28D
012454,000095: 23,2036 02766 STAR
012455,000096: 23,2037 77624 CALL
012456,000097: 23,2040 47644 *SMNB*
012457,000098: 23,2041 76521 MXV VSL1
012458,000099: 23,2042 06260 NB2NB1
012459,000100: 23,2043 26766 STOVL STAR
012460,000101: 23,2044 15333 HIUNITX
012461,000102: 23,2045 26555 STOVL XNB1
012462,000103: 23,2046 15331 HIUNITY
012463,000104: 23,2047 26563 STOVL YNB1
012464,000105: 23,2050 15327 HIUNITZ
012465,000106: 23,2051 36571 STCALL ZNB1
012466,000107: 23,2052 46076 SXTANG1
012467,000108:
012468,000109: # Page 287
012469,000110: # SXTANG COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-OF-
012470,000111: # SIGHT LIES ALONG THE STAR VECTOR.
012471,000112:
012472,000113: # THE INPUTS ARE: 1) THE STAR VECTOR REFERRED TO ANY COORDINATE SYSTEM STORED AT STAR. 2) THE NAVIGATION BASE
012473,000114: # COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STROED AT XNB, YNB,AND
012474,000115: # ZNB.
012475,000116:
012476,000117: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012477,000118: # EQUAL TO ZERO).
012478,000119:
012479,000120: 23,2053 47020 SXTANG ITA RTB # PUSHDOWN 16D,18D,22D-26D,28D
012480,000121: 23,2054 00034 28D
012481,000122: 23,2055 45662 TRANSP1 # EREF WRT NB2
012482,000123: 23,2056 64375 VLOAD MXV
012483,000124: 23,2057 02714 XNB
012484,000125: 23,2060 06260 NB2NB1
012485,000126: 23,2061 77772 VSL1
012486,000127: 23,2062 26555 STOVL XNB1
012487,000128: 23,2063 02722 YNB
012488,000129: 23,2064 76521 MXV VSL1
012489,000130: 23,2065 06260 NB2NB1
012490,000131: 23,2066 26563 STOVL YNB1
012491,000132: 23,2067 02730 ZNB
012492,000133: 23,2070 76521 MXV VSL1
012493,000134: 23,2071 06260 NB2NB1
012494,000135: 23,2072 02571 STORE ZNB1
012495,000136:
012496,000137: 23,2073 47034 RTB RTB
012497,000138: 23,2074 45662 TRANSP1
012498,000139: 23,2075 45676 TRANSP2
012499,000140:
012500,000141: 23,2076 47375 SXTANG1 VLOAD VXV
012501,000142: 23,2077 02571 ZNB1
012502,000143: 23,2100 02766 STAR
012503,000144: 23,2101 77600 BOV
012504,000145: 23,2102 46103 +1
012505,000146: 23,2103 40056 UNIT BOV
012506,000147: 23,2104 46145 ZNB=S1
012507,000148: 23,2105 00027 STORE PDA # PDA = UNIT(ZNB X S)
012508,000149:
012509,000150: 23,2106 57441 DOT DCOMP
012510,000151: 23,2107 02555 XNB1
012511,000152: 23,2110 24023 STOVL SINTH # SIN(SA) = PDA . -XNB
012512,000153: 23,2111 00027 PDA
012513,000154:
012514,000155: 23,2112 77641 DOT
012515,000156: 23,2113 02563 YNB1
012516,000157: 23,2114 34021 STCALL COSTH # COS(SA) = PDA . YNB
012517,000158: 23,2115 47256 ARCTRIG
012518,000159: # Page 288
012519,000160: 23,2116 77634 RTB
012520,000161: 23,2117 45546 1STO2S
012521,000162: 23,2120 26774 STOVL SAC
012522,000163: 23,2121 02766 STAR
012523,000164: 23,2122 77600 BOV
012524,000165: 23,2123 46124 +1
012525,000166: 23,2124 72441 DOT SL1
012526,000167: 23,2125 02571 ZNB1
012527,000168: 23,2126 77726 ACOS
012528,000169: 23,2127 62440 BMN SL2
012529,000170: 23,2130 46142 SXTALARM # TRUNNION ANGLE NEGATIVE
012530,000171: 23,2131 45200 BOV DSU
012531,000172: 23,2132 46142 SXTALARM # TRUNNION ANGLE GREATER THAN 90 DEGREES
012532,000173: 23,2133 06331 20DEG-
012533,000174: 23,2134 77634 RTB
012534,000175: 23,2135 45546 1STO2S
012535,000176: 23,2136 02776 STORE PAC # FOR FLIGHT USE, CULTFLAG IS ON IF
012536,000177: 23,2137 77614 CLRGO # TRUNION IS GREATER THAN 90 DEG
012537,000178: 23,2140 01630 CULTFLAG
012538,000179: 23,2141 00034 28D
012539,000180: 23,2142 77614 SXTALARM SETGO # ALARM HAS BEEN REMOVED FROM THIS
012540,000181: 23,2143 01430 CULTFLAG
012541,000182: 23,2144 00034 28D # SUBROUTINE, ALARM WILL BE SET BY MPI
012542,000183: 23,2145 77745 ZNB=S1 DLOAD
012543,000184: 23,2146 06325 270DEG
012544,000185: 23,2147 16774 STODL SAC
012545,000186: 23,2150 06327 20DEGS-
012546,000187: 23,2151 02776 STORE PAC
012547,000188: 23,2152 77614 CLRGO
012548,000189: 23,2153 01630 CULTFLAG
012549,000190: 23,2154 00034 28D
012550,000191:
012551,000192: # Page 289
012552,000193: # THESE TWO ROUTINES COMPUTE THE ACTUAL STATE VECTOR FOR LM, CSM BY ADDING
012553,000194: # THE CONIC R,V AND THE DEVIATIONS R,V. THE STATE VECTORS ARE CONVERTED TO
012554,000195: # METERS B-29 AND METERS/CSEC B-7 AND STORED APPROPRIATELY IN RN,VN OR
012555,000196: # R-OTHER, V-OTHER FOR DOWNLINK. THE ROUTINES NAMES ARE SWITCHED IN THE
012556,000197: # OTHER VEHICLES COMPUTER.
012557,000198:
012558,000199: # INPUT
012559,000200: # STATE VECTOR IN TEMPORARY STORAGE AREA
012560,000201: # IF STATE VECTOR IS SCALED POS B27 AND VEL B5
012561,000202: # SET X2 TO +2
012562,000203: # IF STATE VECTOR IS SCALED POS B29 AND VEL B7
012563,000204: # SET X2 TO 0
012564,000205:
012565,000206: # OUTPUT
012566,000207: # R(T) IN RN, V(T) IN VN, T IN PIPTIME
012567,000208: # OR
012568,000209: # R(T) IN R-OTHER, V(T) IN V-OTHER (T IS DEFINED BY T-OTHER)
012569,000210:
012570,000211: 23,2155 BANK 23
012571,000212: 10,2000 SETLOC COMGEOM2
012572,000213: 10,2000 BANK
012573,000214: 10,2237 COUNT 10/GEOM
012574,000215: 10,2237 43414 SVDWN1 BOF RVQ # SW=1=AVETOMID DOING W-MATRIX INTEG
012575,000216: 10,2240 04756 AVEMIDSW
012576,000217: 10,2241 20242 +1
012577,000218: 10,2242 53775 VLOAD VSL*
012578,000219: 10,2243 01521 TDELTAV
012579,000220: 10,2244 57605 0 -7,2
012580,000221: 10,2245 53655 VAD VSL*
012581,000222: 10,2246 01535 RCV
012582,000223: 10,2247 57576 0,2
012583,000224: 10,2250 25171 STOVL RN
012584,000225: 10,2251 01527 TNUV
012585,000226: 10,2252 53257 VSL* VAD
012586,000227: 10,2253 57602 0 -4,2
012587,000228: 10,2254 01543 VCV
012588,000229: 10,2255 77657 VSL*
012589,000230: 10,2256 57576 0,2
012590,000231: 10,2257 15177 STODL VN
012591,000232: 10,2260 01517 TET
012592,000233: 10,2261 01205 STORE PIPTIME
012593,000234: 10,2262 77616 RVQ
012594,000235:
012595,000236: 10,2263 53775 SVDWN2 VLOAD VSL*
012596,000237: 10,2264 01521 TDELTAV
012597,000238: 10,2265 57605 0 -7,2
012598,000239: 10,2266 53655 VAD VSL*
012599,000240: 10,2267 01535 RCV
012600,000241: # Page 290
012601,000242: 10,2270 57576 0,2
012602,000243: 10,2271 25722 STOVL R-OTHER
012603,000244: 10,2272 01527 TNUV
012604,000245: 10,2273 53257 VSL* VAD
012605,000246: 10,2274 57602 0 -4,2
012606,000247: 10,2275 01543 VCV
012607,000248: 10,2276 77657 VSL*
012608,000249: 10,2277 57576 0,2
012609,000250: 10,2300 01730 STORE V-OTHER
012610,000251: 10,2301 77616 RVQ
012611,000252:
012612,000253: # Page 291
012613,000254: # SUBROUTINE TO COMPUTE THE NATURAL LOG OF C(MPAC, MPAC +1).
012614,000255:
012615,000256: # ENTRY: CALL
012616,000257: # LOG
012617,000258:
012618,000259: # SUBROUTINE RETURNS WITH -LOG IN DP MPAC.
012619,000260:
012620,000261: # EBANK IS ARBITRARY.
012621,000262:
012622,000263: 14,2000 BANK 14
012623,000264: 23,2000 SETLOC POWFLIT2
012624,000265: 23,2000 BANK
012625,000266: 23,2155 COUNT 23/GEOM
012626,000267:
012627,000268: 23,2155 44301 LOG NORM BDSU # GENERATES LOG BY SHIFTING ARG
012628,000269: 23,2156 00160 MPAC +3 # UNTIL IT LIES BETWEEN .5 AND 1.
012629,000270: 23,2157 06212 NEARLY1 # THE LOG OF THIS PART IS FOUND AND THE
012630,000271: 23,2160 77776 EXIT # LOG OF THE SHIFTED PART IS COMPUTED
012631,000272: 23,2161 07171 TC POLY # AND ADDED IN. SHIFT COUNT STORED
012632,000273: 23,2162 00002 DEC 2 B-14 # (N-1, SUPPLIED BY SMERZH)
012633,000274: 23,2163 00000 00000 2DEC 0 B-28 # IN MPAC +3.
012634,000275: 23,2165 01001 14636 2DEC .031335467
012635,000276: 23,2167 00325 07310 2DEC .0130145859
012636,000277: 23,2171 00541 16735 2DEC .0215738898
012637,000278:
012638,000279: 23,2173 35021 CAF ZERO
012639,000280: 23,2174 54156 TS MPAC +2
012640,000281: 23,2175 00006 EXTEND
012641,000282: 23,2176 32214 DCA CLOG2/32
012642,000283: 23,2177 52155 DXCH MPAC
012643,000284: 23,2200 52160 DXCH MPAC +3
012644,000285: 23,2201 40000 COM # LOAD POSITIVE SHIFT COUNT IN A.
012645,000286: 23,2202 07256 TC SHORTMP # MULTIPLY BY SHIFT COUNT.
012646,000287:
012647,000288: 23,2203 52156 DXCH MPAC +1
012648,000289: 23,2204 52155 DXCH MPAC
012649,000290: 23,2205 52160 DXCH MPAC +3
012650,000291: 23,2206 20155 DAS MPAC
012651,000292: 23,2207 06006 TC INTPRET # RESULT IN MPAC, MPAC +1
012652,000293:
012653,000294: 23,2210 77616 RVQ
012654,000295:
012655,000296: 23,2211 37777 37777 NEARLY1 2DEC .999999999
012656,000297:
012657,000298: # Page 292
012658,000299: 23,2213 00542 34414 CLOG2/32 2DEC .0216608494
012659,000300:
012660,000301: # Page 293
012661,000302: # SUBROUTINE NAME: EARTH ROTATOR (EARROT1 OR EARROT2) DATE: 15 FEB 67
012662,000303: # MOD NO: N +1 LOG SECTION: POWERED FLIGHT SUBROS
012663,000304: # MOD BY: ENTRY GROUP (BAIRNSFATHER)
012664,000305:
012665,000306: # FUNCTIONAL DESCRIPTION: THIS ROUTINE PROJECTS THE INITIAL EARTH TARGET VECTOR RTINIT AHEAD THROUGH
012666,000307: # THE ESTIMATED TIME OF FLIGHT. INITIAL CALL RESOLVES THE INITIAL TARGET VECTOR RTINIT INTO EASTERLY
012667,000308: # AND NORMAL COMPONENTS RTEAST AND RTNORM. INITIAL AND SUBSEQUENT CALLS ROTATE THIS VECTOR
012668,000309: # ABOUT THE (FULL) UNIT POLAR AXIS UNITW THROUGH THE ANGLE WIE DTEAROT TO OBTAIN THE ROTATED
012669,000310: # TARGET VECTOR RT. ALL VECTORS EXCEPT UNITW ARE HALF UNIT.
012670,000311: # THE EQUATIONS ARE:
012671,000312: # _ _ _ _
012672,000313: # RT = RTINIT + RTNORM (COS(WT) - 1) + RTEAST SIN(WT)
012673,000314:
012674,000315: # WHERE WT = WIE DTEAROT
012675,000316:
012676,000317: # RTINIT = INITIAL TARGET VECTOR
012677,000318: # _ _ _
012678,000319: # RTEAST = UNITW * RTINIT
012679,000320: # _ _ _
012680,000321: # RTNORM = RTEAST * UNITW
012681,000322:
012682,000323: # FOR CONTINUOUS UPDATING, ONLY ONE ENTRY TO EARROT1 IS REQUIRED, WITH SUBSEQUENT ENTRIES AT EARROT2.
012683,000324: #
012684,000325: # CALLING SEQUENCE: FIRST CALL SUBSEQUENT CALL
012685,000326: # STCALL DTEAROT STCALL DTEAROT
012686,000327: # EARROT1 EARROT2
012687,000328: # C(MPAC) UNSPECIFIED C(MPAC) = DTEAROT
012688,000329: # PUSHLOC = PDL+0, ARBITRARY. 6 LOCATIONS USED.
012689,000330:
012690,000331: # SUBROUTINES USED: NONE
012691,000332:
012692,000333: # NORMAL EXIT MODES: RVQ
012693,000334:
012694,000335: # ALARMS: NONE
012695,000336:
012696,000337: # OUTPUT: RTEAST (-1) .5 UNIT VECTOR EAST, COMPNT OF RTINIT LEFT BY FIRST CALL
012697,000338: # RTNORM (-1) .5 UNIT VECTOR NORML, COMPNT OF RTINIT LEFT BY FIRST CALL
012698,000339: # RT (-1) .5 UNIT TARGET VECTOR, ROTATED LEFT BY ALL CALLS
012699,000340: # DTEAROT (-28) CS MAY BE CHANGED BY EARROT2, IF OVER 1 DAY
012700,000341:
012701,000342: # ERASABLE INITIALIZATION REQUIRED:
012702,000343: # UNITW (0) UNIT POLAR VECTOR PAD LOADED
012703,000344: # RTINIT (-1) .5 UNIT INITIAL TARGET VECTOR LEFT BY ENTRY
012704,000345: # DTEAROT (-28) CS TIME OF FLIGHT LEFT BY CALLER
012705,000346:
012706,000347: # DEBRIS: QPRET, PDL+0 ... PDL+5
012707,000348: # Page 294
012708,000349: 23,2215 E7,1451 EBANK= RTINIT
012709,000350:
012710,000351: 23,2215 47375 EARROT1 VLOAD VXV
012711,000352: 23,2216 01714 UNITW # FULL UNIT VECTOR
012712,000353: 23,2217 03452 RTINIT # .5 UNIT
012713,000354: 23,2220 03460 STORE RTEAST # .5 UNIT
012714,000355:
012715,000356: 23,2221 77635 VXV
012716,000357: 23,2222 01714 UNITW # FULL UNIT
012717,000358: 23,2223 17466 STODL RTNORM # .5 UNIT
012718,000359: 23,2224 03606 DTEAROT # (-28) CS
012719,000360:
012720,000361: 23,2225 56204 EARROT2 BOVB DDV
012721,000362: 23,2226 57352 TCDANZIG # RESET OVFIND, IF ON
012722,000363: 23,2227 06256 1/WIE
012723,000364: 23,2230 41400 BOV PUSH
012724,000365: 23,2231 46245 OVERADAY
012725,000366: 23,2232 45346 COS DSU
012726,000367: 23,2233 15333 HIDPHALF
012727,000368: 23,2234 65361 VXSC PDDL # XCH W PUSH LIST
012728,000369: 23,2235 03466 RTNORM # .5 UNIT
012729,000370: 23,2236 74356 SIN VXSC
012730,000371: 23,2237 03460 RTEAST # .5 UNIT
012731,000372: 23,2240 76455 VAD VSL1
012732,000373: 23,2241 53455 VAD UNIT # INSURE THAT RT IS "UNIT".
012733,000374: 23,2242 03452 RTINIT # .5 UNIT
012734,000375: 23,2243 03474 STORE RT # .5 UNIT TARGET VECTOR
012735,000376:
012736,000377: 23,2244 77616 RVQ
012737,000378:
012738,000379: 23,2245 75345 OVERADAY DLOAD SIGN
012739,000380: 23,2246 06256 1/WIE
012740,000381: 23,2247 03606 DTEAROT
012741,000382: 23,2250 77621 BDSU
012742,000383: 23,2251 03606 DTEAROT
012743,000384: 23,2252 03606 STORE DTEAROT
012744,000385:
012745,000386: 23,2253 77650 GOTO
012746,000387: 23,2254 46225 EARROT2
012747,000388:
012748,000389: # WIE 2DEC .1901487997
012749,000390: 23,2255 01015 34732 1/WIE 2DEC 8616410 B-28
012750,000391: 23,2257 15373 11346 NB2NB1 2DEC +.8431756920 B-1
012751,000392: 23,2261 00000 00000 2DEC 0 B-28
012752,000393: 23,2263 67313 65307 2DEC -.5376381241 B-1
012753,000394: # Page 295
012754,000395: 23,2265 00000 00000 ZERINFLT 2DEC 0 B-28
012755,000396: 23,2267 20000 00000 HALFNFLT 2DEC .5
012756,000397: 23,2271 00000 00000 2DEC 0 B-28
012757,000398: 23,2273 10464 12470 2DEC +.5376381241 B-1
012758,000399: 23,2275 00000 00000 2DEC 0 B-28
012759,000400: 23,2277 15373 11346 2DEC +.8431756920 B-1
012760,000401: 23,2301 15373 11346 NB1NB2 2DEC +.8431756920 B-1
012761,000402: 23,2303 00000 00000 2DEC 0 B-28
012762,000403: 23,2305 10464 12470 2DEC +.5376381241 B-1
012763,000404: 23,2307 00000 00000 2DEC 0 B-28
012764,000405: 23,2311 20000 00000 2DEC .5
012765,000406: 23,2313 00000 00000 2DEC 0 B-28
012766,000407: 23,2315 67313 65307 2DEC -.5376381241 B-1
012767,000408: 23,2317 00000 00000 2DEC 0 B-28
012768,000409: 23,2321 15373 11346 2DEC +.8431756920 B-1
012769,000410: # Page 296
012770,000411: 23,2323 07020 10DEGS- DEC 3600 B-14
012771,000412: 23,2324 60000 270DEG OCT 60000 # SHAFT 270 DEGREES 25 COMP.
012772,000413: 23,2325 00000 OCT 00000
012773,000414: 23,2326 61740 20DEGS- DEC -07199 B-14
012774,000415: 23,2327 77777 DEC -00000 B-14
012775,000416: 23,2330 07020 20DEG- DEC 03600 B-14
012776,000417: 23,2331 00000 DEC 00000 B-14
012777,000418:
End of include-file CSM_GEOMETRY.agc. Parent file is MAIN.agc