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