Source Code
012359,000001: # Copyright: Public domain.
012360,000002: # Filename: CSM_GEOMETRY.agc
012361,000003: # Purpose: Part of the source code for Colossus 2A, AKA Comanche 055.
012362,000004: # It is part of the source code for the Command Module's (CM)
012363,000005: # Apollo Guidance Computer (AGC), for Apollo 11.
012364,000006: # Assembler: yaYUL
012365,000007: # Contact: Ron Burkey <info@sandroid.org>.
012366,000008: # Website: www.ibiblio.org/apollo.
012367,000009: # Pages: 285-296
012368,000010: # Mod history: 2009-05-08 RSB Adapted from the Colossus249/ file of the
012369,000011: # same name, using Comanche055 page images.
012370,000012:
012371,000013: # This source code has been transcribed or otherwise adapted from digitized
012372,000014: # images of a hardcopy from the MIT Museum. The digitization was performed
012373,000015: # by Paul Fjeld, and arranged for by Deborah Douglas of the Museum. Many
012374,000016: # thanks to both. The images (with suitable reduction in storage size and
012375,000017: # consequent reduction in image quality as well) are available online at
012376,000018: # www.ibiblio.org/apollo. If for some reason you find that the images are
012377,000019: # illegible, contact me at info@sandroid.org about getting access to the
012378,000020: # (much) higher-quality images which Paul actually created.
012379,000021:
012380,000022: # Notations on the hardcopy document read, in part:
012381,000023:
012382,000024: # Assemble revision 055 of AGC program Comanche by NASA
012383,000025: # 2021113-051. 10:28 APR. 1, 1969
012384,000026:
012385,000027: # This AGC program shall also be referred to as
012386,000028: # Colossus 2A
012387,000029:
012388,000030: # Page 285
012389,000031: 22,2000 BANK 22
012390,000032: 23,2000 SETLOC COMGEOM1
012391,000033: 23,2000 BANK
012392,000034:
012393,000035: # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT
012394,000036: # VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WTIH THE SEXTANT LINE OF SIGHT.
012395,000037:
012396,000038: # THE INPUTS ARE: 1) THE SEXTAND SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE
012397,000039: # MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR
012398,000040: # JOB VAC AREA.
012399,000041:
012400,000042: # THE OUTPUT IS A HALF-UNIT VECTOR IN NAVIGATION BASE COORDINATES AND STORED AT LOCATION 32D OF THE VAC AREA. THE
012401,000043: # OUTPUT IS ALSO AVAILABLE AT MPAC.
012402,000044:
012403,000045: 23,2000 COUNT 23/GEOM
012404,000046:
012405,000047: 23,2000 47133 SXTNB SLOAD* RTB # PUSHDOWN 00,02,04,(17D-19D),32D-36D
012406,000048: 23,2001 00006 5,1 # TRUNNION = TA
012407,000049: 23,2002 45513 CDULOGIC
012408,000050: 23,2003 41434 RTB PUSH
012409,000051: 23,2004 46027 SXTLOGIC
012410,000052: 23,2005 72556 SIN SL1
012411,000053: 23,2006 66606 PUSH SLOAD* # PD2 = SIN(TA)
012412,000054: 23,2007 00004 3,1 # SHAFT = SA
012413,000055: 23,2010 41434 RTB PUSH # PD4 = SA
012414,000056: 23,2011 45513 CDULOGIC
012415,000057:
012416,000058: 23,2012 41346 COS DMP
012417,000059: 23,2013 00003 2
012418,000060: 23,2014 14041 STODL STARM # COS(SA)SIN(TA)
012419,000061:
012420,000062: 23,2015 41356 SIN DMP
012421,000063: 23,2016 77626 STADR
012422,000064: 23,2017 63734 STODL STARM +2 # SIN(SA)SIN(TA)
012423,000065:
012424,000066: 23,2020 77746 COS
012425,000067: 23,2021 24045 STOVL STARM +4
012426,000068: 23,2022 00041 STARM # STARM = 32D
012427,000069: 23,2023 76521 MXV VSL1
012428,000070: 23,2024 06302 NB1NB2
012429,000071: 23,2025 00041 STORE 32D
012430,000072: 23,2026 77616 RVQ
012431,000073:
012432,000074: 23,2027 32323 SXTLOGIC CAF 10DEGS- # CORRECT FOR 19.775 DEGREE OFFSET
012433,000075: 23,2030 26154 ADS MPAC
012434,000076: 23,2031 35003 CAF QUARTER
012435,000077: 23,2032 07256 TC SHORTMP
012436,000078: 23,2033 06030 TC DANZIG
012437,000079:
012438,000080: # Page 286
012439,000081: # CALCSXA COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-
012440,000082: # OF-SIGHT LIES ALONG THE STAR VECTOR. THE ROUTINE TAKES THE GIVEN STAR VECTOR AND EXPRESSES IT AS A VECTOR REF-
012441,000083: # ERENECED TO THE OPTICS COORDINATE SYSTEM. IN ADDITION IT SETS UP THREE UNIT VECTORS DEFINING THE X, Y, AND Z AXES
012442,000084: # REFERENCED TO THE OPTICS COORDINATE SYSTEM.
012443,000085:
012444,000086: # THE INPUTS ARE: 1) THE STAR VECTOR REFERRED TO THE PRESENT STABLE MEMMBER COORDINATES STORED AT STAR. 2) SAME ANGLE
012445,000087: # INPUT AS *SMNB*, I.E., SINES AND COSINES OF THE CDU ANGLES, IN THE ORDER Y Z X, AT SINCDU AND COSCDU. A CALL
012446,000088: # TO CDUTRIG WILL PROVIDE THIS INPUT.
012447,000089:
012448,000090: # THE OUTPUT ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012449,000091: # EQUAL TO ZERO).
012450,000092:
012451,000093: 23,2034 77220 CALCSXA ITA VLOAD # PUSHDOWN 00-26D, 28D, 30D, 32D-36D
012452,000094: 23,2035 00034 28D
012453,000095: 23,2036 02766 STAR
012454,000096: 23,2037 77624 CALL
012455,000097: 23,2040 47644 *SMNB*
012456,000098: 23,2041 76521 MXV VSL1
012457,000099: 23,2042 06260 NB2NB1
012458,000100: 23,2043 26766 STOVL STAR
012459,000101: 23,2044 15333 HIUNITX
012460,000102: 23,2045 26555 STOVL XNB1
012461,000103: 23,2046 15331 HIUNITY
012462,000104: 23,2047 26563 STOVL YNB1
012463,000105: 23,2050 15327 HIUNITZ
012464,000106: 23,2051 36571 STCALL ZNB1
012465,000107: 23,2052 46076 SXTANG1
012466,000108:
012467,000109: # Page 287
012468,000110: # SXTANG COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-OF-
012469,000111: # SIGHT LIES ALONG THE STAR VECTOR.
012470,000112:
012471,000113: # THE INPUTS ARE: 1) THE STAR VECTOR REFERRED TO ANY COORDINATE SYSTEM STORED AT STAR. 2) THE NAVIGATION BASE
012472,000114: # COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STROED AT XNB, YNB,AND
012473,000115: # ZNB.
012474,000116:
012475,000117: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012476,000118: # EQUAL TO ZERO).
012477,000119:
012478,000120: 23,2053 47020 SXTANG ITA RTB # PUSHDOWN 16D,18D,22D-26D,28D
012479,000121: 23,2054 00034 28D
012480,000122: 23,2055 45662 TRANSP1 # EREF WRT NB2
012481,000123: 23,2056 64375 VLOAD MXV
012482,000124: 23,2057 02714 XNB
012483,000125: 23,2060 06260 NB2NB1
012484,000126: 23,2061 77772 VSL1
012485,000127: 23,2062 26555 STOVL XNB1
012486,000128: 23,2063 02722 YNB
012487,000129: 23,2064 76521 MXV VSL1
012488,000130: 23,2065 06260 NB2NB1
012489,000131: 23,2066 26563 STOVL YNB1
012490,000132: 23,2067 02730 ZNB
012491,000133: 23,2070 76521 MXV VSL1
012492,000134: 23,2071 06260 NB2NB1
012493,000135: 23,2072 02571 STORE ZNB1
012494,000136:
012495,000137: 23,2073 47034 RTB RTB
012496,000138: 23,2074 45662 TRANSP1
012497,000139: 23,2075 45676 TRANSP2
012498,000140:
012499,000141: 23,2076 47375 SXTANG1 VLOAD VXV
012500,000142: 23,2077 02571 ZNB1
012501,000143: 23,2100 02766 STAR
012502,000144: 23,2101 77600 BOV
012503,000145: 23,2102 46103 +1
012504,000146: 23,2103 40056 UNIT BOV
012505,000147: 23,2104 46145 ZNB=S1
012506,000148: 23,2105 00027 STORE PDA # PDA = UNIT(ZNB X S)
012507,000149:
012508,000150: 23,2106 57441 DOT DCOMP
012509,000151: 23,2107 02555 XNB1
012510,000152: 23,2110 24023 STOVL SINTH # SIN(SA) = PDA . -XNB
012511,000153: 23,2111 00027 PDA
012512,000154:
012513,000155: 23,2112 77641 DOT
012514,000156: 23,2113 02563 YNB1
012515,000157: 23,2114 34021 STCALL COSTH # COS(SA) = PDA . YNB
012516,000158: 23,2115 47256 ARCTRIG
012517,000159: # Page 288
012518,000160: 23,2116 77634 RTB
012519,000161: 23,2117 45546 1STO2S
012520,000162: 23,2120 26774 STOVL SAC
012521,000163: 23,2121 02766 STAR
012522,000164: 23,2122 77600 BOV
012523,000165: 23,2123 46124 +1
012524,000166: 23,2124 72441 DOT SL1
012525,000167: 23,2125 02571 ZNB1
012526,000168: 23,2126 77726 ACOS
012527,000169: 23,2127 62440 BMN SL2
012528,000170: 23,2130 46142 SXTALARM # TRUNNION ANGLE NEGATIVE
012529,000171: 23,2131 45200 BOV DSU
012530,000172: 23,2132 46142 SXTALARM # TRUNNION ANGLE GREATER THAN 90 DEGREES
012531,000173: 23,2133 06331 20DEG-
012532,000174: 23,2134 77634 RTB
012533,000175: 23,2135 45546 1STO2S
012534,000176: 23,2136 02776 STORE PAC # FOR FLIGHT USE, CULTFLAG IS ON IF
012535,000177: 23,2137 77614 CLRGO # TRUNION IS GREATER THAN 90 DEG
012536,000178: 23,2140 01630 CULTFLAG
012537,000179: 23,2141 00034 28D
012538,000180: 23,2142 77614 SXTALARM SETGO # ALARM HAS BEEN REMOVED FROM THIS
012539,000181: 23,2143 01430 CULTFLAG
012540,000182: 23,2144 00034 28D # SUBROUTINE, ALARM WILL BE SET BY MPI
012541,000183: 23,2145 77745 ZNB=S1 DLOAD
012542,000184: 23,2146 06325 270DEG
012543,000185: 23,2147 16774 STODL SAC
012544,000186: 23,2150 06327 20DEGS-
012545,000187: 23,2151 02776 STORE PAC
012546,000188: 23,2152 77614 CLRGO
012547,000189: 23,2153 01630 CULTFLAG
012548,000190: 23,2154 00034 28D
012549,000191:
012550,000192: # Page 289
012551,000193: # THESE TWO ROUTINES COMPUTE THE ACTUAL STATE VECTOR FOR LM, CSM BY ADDING
012552,000194: # THE CONIC R,V AND THE DEVIATIONS R,V. THE STATE VECTORS ARE CONVERTED TO
012553,000195: # METERS B-29 AND METERS/CSEC B-7 AND STORED APPROPRIATELY IN RN,VN OR
012554,000196: # R-OTHER, V-OTHER FOR DOWNLINK. THE ROUTINES NAMES ARE SWITCHED IN THE
012555,000197: # OTHER VEHICLES COMPUTER.
012556,000198:
012557,000199: # INPUT
012558,000200: # STATE VECTOR IN TEMPORARY STORAGE AREA
012559,000201: # IF STATE VECTOR IS SCALED POS B27 AND VEL B5
012560,000202: # SET X2 TO +2
012561,000203: # IF STATE VECTOR IS SCALED POS B29 AND VEL B7
012562,000204: # SET X2 TO 0
012563,000205:
012564,000206: # OUTPUT
012565,000207: # R(T) IN RN, V(T) IN VN, T IN PIPTIME
012566,000208: # OR
012567,000209: # R(T) IN R-OTHER, V(T) IN V-OTHER (T IS DEFINED BY T-OTHER)
012568,000210:
012569,000211: 23,2155 BANK 23
012570,000212: 10,2000 SETLOC COMGEOM2
012571,000213: 10,2000 BANK
012572,000214: 10,2237 COUNT 10/GEOM
012573,000215: 10,2237 43414 SVDWN1 BOF RVQ # SW=1=AVETOMID DOING W-MATRIX INTEG
012574,000216: 10,2240 04756 AVEMIDSW
012575,000217: 10,2241 20242 +1
012576,000218: 10,2242 53775 VLOAD VSL*
012577,000219: 10,2243 01521 TDELTAV
012578,000220: 10,2244 57605 0 -7,2
012579,000221: 10,2245 53655 VAD VSL*
012580,000222: 10,2246 01535 RCV
012581,000223: 10,2247 57576 0,2
012582,000224: 10,2250 25171 STOVL RN
012583,000225: 10,2251 01527 TNUV
012584,000226: 10,2252 53257 VSL* VAD
012585,000227: 10,2253 57602 0 -4,2
012586,000228: 10,2254 01543 VCV
012587,000229: 10,2255 77657 VSL*
012588,000230: 10,2256 57576 0,2
012589,000231: 10,2257 15177 STODL VN
012590,000232: 10,2260 01517 TET
012591,000233: 10,2261 01205 STORE PIPTIME
012592,000234: 10,2262 77616 RVQ
012593,000235:
012594,000236: 10,2263 53775 SVDWN2 VLOAD VSL*
012595,000237: 10,2264 01521 TDELTAV
012596,000238: 10,2265 57605 0 -7,2
012597,000239: 10,2266 53655 VAD VSL*
012598,000240: 10,2267 01535 RCV
012599,000241: # Page 290
012600,000242: 10,2270 57576 0,2
012601,000243: 10,2271 25722 STOVL R-OTHER
012602,000244: 10,2272 01527 TNUV
012603,000245: 10,2273 53257 VSL* VAD
012604,000246: 10,2274 57602 0 -4,2
012605,000247: 10,2275 01543 VCV
012606,000248: 10,2276 77657 VSL*
012607,000249: 10,2277 57576 0,2
012608,000250: 10,2300 01730 STORE V-OTHER
012609,000251: 10,2301 77616 RVQ
012610,000252:
012611,000253: # Page 291
012612,000254: # SUBROUTINE TO COMPUTE THE NATURAL LOG OF C(MPAC, MPAC +1).
012613,000255:
012614,000256: # ENTRY: CALL
012615,000257: # LOG
012616,000258:
012617,000259: # SUBROUTINE RETURNS WITH -LOG IN DP MPAC.
012618,000260:
012619,000261: # EBANK IS ARBITRARY.
012620,000262:
012621,000263: 14,2000 BANK 14
012622,000264: 23,2000 SETLOC POWFLIT2
012623,000265: 23,2000 BANK
012624,000266: 23,2155 COUNT 23/GEOM
012625,000267:
012626,000268: 23,2155 44301 LOG NORM BDSU # GENERATES LOG BY SHIFTING ARG
012627,000269: 23,2156 00160 MPAC +3 # UNTIL IT LIES BETWEEN .5 AND 1.
012628,000270: 23,2157 06212 NEARLY1 # THE LOG OF THIS PART IS FOUND AND THE
012629,000271: 23,2160 77776 EXIT # LOG OF THE SHIFTED PART IS COMPUTED
012630,000272: 23,2161 07171 TC POLY # AND ADDED IN. SHIFT COUNT STORED
012631,000273: 23,2162 00002 DEC 2 B-14 # (N-1, SUPPLIED BY SMERZH)
012632,000274: 23,2163 00000 00000 2DEC 0 B-28 # IN MPAC +3.
012633,000275: 23,2165 01001 14636 2DEC .031335467
012634,000276: 23,2167 00325 07310 2DEC .0130145859
012635,000277: 23,2171 00541 16735 2DEC .0215738898
012636,000278:
012637,000279: 23,2173 35021 CAF ZERO
012638,000280: 23,2174 54156 TS MPAC +2
012639,000281: 23,2175 00006 EXTEND
012640,000282: 23,2176 32214 DCA CLOG2/32
012641,000283: 23,2177 52155 DXCH MPAC
012642,000284: 23,2200 52160 DXCH MPAC +3
012643,000285: 23,2201 40000 COM # LOAD POSITIVE SHIFT COUNT IN A.
012644,000286: 23,2202 07256 TC SHORTMP # MULTIPLY BY SHIFT COUNT.
012645,000287:
012646,000288: 23,2203 52156 DXCH MPAC +1
012647,000289: 23,2204 52155 DXCH MPAC
012648,000290: 23,2205 52160 DXCH MPAC +3
012649,000291: 23,2206 20155 DAS MPAC
012650,000292: 23,2207 06006 TC INTPRET # RESULT IN MPAC, MPAC +1
012651,000293:
012652,000294: 23,2210 77616 RVQ
012653,000295:
012654,000296: 23,2211 37777 37777 NEARLY1 2DEC .999999999
012655,000297:
012656,000298: # Page 292
012657,000299: 23,2213 00542 34414 CLOG2/32 2DEC .0216608494
012658,000300:
012659,000301: # Page 293
012660,000302: # SUBROUTINE NAME: EARTH ROTATOR (EARROT1 OR EARROT2) DATE: 15 FEB 67
012661,000303: # MOD NO: N +1 LOG SECTION: POWERED FLIGHT SUBROS
012662,000304: # MOD BY: ENTRY GROUP (BAIRNSFATHER)
012663,000305:
012664,000306: # FUNCTIONAL DESCRIPTION: THIS ROUTINE PROJECTS THE INITIAL EARTH TARGET VECTOR RTINIT AHEAD THROUGH
012665,000307: # THE ESTIMATED TIME OF FLIGHT. INITIAL CALL RESOLVES THE INITIAL TARGET VECTOR RTINIT INTO EASTERLY
012666,000308: # AND NORMAL COMPONENTS RTEAST AND RTNORM. INITIAL AND SUBSEQUENT CALLS ROTATE THIS VECTOR
012667,000309: # ABOUT THE (FULL) UNIT POLAR AXIS UNITW THROUGH THE ANGLE WIE DTEAROT TO OBTAIN THE ROTATED
012668,000310: # TARGET VECTOR RT. ALL VECTORS EXCEPT UNITW ARE HALF UNIT.
012669,000311: # THE EQUATIONS ARE:
012670,000312: # _ _ _ _
012671,000313: # RT = RTINIT + RTNORM (COS(WT) - 1) + RTEAST SIN(WT)
012672,000314:
012673,000315: # WHERE WT = WIE DTEAROT
012674,000316:
012675,000317: # RTINIT = INITIAL TARGET VECTOR
012676,000318: # _ _ _
012677,000319: # RTEAST = UNITW * RTINIT
012678,000320: # _ _ _
012679,000321: # RTNORM = RTEAST * UNITW
012680,000322:
012681,000323: # FOR CONTINUOUS UPDATING, ONLY ONE ENTRY TO EARROT1 IS REQUIRED, WITH SUBSEQUENT ENTRIES AT EARROT2.
012682,000324: #
012683,000325: # CALLING SEQUENCE: FIRST CALL SUBSEQUENT CALL
012684,000326: # STCALL DTEAROT STCALL DTEAROT
012685,000327: # EARROT1 EARROT2
012686,000328: # C(MPAC) UNSPECIFIED C(MPAC) = DTEAROT
012687,000329: # PUSHLOC = PDL+0, ARBITRARY. 6 LOCATIONS USED.
012688,000330:
012689,000331: # SUBROUTINES USED: NONE
012690,000332:
012691,000333: # NORMAL EXIT MODES: RVQ
012692,000334:
012693,000335: # ALARMS: NONE
012694,000336:
012695,000337: # OUTPUT: RTEAST (-1) .5 UNIT VECTOR EAST, COMPNT OF RTINIT LEFT BY FIRST CALL
012696,000338: # RTNORM (-1) .5 UNIT VECTOR NORML, COMPNT OF RTINIT LEFT BY FIRST CALL
012697,000339: # RT (-1) .5 UNIT TARGET VECTOR, ROTATED LEFT BY ALL CALLS
012698,000340: # DTEAROT (-28) CS MAY BE CHANGED BY EARROT2, IF OVER 1 DAY
012699,000341:
012700,000342: # ERASABLE INITIALIZATION REQUIRED:
012701,000343: # UNITW (0) UNIT POLAR VECTOR PAD LOADED
012702,000344: # RTINIT (-1) .5 UNIT INITIAL TARGET VECTOR LEFT BY ENTRY
012703,000345: # DTEAROT (-28) CS TIME OF FLIGHT LEFT BY CALLER
012704,000346:
012705,000347: # DEBRIS: QPRET, PDL+0 ... PDL+5
012706,000348: # Page 294
012707,000349: 23,2215 E7,1451 EBANK= RTINIT
012708,000350:
012709,000351: 23,2215 47375 EARROT1 VLOAD VXV
012710,000352: 23,2216 01714 UNITW # FULL UNIT VECTOR
012711,000353: 23,2217 03452 RTINIT # .5 UNIT
012712,000354: 23,2220 03460 STORE RTEAST # .5 UNIT
012713,000355:
012714,000356: 23,2221 77635 VXV
012715,000357: 23,2222 01714 UNITW # FULL UNIT
012716,000358: 23,2223 17466 STODL RTNORM # .5 UNIT
012717,000359: 23,2224 03606 DTEAROT # (-28) CS
012718,000360:
012719,000361: 23,2225 56204 EARROT2 BOVB DDV
012720,000362: 23,2226 57352 TCDANZIG # RESET OVFIND, IF ON
012721,000363: 23,2227 06256 1/WIE
012722,000364: 23,2230 41400 BOV PUSH
012723,000365: 23,2231 46245 OVERADAY
012724,000366: 23,2232 45346 COS DSU
012725,000367: 23,2233 15333 HIDPHALF
012726,000368: 23,2234 65361 VXSC PDDL # XCH W PUSH LIST
012727,000369: 23,2235 03466 RTNORM # .5 UNIT
012728,000370: 23,2236 74356 SIN VXSC
012729,000371: 23,2237 03460 RTEAST # .5 UNIT
012730,000372: 23,2240 76455 VAD VSL1
012731,000373: 23,2241 53455 VAD UNIT # INSURE THAT RT IS "UNIT".
012732,000374: 23,2242 03452 RTINIT # .5 UNIT
012733,000375: 23,2243 03474 STORE RT # .5 UNIT TARGET VECTOR
012734,000376:
012735,000377: 23,2244 77616 RVQ
012736,000378:
012737,000379: 23,2245 75345 OVERADAY DLOAD SIGN
012738,000380: 23,2246 06256 1/WIE
012739,000381: 23,2247 03606 DTEAROT
012740,000382: 23,2250 77621 BDSU
012741,000383: 23,2251 03606 DTEAROT
012742,000384: 23,2252 03606 STORE DTEAROT
012743,000385:
012744,000386: 23,2253 77650 GOTO
012745,000387: 23,2254 46225 EARROT2
012746,000388:
012747,000389: # WIE 2DEC .1901487997
012748,000390: 23,2255 01015 34732 1/WIE 2DEC 8616410 B-28
012749,000391: 23,2257 15373 11346 NB2NB1 2DEC +.8431756920 B-1
012750,000392: 23,2261 00000 00000 2DEC 0 B-28
012751,000393: 23,2263 67313 65307 2DEC -.5376381241 B-1
012752,000394: # Page 295
012753,000395: 23,2265 00000 00000 ZERINFLT 2DEC 0 B-28
012754,000396: 23,2267 20000 00000 HALFNFLT 2DEC .5
012755,000397: 23,2271 00000 00000 2DEC 0 B-28
012756,000398: 23,2273 10464 12470 2DEC +.5376381241 B-1
012757,000399: 23,2275 00000 00000 2DEC 0 B-28
012758,000400: 23,2277 15373 11346 2DEC +.8431756920 B-1
012759,000401: 23,2301 15373 11346 NB1NB2 2DEC +.8431756920 B-1
012760,000402: 23,2303 00000 00000 2DEC 0 B-28
012761,000403: 23,2305 10464 12470 2DEC +.5376381241 B-1
012762,000404: 23,2307 00000 00000 2DEC 0 B-28
012763,000405: 23,2311 20000 00000 2DEC .5
012764,000406: 23,2313 00000 00000 2DEC 0 B-28
012765,000407: 23,2315 67313 65307 2DEC -.5376381241 B-1
012766,000408: 23,2317 00000 00000 2DEC 0 B-28
012767,000409: 23,2321 15373 11346 2DEC +.8431756920 B-1
012768,000410: # Page 296
012769,000411: 23,2323 07020 10DEGS- DEC 3600 B-14
012770,000412: 23,2324 60000 270DEG OCT 60000 # SHAFT 270 DEGREES 25 COMP.
012771,000413: 23,2325 00000 OCT 00000
012772,000414: 23,2326 61740 20DEGS- DEC -07199 B-14
012773,000415: 23,2327 77777 DEC -00000 B-14
012774,000416: 23,2330 07020 20DEG- DEC 03600 B-14
012775,000417: 23,2331 00000 DEC 00000 B-14
012776,000418:
End of include-file CSM_GEOMETRY.agc. Parent file is MAIN.agc