Source Code
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These source-code files are part of a reconstructed copy of Comanche 45, the
second release, though not the final mission release, of the Apollo 10
Command Module (CM) Apollo Guidance Computer (AGC) software. Comanche 45 was
preceded by Comanche 44 and followed by Comanche 45/2 (the flown release). The reconstruction
is believed to be exactly accurate, but in the absence of an actual Apollo-era
listing of Comanche 45, some explanation of the reconstruction process is needed
to insure confidence in that accuracy.
The starting point was the source code of Comanche 44 (itself previously accurately
reconstructed). Comanche 44 source code was then modified
by incorporating changes known from contemporary documentation to have been
made between revisions 44 and 45. The now-reconstructed Comanche 45 source code was
verified by assembling it and checking that the assembled code had
the expected known-correct memory-bank checksums.
Note that page numbers in the reconstructed code tend to match those in the Comanche 55, the
most-similar revision of Comanche for which we have access to an actual non-reconstructed hardcopy;
the source code would likely have different page numbers in a contemporary
Comanche 45 listing.
Annotations that were not present in the contemporary source code have been added to the reconstructed
code to justify each change relative to Comanche 44. Here's a guide to the Apollo documentation referenced
in those annotations:
There is also
a detailed commentary about the reconstruction process.
Comments expected to have been present in the original source code are prefixed with a single '#' symbol,
whereas comments added later are prefixed by "##" or "###". Report any errors
noted by creating an
issue report at the Virtual AGC
Project's GitHub repository.
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012144,000002: ## Copyright: Public domain.
012145,000003: ## Filename: CSM_GEOMETRY.agc
012146,000004: ## Purpose: A section of Comanche revision 045.
012147,000005: ## It is part of the reconstructed source code for the
012148,000006: ## second release of the flight software for the Command
012149,000007: ## Module's (CM) Apollo Guidance Computer (AGC) for Apollo 10.
012150,000008: ## The code has been recreated from a copy of Comanche 055. It
012151,000009: ## has been adapted such that the resulting bugger words
012152,000010: ## exactly match those specified for Comanche 45 in NASA drawing
012153,000011: ## 2021153D, which gives relatively high confidence that the
012154,000012: ## reconstruction is correct.
012155,000013: ## Assembler: yaYUL
012156,000014: ## Contact: Ron Burkey <info@sandroid.org>.
012157,000015: ## Website: www.ibiblio.org/apollo/index.html
012158,000016: ## Mod history: 2020-12-06 MAS Created from Comanche 44.
012159,000017:
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012161,000019: 22,2000 BANK 22
012162,000020: 23,2000 SETLOC COMGEOM1
012163,000021: 23,2000 BANK
012164,000022:
012165,000023: # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT
012166,000024: # VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WITH THE SEXTANT LINE OF SIGHT.
012167,000025:
012168,000026: # THE INPUTS ARE 1) THE SEXTANT SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE
012169,000027: # MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR
012170,000028: # JOB VAC AREA.
012171,000029:
012172,000030: # THE OUTPUT IS A HALF-UNIT VECTOR IN NAVIGATION BASE COORDINATES AND STORED AT LOCATION 32D OF THE VAC AREA. THE
012173,000031: # OUTPUT IS ALSO AVAILABLE AT MPAC.
012174,000032:
012175,000033: 23,2000 COUNT 23/GEOM
012176,000034:
012177,000035: 23,2000 47133 SXTNB SLOAD* RTB # PUSHDOWN 00,02,04,(17D-19D),32D-36D
012178,000036: 23,2001 00006 5,1 # TRUNNION = TA
012179,000037: 23,2002 45513 CDULOGIC
012180,000038: 23,2003 41434 RTB PUSH
012181,000039: 23,2004 46027 SXTLOGIC
012182,000040: 23,2005 72556 SIN SL1
012183,000041: 23,2006 66606 PUSH SLOAD* # PD2 = SIN(TA)
012184,000042: 23,2007 00004 3,1 # SHAFT = SA
012185,000043: 23,2010 41434 RTB PUSH # PD4 = SA
012186,000044: 23,2011 45513 CDULOGIC
012187,000045:
012188,000046: 23,2012 41346 COS DMP
012189,000047: 23,2013 00003 2
012190,000048: 23,2014 14041 STODL STARM # COS(SA)SIN(TA)
012191,000049:
012192,000050: 23,2015 41356 SIN DMP
012193,000051: 23,2016 77626 STADR
012194,000052: 23,2017 63734 STODL STARM +2 # SIN(SA)SIN(TA)
012195,000053:
012196,000054: 23,2020 77746 COS
012197,000055: 23,2021 24045 STOVL STARM +4
012198,000056: 23,2022 00041 STARM # STARM = 32D
012199,000057: 23,2023 76521 MXV VSL1
012200,000058: 23,2024 06302 NB1NB2
012201,000059: 23,2025 00041 STORE 32D
012202,000060: 23,2026 77616 RVQ
012203,000061:
012204,000062: 23,2027 32323 SXTLOGIC CAF 10DEGS- # CORRECT FOR 19.775 DEGREE OFFSET
012205,000063: 23,2030 26154 ADS MPAC
012206,000064: 23,2031 35003 CAF QUARTER
012207,000065: 23,2032 07256 TC SHORTMP
012208,000066: 23,2033 06030 TC DANZIG
012209,000067:
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012211,000069: # CALCSXA COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-
012212,000070: # OF-SIGHT LIES ALONG THE STAR VECTOR. THE ROUTINE TAKES THE GIVEN STAR VECTOR AND EXPRESSES IT AS A VECTOR REF-
012213,000071: # ERENCED TO THE OPTICS COORDINATE SYSTEM. IN ADDITION IT SETS UP THREE UNIT VECTORS DEFINING THE X, Y, AND Z AXES
012214,000072: # REFERENCED TO THE OPTICS COORDINATE SYSTEM.
012215,000073:
012216,000074: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO PRESENT STABLE MEMBER COORDINATES STORED AT STAR. 2) SAME ANGLE
012217,000075: # INPUT AS *SMNB*, I.E. SINES AND COSINES OF THE CDU ANGLES, IN THE ORDER Y Z X, AT SINCDU AND COSCDU. A CALL
012218,000076: # TO CDUTRIG WILL PROVIDE THIS INPUT.
012219,000077:
012220,000078: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012221,000079: # EQUAL TO ZERO).
012222,000080:
012223,000081: 23,2034 77220 CALCSXA ITA VLOAD # PUSHDOWN 00-26D, 28D, 30D, 32D-36D
012224,000082: 23,2035 00034 28D
012225,000083: 23,2036 02766 STAR
012226,000084: 23,2037 77624 CALL
012227,000085: 23,2040 47644 *SMNB*
012228,000086: 23,2041 76521 MXV VSL1
012229,000087: 23,2042 06260 NB2NB1
012230,000088: 23,2043 26766 STOVL STAR
012231,000089: 23,2044 15333 HIUNITX
012232,000090: 23,2045 26555 STOVL XNB1
012233,000091: 23,2046 15331 HIUNITY
012234,000092: 23,2047 26563 STOVL YNB1
012235,000093: 23,2050 15327 HIUNITZ
012236,000094: 23,2051 36571 STCALL ZNB1
012237,000095: 23,2052 46076 SXTANG1
012238,000096:
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012240,000098: # SXTANG COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-OF-
012241,000099: # SIGHT LIES ALONG THE STAR VECTOR.
012242,000100:
012243,000101: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO ANY COORDINATE SYSTEM STORED AT STAR. 2) THE NAVIGATION BASE
012244,000102: # COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STORED AT XNB, YNB,AND
012245,000103: # ZNB.
012246,000104:
012247,000105: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012248,000106: # EQUAL TO ZERO).
012249,000107:
012250,000108: 23,2053 47020 SXTANG ITA RTB # PUSHDOWN 16D,18D,22D-26D,28D
012251,000109: 23,2054 00034 28D
012252,000110: 23,2055 45662 TRANSP1 # EREF WRT NB2
012253,000111: 23,2056 64375 VLOAD MXV
012254,000112: 23,2057 02714 XNB
012255,000113: 23,2060 06260 NB2NB1
012256,000114: 23,2061 77772 VSL1
012257,000115: 23,2062 26555 STOVL XNB1
012258,000116: 23,2063 02722 YNB
012259,000117: 23,2064 76521 MXV VSL1
012260,000118: 23,2065 06260 NB2NB1
012261,000119: 23,2066 26563 STOVL YNB1
012262,000120: 23,2067 02730 ZNB
012263,000121: 23,2070 76521 MXV VSL1
012264,000122: 23,2071 06260 NB2NB1
012265,000123: 23,2072 02571 STORE ZNB1
012266,000124:
012267,000125: 23,2073 47034 RTB RTB
012268,000126: 23,2074 45662 TRANSP1
012269,000127: 23,2075 45676 TRANSP2
012270,000128:
012271,000129: 23,2076 47375 SXTANG1 VLOAD VXV
012272,000130: 23,2077 02571 ZNB1
012273,000131: 23,2100 02766 STAR
012274,000132: 23,2101 77600 BOV
012275,000133: 23,2102 46103 +1
012276,000134: 23,2103 40056 UNIT BOV
012277,000135: 23,2104 46145 ZNB=S1
012278,000136: 23,2105 00027 STORE PDA # PDA = UNIT(ZNB X S)
012279,000137:
012280,000138: 23,2106 57441 DOT DCOMP
012281,000139: 23,2107 02555 XNB1
012282,000140: 23,2110 24023 STOVL SINTH # SIN(SA) = PDA . -XNB
012283,000141: 23,2111 00027 PDA
012284,000142:
012285,000143: 23,2112 77641 DOT
012286,000144: 23,2113 02563 YNB1
012287,000145: 23,2114 34021 STCALL COSTH # COS(SA) = PDA . YNB
012288,000146: 23,2115 47256 ARCTRIG
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012290,000148: 23,2116 77634 RTB
012291,000149: 23,2117 45546 1STO2S
012292,000150: 23,2120 26774 STOVL SAC
012293,000151: 23,2121 02766 STAR
012294,000152: 23,2122 77600 BOV
012295,000153: 23,2123 46124 +1
012296,000154: 23,2124 72441 DOT SL1
012297,000155: 23,2125 02571 ZNB1
012298,000156: 23,2126 77726 ACOS
012299,000157: 23,2127 62440 BMN SL2
012300,000158: 23,2130 46142 SXTALARM # TRUNNION ANGLE NEGATIVE
012301,000159: 23,2131 45200 BOV DSU
012302,000160: 23,2132 46142 SXTALARM # TRUNNION ANGLE GREATER THAN 90 DEGREES
012303,000161: 23,2133 06331 20DEG-
012304,000162: 23,2134 77634 RTB
012305,000163: 23,2135 45546 1STO2S
012306,000164: 23,2136 02776 STORE PAC # FOR FLIGHT USE, CULTFLAG IS ON IF
012307,000165: 23,2137 77614 CLRGO # TRUNION IS GREATER THAN 90 DEG
012308,000166: 23,2140 01630 CULTFLAG
012309,000167: 23,2141 00034 28D
012310,000168: 23,2142 77614 SXTALARM SETGO # ALARM HAS BEEN REMOVED FROM THIS
012311,000169: 23,2143 01430 CULTFLAG
012312,000170: 23,2144 00034 28D # SUBROUTINE, ALARM WILL BE SET BY MPI
012313,000171: 23,2145 77745 ZNB=S1 DLOAD
012314,000172: 23,2146 06325 270DEG
012315,000173: 23,2147 16774 STODL SAC
012316,000174: 23,2150 06327 20DEGS-
012317,000175: 23,2151 02776 STORE PAC
012318,000176: 23,2152 77614 CLRGO
012319,000177: 23,2153 01630 CULTFLAG
012320,000178: 23,2154 00034 28D
012321,000179:
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012323,000181: # THESE TWO ROUTINES COMPUTE THE ACTUAL STATE VECTOR FOR LM, CSM BY ADDING
012324,000182: # THE CONIC R,V AND THE DEVIATIONS R,V. THE STATE VECTORS ARE CONVERTED TO
012325,000183: # METERS B-29 AND METERS/CSEC B-7 AND STORED APPROPRIATELY IN RN,VN OR
012326,000184: # R-OTHER, V-OTHER FOR DOWNLINK. THE ROUTINES NAMES ARE SWITCHED IN THE
012327,000185: # OTHER VEHICLES COMPUTER.
012328,000186:
012329,000187: # INPUT
012330,000188: # STATE VECTOR IN TEMPORARY STORAGE AREA
012331,000189: # IF STATE VECTOR IS SCALED POS B27 AND VEL B5
012332,000190: # SET X2 TO +2
012333,000191: # IF STATE VECTOR IS SCALED POS B29 AND VEL B7
012334,000192: # SET X2 TO 0
012335,000193:
012336,000194: # OUTPUT
012337,000195: # R(T) IN RN, V(T) IN VN, T IN PIPTIME
012338,000196: # OR
012339,000197: # R(T) IN R-OTHER, V(T) IN V-OTHER (T IS DEFINED BY T-OTHER)
012340,000198:
012341,000199: 23,2155 BANK 23
012342,000200: 10,2000 SETLOC COMGEOM2
012343,000201: 10,2000 BANK
012344,000202: 10,2237 COUNT 10/GEOM
012345,000203: 10,2237 43414 SVDWN1 BOF RVQ # SW=1=AVETOMID DOING W-MATRIX INTEG
012346,000204: 10,2240 04756 AVEMIDSW
012347,000205: 10,2241 20242 +1
012348,000206: 10,2242 53775 VLOAD VSL*
012349,000207: 10,2243 01521 TDELTAV
012350,000208: 10,2244 57605 0 -7,2
012351,000209: 10,2245 53655 VAD VSL*
012352,000210: 10,2246 01535 RCV
012353,000211: 10,2247 57576 0,2
012354,000212: 10,2250 25171 STOVL RN
012355,000213: 10,2251 01527 TNUV
012356,000214: 10,2252 53257 VSL* VAD
012357,000215: 10,2253 57602 0 -4,2
012358,000216: 10,2254 01543 VCV
012359,000217: 10,2255 77657 VSL*
012360,000218: 10,2256 57576 0,2
012361,000219: 10,2257 15177 STODL VN
012362,000220: 10,2260 01517 TET
012363,000221: 10,2261 01205 STORE PIPTIME
012364,000222: 10,2262 77616 RVQ
012365,000223:
012366,000224: 10,2263 53775 SVDWN2 VLOAD VSL*
012367,000225: 10,2264 01521 TDELTAV
012368,000226: 10,2265 57605 0 -7,2
012369,000227: 10,2266 53655 VAD VSL*
012370,000228: 10,2267 01535 RCV
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012372,000230: 10,2270 57576 0,2
012373,000231: 10,2271 25722 STOVL R-OTHER
012374,000232: 10,2272 01527 TNUV
012375,000233: 10,2273 53257 VSL* VAD
012376,000234: 10,2274 57602 0 -4,2
012377,000235: 10,2275 01543 VCV
012378,000236: 10,2276 77657 VSL*
012379,000237: 10,2277 57576 0,2
012380,000238: 10,2300 01730 STORE V-OTHER
012381,000239: 10,2301 77616 RVQ
012382,000240:
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012384,000242: # SUBROUTINE TO COMPUTE THE NATURAL LOG OF C(MPAC, MPAC +1).
012385,000243:
012386,000244: # ENTRY: CALL
012387,000245: # LOG
012388,000246:
012389,000247: # SUBROUTINE RETURNS WITH -LOG IN DP MPAC.
012390,000248:
012391,000249: # EBANK IS ARBITRARY..
012392,000250:
012393,000251: 14,2000 BANK 14
012394,000252: 23,2000 SETLOC POWFLIT2
012395,000253: 23,2000 BANK
012396,000254: 23,2155 COUNT 23/GEOM
012397,000255:
012398,000256: 23,2155 44301 LOG NORM BDSU # GENERATES LOG BY SHIFTING ARG
012399,000257: 23,2156 00160 MPAC +3 # UNTIL IT LIES BETWEEN .5 AND 1.
012400,000258: 23,2157 06212 NEARLY1 # THE LOG OF THIS PART IS FOUND AND THE
012401,000259: 23,2160 77776 EXIT # LOG OF THE SHIFTED PART IS COMPUTED
012402,000260: 23,2161 07171 TC POLY # AND ADDED IN. SHIFT COUNT STORED
012403,000261: 23,2162 00002 DEC 2 B-14 # (N-1, SUPPLIED BY SMERZH)
012404,000262: 23,2163 00000 00000 2DEC 0 B-28 # IN MPAC +3.
012405,000263: 23,2165 01001 14636 2DEC .031335467
012406,000264: 23,2167 00325 07310 2DEC .0130145859
012407,000265: 23,2171 00541 16735 2DEC .0215738898
012408,000266:
012409,000267: 23,2173 35021 CAF ZERO
012410,000268: 23,2174 54156 TS MPAC +2
012411,000269: 23,2175 00006 EXTEND
012412,000270: 23,2176 32214 DCA CLOG2/32
012413,000271: 23,2177 52155 DXCH MPAC
012414,000272: 23,2200 52160 DXCH MPAC +3
012415,000273: 23,2201 40000 COM # LOAD POSITIVE SHIFT COUNT IN A.
012416,000274: 23,2202 07256 TC SHORTMP # MULTIPLY BY SHIFT COUNT.
012417,000275:
012418,000276: 23,2203 52156 DXCH MPAC +1
012419,000277: 23,2204 52155 DXCH MPAC
012420,000278: 23,2205 52160 DXCH MPAC +3
012421,000279: 23,2206 20155 DAS MPAC
012422,000280: 23,2207 06006 TC INTPRET # RESULT IN MPAC, MPAC +1
012423,000281:
012424,000282: 23,2210 77616 RVQ
012425,000283:
012426,000284: 23,2211 37777 37777 NEARLY1 2DEC .999999999
012427,000285:
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012429,000287: 23,2213 00542 34414 CLOG2/32 2DEC .0216608494
012430,000288:
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012432,000290: # SUBROUTINE NAME: EARTH ROTATOR (EARROT1 OR EARROT2) DATE: 15 FEB 67
012433,000291: # MOD NO: N +1 LOG SECTION: POWERED FLIGHT SUBROS
012434,000292: # MOD BY: ENTRY GROUP (BAIRNSFATHER)
012435,000293:
012436,000294: # FUNCTIONAL DESCRIPTION: THIS ROUTINE PROJECTS THE INITIAL EARTH TARGET VECTOR RTINIT AHEAD THROUGH
012437,000295: # THE ESTIMATED TIME OF FLIGHT. INITIAL CALL RESOLVES THE INITIAL TARGET VECTOR RTINIT INTO EASTERLY
012438,000296: # AND NORMAL COMPONENTS RTEAST AND RTNORM. INITIAL AND SUBSEQUENT CALLS ROTATE THIS VECTOR
012439,000297: # ABOUT THE (FULL) UNIT POLAR AXIS UNITW THROUGH THE ANGLE WIE DTEAROT TO OBTAIN THE ROTATED
012440,000298: # TARGET VECTOR RT. ALL VECTORS EXCEPT UNITW ARE HALF UNIT.
012441,000299: # THE EQUATIONS ARE
012442,000300: # - - - -
012443,000301: # RT = RTINIT + RTNORM (COS(WT) - 1) + RTEAST SIN(WT)
012444,000302:
012445,000303: # WHERE WT = WIE DTEAROT
012446,000304:
012447,000305: # RTINIT = INITIAL TARGET VECTOR
012448,000306: # - - -
012449,000307: # RTEAST = UNITW * RTINIT
012450,000308: # - - -
012451,000309: # RTNORM = RTEAST * UNITW
012452,000310:
012453,000311: # FOR CONTINUOUS UPDATING, ONLY ONE ENTRY TO EARROT1 IS REQUIRED, WITH SUBSEQUENT ENTRIES AT EARROT2.
012454,000312: #
012455,000313: # CALLING SEQUENCE: FIRST CALL SUBSEQUENT CALL
012456,000314: # STCALL DTEAROT STCALL DTEAROT
012457,000315: # EARROT1 EARROT2
012458,000316: # C(MPAC) UNSPECIFIED C(MPAC) = DTEAROT
012459,000317: # PUSHLOC = PDL+0, ARBITRARY. 6 LOCATIONS USED.
012460,000318:
012461,000319: # SUBROUTINES USED: NONE
012462,000320:
012463,000321: # NORMAL EXIT MODES: RVQ
012464,000322:
012465,000323: # ALARMS: NONE
012466,000324:
012467,000325: # OUTPUT: RTEAST (-1) .5 UNIT VECTOR EAST, COMPNT OF RTINIT LEFT BY FIRST CALL
012468,000326: # RTNORM (-1) .5 UNIT VECTOR NORML, COMPNT OF RTINIT LEFT BY FIRST CALL
012469,000327: # RT (-1) .5 UNIT TARGET VECTOR, ROTATED LEFT BY ALL CALLS
012470,000328: # DTEAROT (-28) CS MAY BE CHANGED BY EARROT2, IF OVER 1 DAY
012471,000329:
012472,000330: # ERASABLE INITIALIZATION REQUIRED:
012473,000331: # UNITW (0) UNIT POLAR VECTOR PAD LOADED
012474,000332: # RTINIT (-1) .5 UNIT INITIAL TARGET VECTOR LEFT BY ENTRY
012475,000333: # DTEAROT (-28) CS TIME OF FLIGHT LEFT BY CALLER
012476,000334:
012477,000335: # DEBRIS: QPRET, PDL+0 ... PDL+5
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012479,000337: 23,2215 E7,1451 EBANK= RTINIT
012480,000338:
012481,000339: 23,2215 47375 EARROT1 VLOAD VXV
012482,000340: 23,2216 01714 UNITW # FULL UNIT VECTOR
012483,000341: 23,2217 03452 RTINIT # .5 UNIT
012484,000342: 23,2220 03460 STORE RTEAST # .5 UNIT
012485,000343:
012486,000344: 23,2221 77635 VXV
012487,000345: 23,2222 01714 UNITW # FULL UNIT
012488,000346: 23,2223 17466 STODL RTNORM # .5 UNIT
012489,000347: 23,2224 03606 DTEAROT # (-28) CS
012490,000348:
012491,000349: 23,2225 56204 EARROT2 BOVB DDV
012492,000350: 23,2226 57352 TCDANZIG # RESET OVFIND, IF ON
012493,000351: 23,2227 06256 1/WIE
012494,000352: 23,2230 41400 BOV PUSH
012495,000353: 23,2231 46245 OVERADAY
012496,000354: 23,2232 45346 COS DSU
012497,000355: 23,2233 15333 HIDPHALF
012498,000356: 23,2234 65361 VXSC PDDL # XCH W PUSH LIST
012499,000357: 23,2235 03466 RTNORM # .5 UNIT
012500,000358: 23,2236 74356 SIN VXSC
012501,000359: 23,2237 03460 RTEAST # .5 UNIT
012502,000360: 23,2240 76455 VAD VSL1
012503,000361: 23,2241 53455 VAD UNIT # INSURE THAT RT IS 'UNIT'.
012504,000362: 23,2242 03452 RTINIT # .5 UNIT
012505,000363: 23,2243 03474 STORE RT # .5 UNIT TARGET VECTOR
012506,000364:
012507,000365: 23,2244 77616 RVQ
012508,000366:
012509,000367: 23,2245 75345 OVERADAY DLOAD SIGN
012510,000368: 23,2246 06256 1/WIE
012511,000369: 23,2247 03606 DTEAROT
012512,000370: 23,2250 77621 BDSU
012513,000371: 23,2251 03606 DTEAROT
012514,000372: 23,2252 03606 STORE DTEAROT
012515,000373:
012516,000374: 23,2253 77650 GOTO
012517,000375: 23,2254 46225 EARROT2
012518,000376:
012519,000377: # WIE 2DEC .1901487997
012520,000378: 23,2255 01015 34732 1/WIE 2DEC 8616410 B-28
012521,000379: 23,2257 15373 11346 NB2NB1 2DEC +.8431756920 B-1
012522,000380: 23,2261 00000 00000 2DEC 0 B-28
012523,000381: 23,2263 67313 65307 2DEC -.5376381241 B-1
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Page 295
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012525,000383: 23,2265 00000 00000 ZERINFLT 2DEC 0 B-28
012526,000384: 23,2267 20000 00000 HALFNFLT 2DEC .5
012527,000385: 23,2271 00000 00000 2DEC 0 B-28
012528,000386: 23,2273 10464 12470 2DEC +.5376381241 B-1
012529,000387: 23,2275 00000 00000 2DEC 0 B-28
012530,000388: 23,2277 15373 11346 2DEC +.8431756920 B-1
012531,000389: 23,2301 15373 11346 NB1NB2 2DEC +.8431756920 B-1
012532,000390: 23,2303 00000 00000 2DEC 0 B-28
012533,000391: 23,2305 10464 12470 2DEC +.5376381241 B-1
012534,000392: 23,2307 00000 00000 2DEC 0 B-28
012535,000393: 23,2311 20000 00000 2DEC .5
012536,000394: 23,2313 00000 00000 2DEC 0 B-28
012537,000395: 23,2315 67313 65307 2DEC -.5376381241 B-1
012538,000396: 23,2317 00000 00000 2DEC 0 B-28
012539,000397: 23,2321 15373 11346 2DEC +.8431756920 B-1
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Page 296
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012541,000399: 23,2323 07020 10DEGS- DEC 3600 B-14
012542,000400: 23,2324 60000 270DEG OCT 60000 # SHAFT 270 DEGREES 2S COMP.
012543,000401: 23,2325 00000 OCT 00000
012544,000402: 23,2326 61740 20DEGS- DEC -07199 B-14
012545,000403: 23,2327 77777 DEC -00000 B-14
012546,000404: 23,2330 07020 20DEG- DEC 03600 B-14
012547,000405: 23,2331 00000 DEC 00000 B-14
012548,000406:
End of include-file CSM_GEOMETRY.agc. Parent file is MAIN.agc