Source Code
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These source-code files are part of a reconstructed copy of Comanche 51, the
initial release (though not the final mission release) of the Apollo 11
Command Module (CM) Apollo Guidance Computer (AGC) software. The flown, final
release was Comanche 55. The reconstruction is believed to be exactly accurate,
but in the absence of an actual Apollo-era listing of Comanche 51, some
explanation of the reconstruction process is needed to insure confidence in
that accuracy.
The starting point was the source code of Comanche 55, whose original source code
is available. Comanche 55 source code was then modified by undoing changes known
to have been made between revisions 51 and 55. The most-significant steps involved
reverting changes related to the R-2 lunar potential model, the details of which
were known from the previous, separate, independent reconstruction of the Apollo 10
Lunar Module software Luminary 69/2. The now-reconstructed
Comanche 51 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 match those on the Comanche 55 or Luminary 69 printouts, although
the source code would likely have different page numbers in a contemporary Comanche 51 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 55. Here's a guide
to some of the Apollo documentation relevant to those annotations:
Among documentation not actually referenced in the annotations, there is
a short writeup about the reconstruction process in our software repository
that may be helpful in understanding it from a different perspective. There's also
a handy table
that lists what the number of memory-words should be for each routine in Comanche 51,
which could make a nice double-check; however, we've not performed that double-check ourselves.
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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012154,000002: ## Copyright: Public domain.
012155,000003: ## Filename: CSM_GEOMETRY.agc
012156,000004: ## Purpose: A section of Comanche revision 051.
012157,000005: ## It is part of the reconstructed source code for the
012158,000006: ## original release of the flight software for the Command
012159,000007: ## Module's (CM) Apollo Guidance Computer (AGC) for Apollo 11.
012160,000008: ## The code has been recreated from a copy of Comanche 055. It
012161,000009: ## has been adapted such that the resulting bugger words
012162,000010: ## exactly match those specified for Comanche 51 in NASA drawing
012163,000011: ## 2021153D, which gives relatively high confidence that the
012164,000012: ## reconstruction is correct.
012165,000013: ## Reference: pp. 285-296
012166,000014: ## Assembler: yaYUL
012167,000015: ## Contact: Ron Burkey <info@sandroid.org>.
012168,000016: ## Website: www.ibiblio.org/apollo/index.html
012169,000017: ## Mod history: 2019-07-30 MAS Created from Comanche 55.
012170,000018:
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012172,000020: 22,2000 BANK 22
012173,000021: 23,2000 SETLOC COMGEOM1
012174,000022: 23,2000 BANK
012175,000023:
012176,000024: # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT
012177,000025: # VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WITH THE SEXTANT LINE OF SIGHT.
012178,000026:
012179,000027: # THE INPUTS ARE 1) THE SEXTANT SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE
012180,000028: # MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR
012181,000029: # JOB VAC AREA.
012182,000030:
012183,000031: # THE OUTPUT IS A HALF-UNIT VECTOR IN NAVIGATION BASE COORDINATES AND STORED AT LOCATION 32D OF THE VAC AREA. THE
012184,000032: # OUTPUT IS ALSO AVAILABLE AT MPAC.
012185,000033:
012186,000034: 23,2000 COUNT 23/GEOM
012187,000035:
012188,000036: 23,2000 47133 SXTNB SLOAD* RTB # PUSHDOWN 00,02,04,(17D-19D),32D-36D
012189,000037: 23,2001 00006 5,1 # TRUNNION = TA
012190,000038: 23,2002 45513 CDULOGIC
012191,000039: 23,2003 41434 RTB PUSH
012192,000040: 23,2004 46027 SXTLOGIC
012193,000041: 23,2005 72556 SIN SL1
012194,000042: 23,2006 66606 PUSH SLOAD* # PD2 = SIN(TA)
012195,000043: 23,2007 00004 3,1 # SHAFT = SA
012196,000044: 23,2010 41434 RTB PUSH # PD4 = SA
012197,000045: 23,2011 45513 CDULOGIC
012198,000046:
012199,000047: 23,2012 41346 COS DMP
012200,000048: 23,2013 00003 2
012201,000049: 23,2014 14041 STODL STARM # COS(SA)SIN(TA)
012202,000050:
012203,000051: 23,2015 41356 SIN DMP
012204,000052: 23,2016 77626 STADR
012205,000053: 23,2017 63734 STODL STARM +2 # SIN(SA)SIN(TA)
012206,000054:
012207,000055: 23,2020 77746 COS
012208,000056: 23,2021 24045 STOVL STARM +4
012209,000057: 23,2022 00041 STARM # STARM = 32D
012210,000058: 23,2023 76521 MXV VSL1
012211,000059: 23,2024 06302 NB1NB2
012212,000060: 23,2025 00041 STORE 32D
012213,000061: 23,2026 77616 RVQ
012214,000062:
012215,000063: 23,2027 32323 SXTLOGIC CAF 10DEGS- # CORRECT FOR 19.775 DEGREE OFFSET
012216,000064: 23,2030 26154 ADS MPAC
012217,000065: 23,2031 35003 CAF QUARTER
012218,000066: 23,2032 07256 TC SHORTMP
012219,000067: 23,2033 06030 TC DANZIG
012220,000068:
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012222,000070: # CALCSXA COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-
012223,000071: # OF-SIGHT LIES ALONG THE STAR VECTOR. THE ROUTINE TAKES THE GIVEN STAR VECTOR AND EXPRESSES IT AS A VECTOR REF-
012224,000072: # ERENCED TO THE OPTICS COORDINATE SYSTEM. IN ADDITION IT SETS UP THREE UNIT VECTORS DEFINING THE X, Y, AND Z AXES
012225,000073: # REFERENCED TO THE OPTICS COORDINATE SYSTEM.
012226,000074:
012227,000075: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO PRESENT STABLE MEMBER COORDINATES STORED AT STAR. 2) SAME ANGLE
012228,000076: # INPUT AS *SMNB*, I.E. SINES AND COSINES OF THE CDU ANGLES, IN THE ORDER Y Z X, AT SINCDU AND COSCDU. A CALL
012229,000077: # TO CDUTRIG WILL PROVIDE THIS INPUT.
012230,000078:
012231,000079: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012232,000080: # EQUAL TO ZERO).
012233,000081:
012234,000082: 23,2034 77220 CALCSXA ITA VLOAD # PUSHDOWN 00-26D, 28D, 30D, 32D-36D
012235,000083: 23,2035 00034 28D
012236,000084: 23,2036 02766 STAR
012237,000085: 23,2037 77624 CALL
012238,000086: 23,2040 47644 *SMNB*
012239,000087: 23,2041 76521 MXV VSL1
012240,000088: 23,2042 06260 NB2NB1
012241,000089: 23,2043 26766 STOVL STAR
012242,000090: 23,2044 15333 HIUNITX
012243,000091: 23,2045 26555 STOVL XNB1
012244,000092: 23,2046 15331 HIUNITY
012245,000093: 23,2047 26563 STOVL YNB1
012246,000094: 23,2050 15327 HIUNITZ
012247,000095: 23,2051 36571 STCALL ZNB1
012248,000096: 23,2052 46076 SXTANG1
012249,000097:
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012251,000099: # SXTANG COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-OF-
012252,000100: # SIGHT LIES ALONG THE STAR VECTOR.
012253,000101:
012254,000102: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO ANY COORDINATE SYSTEM STORED AT STAR. 2) THE NAVIGATION BASE
012255,000103: # COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STORED AT XNB, YNB,AND
012256,000104: # ZNB.
012257,000105:
012258,000106: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012259,000107: # EQUAL TO ZERO).
012260,000108:
012261,000109: 23,2053 47020 SXTANG ITA RTB # PUSHDOWN 16D,18D,22D-26D,28D
012262,000110: 23,2054 00034 28D
012263,000111: 23,2055 45662 TRANSP1 # EREF WRT NB2
012264,000112: 23,2056 64375 VLOAD MXV
012265,000113: 23,2057 02714 XNB
012266,000114: 23,2060 06260 NB2NB1
012267,000115: 23,2061 77772 VSL1
012268,000116: 23,2062 26555 STOVL XNB1
012269,000117: 23,2063 02722 YNB
012270,000118: 23,2064 76521 MXV VSL1
012271,000119: 23,2065 06260 NB2NB1
012272,000120: 23,2066 26563 STOVL YNB1
012273,000121: 23,2067 02730 ZNB
012274,000122: 23,2070 76521 MXV VSL1
012275,000123: 23,2071 06260 NB2NB1
012276,000124: 23,2072 02571 STORE ZNB1
012277,000125:
012278,000126: 23,2073 47034 RTB RTB
012279,000127: 23,2074 45662 TRANSP1
012280,000128: 23,2075 45676 TRANSP2
012281,000129:
012282,000130: 23,2076 47375 SXTANG1 VLOAD VXV
012283,000131: 23,2077 02571 ZNB1
012284,000132: 23,2100 02766 STAR
012285,000133: 23,2101 77600 BOV
012286,000134: 23,2102 46103 +1
012287,000135: 23,2103 40056 UNIT BOV
012288,000136: 23,2104 46145 ZNB=S1
012289,000137: 23,2105 00027 STORE PDA # PDA = UNIT(ZNB X S)
012290,000138:
012291,000139: 23,2106 57441 DOT DCOMP
012292,000140: 23,2107 02555 XNB1
012293,000141: 23,2110 24023 STOVL SINTH # SIN(SA) = PDA . -XNB
012294,000142: 23,2111 00027 PDA
012295,000143:
012296,000144: 23,2112 77641 DOT
012297,000145: 23,2113 02563 YNB1
012298,000146: 23,2114 34021 STCALL COSTH # COS(SA) = PDA . YNB
012299,000147: 23,2115 47256 ARCTRIG
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012301,000149: 23,2116 77634 RTB
012302,000150: 23,2117 45546 1STO2S
012303,000151: 23,2120 26774 STOVL SAC
012304,000152: 23,2121 02766 STAR
012305,000153: 23,2122 77600 BOV
012306,000154: 23,2123 46124 +1
012307,000155: 23,2124 72441 DOT SL1
012308,000156: 23,2125 02571 ZNB1
012309,000157: 23,2126 77726 ACOS
012310,000158: 23,2127 62440 BMN SL2
012311,000159: 23,2130 46142 SXTALARM # TRUNNION ANGLE NEGATIVE
012312,000160: 23,2131 45200 BOV DSU
012313,000161: 23,2132 46142 SXTALARM # TRUNNION ANGLE GREATER THAN 90 DEGREES
012314,000162: 23,2133 06331 20DEG-
012315,000163: 23,2134 77634 RTB
012316,000164: 23,2135 45546 1STO2S
012317,000165: 23,2136 02776 STORE PAC # FOR FLIGHT USE, CULTFLAG IS ON IF
012318,000166: 23,2137 77614 CLRGO # TRUNION IS GREATER THAN 90 DEG
012319,000167: 23,2140 01630 CULTFLAG
012320,000168: 23,2141 00034 28D
012321,000169: 23,2142 77614 SXTALARM SETGO # ALARM HAS BEEN REMOVED FROM THIS
012322,000170: 23,2143 01430 CULTFLAG
012323,000171: 23,2144 00034 28D # SUBROUTINE, ALARM WILL BE SET BY MPI
012324,000172: 23,2145 77745 ZNB=S1 DLOAD
012325,000173: 23,2146 06325 270DEG
012326,000174: 23,2147 16774 STODL SAC
012327,000175: 23,2150 06327 20DEGS-
012328,000176: 23,2151 02776 STORE PAC
012329,000177: 23,2152 77614 CLRGO
012330,000178: 23,2153 01630 CULTFLAG
012331,000179: 23,2154 00034 28D
012332,000180:
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012334,000182: # THESE TWO ROUTINES COMPUTE THE ACTUAL STATE VECTOR FOR LM, CSM BY ADDING
012335,000183: # THE CONIC R,V AND THE DEVIATIONS R,V. THE STATE VECTORS ARE CONVERTED TO
012336,000184: # METERS B-29 AND METERS/CSEC B-7 AND STORED APPROPRIATELY IN RN,VN OR
012337,000185: # R-OTHER, V-OTHER FOR DOWNLINK. THE ROUTINES NAMES ARE SWITCHED IN THE
012338,000186: # OTHER VEHICLES COMPUTER.
012339,000187:
012340,000188: # INPUT
012341,000189: # STATE VECTOR IN TEMPORARY STORAGE AREA
012342,000190: # IF STATE VECTOR IS SCALED POS B27 AND VEL B5
012343,000191: # SET X2 TO +2
012344,000192: # IF STATE VECTOR IS SCALED POS B29 AND VEL B7
012345,000193: # SET X2 TO 0
012346,000194:
012347,000195: # OUTPUT
012348,000196: # R(T) IN RN, V(T) IN VN, T IN PIPTIME
012349,000197: # OR
012350,000198: # R(T) IN R-OTHER, V(T) IN V-OTHER (T IS DEFINED BY T-OTHER)
012351,000199:
012352,000200: 23,2155 BANK 23
012353,000201: 10,2000 SETLOC COMGEOM2
012354,000202: 10,2000 BANK
012355,000203: 10,2237 COUNT 10/GEOM
012356,000204: 10,2237 43414 SVDWN1 BOF RVQ # SW=1=AVETOMID DOING W-MATRIX INTEG
012357,000205: 10,2240 04756 AVEMIDSW
012358,000206: 10,2241 20242 +1
012359,000207: 10,2242 53775 VLOAD VSL*
012360,000208: 10,2243 01521 TDELTAV
012361,000209: 10,2244 57605 0 -7,2
012362,000210: 10,2245 53655 VAD VSL*
012363,000211: 10,2246 01535 RCV
012364,000212: 10,2247 57576 0,2
012365,000213: 10,2250 25171 STOVL RN
012366,000214: 10,2251 01527 TNUV
012367,000215: 10,2252 53257 VSL* VAD
012368,000216: 10,2253 57602 0 -4,2
012369,000217: 10,2254 01543 VCV
012370,000218: 10,2255 77657 VSL*
012371,000219: 10,2256 57576 0,2
012372,000220: 10,2257 15177 STODL VN
012373,000221: 10,2260 01517 TET
012374,000222: 10,2261 01205 STORE PIPTIME
012375,000223: 10,2262 77616 RVQ
012376,000224:
012377,000225: 10,2263 53775 SVDWN2 VLOAD VSL*
012378,000226: 10,2264 01521 TDELTAV
012379,000227: 10,2265 57605 0 -7,2
012380,000228: 10,2266 53655 VAD VSL*
012381,000229: 10,2267 01535 RCV
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012383,000231: 10,2270 57576 0,2
012384,000232: 10,2271 25722 STOVL R-OTHER
012385,000233: 10,2272 01527 TNUV
012386,000234: 10,2273 53257 VSL* VAD
012387,000235: 10,2274 57602 0 -4,2
012388,000236: 10,2275 01543 VCV
012389,000237: 10,2276 77657 VSL*
012390,000238: 10,2277 57576 0,2
012391,000239: 10,2300 01730 STORE V-OTHER
012392,000240: 10,2301 77616 RVQ
012393,000241:
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012395,000243: # SUBROUTINE TO COMPUTE THE NATURAL LOG OF C(MPAC, MPAC +1).
012396,000244:
012397,000245: # ENTRY: CALL
012398,000246: # LOG
012399,000247:
012400,000248: # SUBROUTINE RETURNS WITH -LOG IN DP MPAC.
012401,000249:
012402,000250: # EBANK IS ARBITRARY..
012403,000251:
012404,000252: 14,2000 BANK 14
012405,000253: 23,2000 SETLOC POWFLIT2
012406,000254: 23,2000 BANK
012407,000255: 23,2155 COUNT 23/GEOM
012408,000256:
012409,000257: 23,2155 44301 LOG NORM BDSU # GENERATES LOG BY SHIFTING ARG
012410,000258: 23,2156 00160 MPAC +3 # UNTIL IT LIES BETWEEN .5 AND 1.
012411,000259: 23,2157 06212 NEARLY1 # THE LOG OF THIS PART IS FOUND AND THE
012412,000260: 23,2160 77776 EXIT # LOG OF THE SHIFTED PART IS COMPUTED
012413,000261: 23,2161 07171 TC POLY # AND ADDED IN. SHIFT COUNT STORED
012414,000262: 23,2162 00002 DEC 2 B-14 # (N-1, SUPPLIED BY SMERZH)
012415,000263: 23,2163 00000 00000 2DEC 0 B-28 # IN MPAC +3.
012416,000264: 23,2165 01001 14636 2DEC .031335467
012417,000265: 23,2167 00325 07310 2DEC .0130145859
012418,000266: 23,2171 00541 16735 2DEC .0215738898
012419,000267:
012420,000268: 23,2173 35021 CAF ZERO
012421,000269: 23,2174 54156 TS MPAC +2
012422,000270: 23,2175 00006 EXTEND
012423,000271: 23,2176 32214 DCA CLOG2/32
012424,000272: 23,2177 52155 DXCH MPAC
012425,000273: 23,2200 52160 DXCH MPAC +3
012426,000274: 23,2201 40000 COM # LOAD POSITIVE SHIFT COUNT IN A.
012427,000275: 23,2202 07256 TC SHORTMP # MULTIPLY BY SHIFT COUNT.
012428,000276:
012429,000277: 23,2203 52156 DXCH MPAC +1
012430,000278: 23,2204 52155 DXCH MPAC
012431,000279: 23,2205 52160 DXCH MPAC +3
012432,000280: 23,2206 20155 DAS MPAC
012433,000281: 23,2207 06006 TC INTPRET # RESULT IN MPAC, MPAC +1
012434,000282:
012435,000283: 23,2210 77616 RVQ
012436,000284:
012437,000285: 23,2211 37777 37777 NEARLY1 2DEC .999999999
012438,000286:
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012440,000288: 23,2213 00542 34414 CLOG2/32 2DEC .0216608494
012441,000289:
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012443,000291: # SUBROUTINE NAME: EARTH ROTATOR (EARROT1 OR EARROT2) DATE: 15 FEB 67
012444,000292: # MOD NO: N +1 LOG SECTION: POWERED FLIGHT SUBROS
012445,000293: # MOD BY: ENTRY GROUP (BAIRNSFATHER)
012446,000294:
012447,000295: # FUNCTIONAL DESCRIPTION: THIS ROUTINE PROJECTS THE INITIAL EARTH TARGET VECTOR RTINIT AHEAD THROUGH
012448,000296: # THE ESTIMATED TIME OF FLIGHT. INITIAL CALL RESOLVES THE INITIAL TARGET VECTOR RTINIT INTO EASTERLY
012449,000297: # AND NORMAL COMPONENTS RTEAST AND RTNORM. INITIAL AND SUBSEQUENT CALLS ROTATE THIS VECTOR
012450,000298: # ABOUT THE (FULL) UNIT POLAR AXIS UNITW THROUGH THE ANGLE WIE DTEAROT TO OBTAIN THE ROTATED
012451,000299: # TARGET VECTOR RT. ALL VECTORS EXCEPT UNITW ARE HALF UNIT.
012452,000300: # THE EQUATIONS ARE
012453,000301: # - - - -
012454,000302: # RT = RTINIT + RTNORM (COS(WT) - 1) + RTEAST SIN(WT)
012455,000303:
012456,000304: # WHERE WT = WIE DTEAROT
012457,000305:
012458,000306: # RTINIT = INITIAL TARGET VECTOR
012459,000307: # - - -
012460,000308: # RTEAST = UNITW * RTINIT
012461,000309: # - - -
012462,000310: # RTNORM = RTEAST * UNITW
012463,000311:
012464,000312: # FOR CONTINUOUS UPDATING, ONLY ONE ENTRY TO EARROT1 IS REQUIRED, WITH SUBSEQUENT ENTRIES AT EARROT2.
012465,000313: #
012466,000314: # CALLING SEQUENCE: FIRST CALL SUBSEQUENT CALL
012467,000315: # STCALL DTEAROT STCALL DTEAROT
012468,000316: # EARROT1 EARROT2
012469,000317: # C(MPAC) UNSPECIFIED C(MPAC) = DTEAROT
012470,000318: # PUSHLOC = PDL+0, ARBITRARY. 6 LOCATIONS USED.
012471,000319:
012472,000320: # SUBROUTINES USED: NONE
012473,000321:
012474,000322: # NORMAL EXIT MODES: RVQ
012475,000323:
012476,000324: # ALARMS: NONE
012477,000325:
012478,000326: # OUTPUT: RTEAST (-1) .5 UNIT VECTOR EAST, COMPNT OF RTINIT LEFT BY FIRST CALL
012479,000327: # RTNORM (-1) .5 UNIT VECTOR NORML, COMPNT OF RTINIT LEFT BY FIRST CALL
012480,000328: # RT (-1) .5 UNIT TARGET VECTOR, ROTATED LEFT BY ALL CALLS
012481,000329: # DTEAROT (-28) CS MAY BE CHANGED BY EARROT2, IF OVER 1 DAY
012482,000330:
012483,000331: # ERASABLE INITIALIZATION REQUIRED:
012484,000332: # UNITW (0) UNIT POLAR VECTOR PAD LOADED
012485,000333: # RTINIT (-1) .5 UNIT INITIAL TARGET VECTOR LEFT BY ENTRY
012486,000334: # DTEAROT (-28) CS TIME OF FLIGHT LEFT BY CALLER
012487,000335:
012488,000336: # DEBRIS: QPRET, PDL+0 ... PDL+5
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012490,000338: 23,2215 E7,1451 EBANK= RTINIT
012491,000339:
012492,000340: 23,2215 47375 EARROT1 VLOAD VXV
012493,000341: 23,2216 01714 UNITW # FULL UNIT VECTOR
012494,000342: 23,2217 03452 RTINIT # .5 UNIT
012495,000343: 23,2220 03460 STORE RTEAST # .5 UNIT
012496,000344:
012497,000345: 23,2221 77635 VXV
012498,000346: 23,2222 01714 UNITW # FULL UNIT
012499,000347: 23,2223 17466 STODL RTNORM # .5 UNIT
012500,000348: 23,2224 03606 DTEAROT # (-28) CS
012501,000349:
012502,000350: 23,2225 56204 EARROT2 BOVB DDV
012503,000351: 23,2226 57352 TCDANZIG # RESET OVFIND, IF ON
012504,000352: 23,2227 06256 1/WIE
012505,000353: 23,2230 41400 BOV PUSH
012506,000354: 23,2231 46245 OVERADAY
012507,000355: 23,2232 45346 COS DSU
012508,000356: 23,2233 15333 HIDPHALF
012509,000357: 23,2234 65361 VXSC PDDL # XCH W PUSH LIST
012510,000358: 23,2235 03466 RTNORM # .5 UNIT
012511,000359: 23,2236 74356 SIN VXSC
012512,000360: 23,2237 03460 RTEAST # .5 UNIT
012513,000361: 23,2240 76455 VAD VSL1
012514,000362: 23,2241 53455 VAD UNIT # INSURE THAT RT IS 'UNIT'.
012515,000363: 23,2242 03452 RTINIT # .5 UNIT
012516,000364: 23,2243 03474 STORE RT # .5 UNIT TARGET VECTOR
012517,000365:
012518,000366: 23,2244 77616 RVQ
012519,000367:
012520,000368: 23,2245 75345 OVERADAY DLOAD SIGN
012521,000369: 23,2246 06256 1/WIE
012522,000370: 23,2247 03606 DTEAROT
012523,000371: 23,2250 77621 BDSU
012524,000372: 23,2251 03606 DTEAROT
012525,000373: 23,2252 03606 STORE DTEAROT
012526,000374:
012527,000375: 23,2253 77650 GOTO
012528,000376: 23,2254 46225 EARROT2
012529,000377:
012530,000378: # WIE 2DEC .1901487997
012531,000379: 23,2255 01015 34732 1/WIE 2DEC 8616410 B-28
012532,000380: 23,2257 15373 11346 NB2NB1 2DEC +.8431756920 B-1
012533,000381: 23,2261 00000 00000 2DEC 0 B-28
012534,000382: 23,2263 67313 65307 2DEC -.5376381241 B-1
|
|
Page 295
|
012536,000384: 23,2265 00000 00000 ZERINFLT 2DEC 0 B-28
012537,000385: 23,2267 20000 00000 HALFNFLT 2DEC .5
012538,000386: 23,2271 00000 00000 2DEC 0 B-28
012539,000387: 23,2273 10464 12470 2DEC +.5376381241 B-1
012540,000388: 23,2275 00000 00000 2DEC 0 B-28
012541,000389: 23,2277 15373 11346 2DEC +.8431756920 B-1
012542,000390: 23,2301 15373 11346 NB1NB2 2DEC +.8431756920 B-1
012543,000391: 23,2303 00000 00000 2DEC 0 B-28
012544,000392: 23,2305 10464 12470 2DEC +.5376381241 B-1
012545,000393: 23,2307 00000 00000 2DEC 0 B-28
012546,000394: 23,2311 20000 00000 2DEC .5
012547,000395: 23,2313 00000 00000 2DEC 0 B-28
012548,000396: 23,2315 67313 65307 2DEC -.5376381241 B-1
012549,000397: 23,2317 00000 00000 2DEC 0 B-28
012550,000398: 23,2321 15373 11346 2DEC +.8431756920 B-1
|
|
Page 296
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012552,000400: 23,2323 07020 10DEGS- DEC 3600 B-14
012553,000401: 23,2324 60000 270DEG OCT 60000 # SHAFT 270 DEGREES 2S COMP.
012554,000402: 23,2325 00000 OCT 00000
012555,000403: 23,2326 61740 20DEGS- DEC -07199 B-14
012556,000404: 23,2327 77777 DEC -00000 B-14
012557,000405: 23,2330 07020 20DEG- DEC 03600 B-14
012558,000406: 23,2331 00000 DEC 00000 B-14
012559,000407:
End of include-file CSM_GEOMETRY.agc. Parent file is MAIN.agc