Source Code
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These source-code files were obtained by digitally photographing the
Colossus 237 program listing from the private collection of original
AGC developer Fred Martin, and then modifying pre-existing Colossus 249
(Apollo 9) source files to incorporate changes. Note that the page images
presented online are of reduced quality, and that additional images
are available. Report any conversion errors or legibility
problems in page images to info@sandroid.org.
Notations on the program listing read, in part:GAP: ASSEMBLE REVISION 237 OF AGC PROGRAM COLOSSUS BY NASA 2021111-031 1:17 AUG. 24, 1968 |
016703,000002: # Copyright: Public domain.
016704,000003: # Filename: R60,R62.agc
016705,000004: # Purpose: Part of the source code for Colossus build 237.
016706,000005: # This is for the Command Module's (CM) Apollo Guidance
016707,000006: # Computer (AGC), we believe for Apollo 8.
016708,000007: # Assembler: yaYUL
016709,000008: # Contact: Jim Lawton <jim DOT lawton AT gmail DOT com>
016710,000009: # Website: www.ibiblio.org/apollo/index.html
016711,000010: # Page scans: www.ibiblio.org/apollo/ScansForConversion/Colossus237/
016712,000011: # Mod history: 2011-01-27 JL Adapted from corresponding Colossus 249 file.
016713,000012:
016714,000013: # # Page 381
016715,000014: 34,2002 BANK 34
016716,000015: 27,2000 SETLOC MANUVER
016717,000016: 27,2000 BANK
016718,000017:
016719,000018: 27,2000 1146 EBANK= TEMPR60
016720,000019:
016721,000020: 27,2000 COUNT 27/R60
016722,000021:
016723,000022:
016724,000023: # R60CSM
016725,000024: # REV 13 CONFORMS TO GSOP CHAPTER FOUR REVISION LOGIC 09 JAN 18,1968
016726,000025:
016727,000026:
016728,000027:
016729,000028: 27,2000 04604 R60CSM TC MAKECADR
016730,000029: 27,2001 55146 TS TEMPR60
016731,000030:
016732,000031: # INSERT PRIODSP CHECK WITH R22 (V06N49) WITH JENNINGS BRODEUR
016733,000032:
016734,000033: 27,2002 34705 REDOMANN CAF BIT6
016735,000034: 27,2003 70101 MASK FLAGWRD5 # IS 3-AXIS FLAG SET
016736,000035: 27,2004 10000 CCS A
016737,000036: 27,2005 12013 TCF TOBALL # YES
016738,000037: 27,2006 06006 TC INTPRET
016739,000038: 27,2007 77624 CALL
016740,000039: 27,2010 56126 VECPOINT # TO COMPUTE FINAL ANGLES
016741,000040: 27,2011 01156 STORE CPHI # STORE FINAL ANGLES - CPHI,CTHETA,CPSI
016742,000041: 27,2012 77776 EXIT
016743,000042:
016744,000043: 27,2013 32125 TOBALL CAF V06N18
016745,000044: 27,2014 04555 TC BANKCALL
016746,000045: 27,2015 21036 CADR GOPERF2R # DISPLAY PLEASE PERFORM AUTO MANEUVER
016747,000046: 27,2016 02114 TC R61TEST
016748,000047: 27,2017 02023 TC REDOMANC # PROCEED
016749,000048: 27,2020 12052 TCF ENDMANU1 # ENTER I.E. FINISHED WITH R60
016750,000049:
016751,000050: 27,2021 02056 TC CHKLINUS # TO CHECK FOR PRIORITY DISPLAYS
016752,000051: 27,2022 05112 TC ENDOFJOB
016753,000052:
016754,000053: 27,2023 34705 REDOMANC CAF BIT6
016755,000054: 27,2024 70101 MASK FLAGWRD5 # IS 3-AXIS FLAG SET
016756,000055: 27,2025 10000 CCS A
016757,000056: 27,2026 12034 TCF TOBALLC # YES
016758,000057: 27,2027 06006 TC INTPRET
016759,000058: 27,2030 77624 CALL
016760,000059: 27,2031 56126 VECPOINT # TO COMPUTE FINAL ANGLES
016761,000060: 27,2032 01156 STORE CPHI # STORE ANGLES
016762,000061: 27,2033 77776 EXIT
016763,000062:
016764,000063: 27,2034 34371 TOBALLC CAF PRIO30 # IS MODE AUTO AND CTL GNC
016765,000064: # # Page 382
016766,000065: 27,2035 00006 EXTEND
016767,000066: 27,2036 06031 RXOR CHAN31
016768,000067: 27,2037 77707 MASK 13,14,15
016769,000068: 27,2040 00006 EXTEND
016770,000069: 27,2041 12043 BZF +2 # AUTO, NON-FLASH N18
016771,000070: 27,2042 12013 TCF TOBALL # NOT AUTO
016772,000071:
016773,000072: 27,2043 32125 CAF V06N18 # SET UP NON-FLASHING V06 N18
016774,000073: 27,2044 04555 TC BANKCALL
016775,000074: 27,2045 20602 CADR GODSPR
016776,000075: 27,2046 02056 TC CHKLINUS # TO CHECK FOR PRIORITY DISPLAYS
016777,000076:
016778,000077: 27,2047 04555 STARTMNV TC BANKCALL
016779,000078: 27,2050 17547 CADR GOMANUR
016780,000079: 27,2051 12013 ENDMANUV TCF TOBALL # FINISHED MANEUVER
016781,000080:
016782,000081: 27,2052 05447 ENDMANU1 TC DOWNFLAG # RESET 3-AXIS FLAG
016783,000082: 27,2053 00124 ADRES 3AXISFLG # BIT 6 FLAG 5
016784,000083: 27,2054 31146 CAE TEMPR60 # -
016785,000084: 27,2055 04577 TC BANKJUMP # -
016786,000085:
016787,000086: 27,2056 40100 CHKLINUS CS FLAGWRD4
016788,000087: 27,2057 74677 MASK BIT12 # IS PRIORITY DISPLAY FLAG SET -
016789,000088: 27,2060 10000 CCS A # -
016790,000089: 27,2061 00002 TC Q # NO - EXIT
016791,000090: 27,2062 30002 CA Q
016792,000091: 27,2063 54156 TS MPAC +2 # SAVE RETURN
016793,000092: 27,2064 46214 CS THREE # OBTAIN LOCATION FOR RESTART.
016794,000093: 27,2065 60133 AD BUF2 # HOLD Q OF LAST DISPALY
016795,000094: 27,2066 55053 TS TBASE1
016796,000095:
016797,000096: 27,2067 05301 TC PHASCHNG
016798,000097: 27,2070 00071 OCT 71 # 1.7SPOT FOR RELINUS
016799,000098: 27,2071 34704 CAF BIT7
016800,000099: 27,2072 05415 TC LINUS # GO SET BITS FOR PRIORITY DISPLAY -
016801,000100: 27,2073 00156 TC MPAC +2
016802,000101:
016803,000102: 27,2074 34706 RELINUS CAF BIT5 # IS TRACK FLAG ON
016804,000103: 27,2075 70075 MASK FLAGWRD1
016805,000104: 27,2076 00006 EXTEND
016806,000105: 27,2077 12111 BZF GOREDO20 # NO
016807,000106:
016808,000107: 27,2100 05435 TC UPFLAG
016809,000108: 27,2101 00077 ADRES PDSPFLAG # R60 PRIODSP FLAG
016810,000109:
016811,000110: 27,2102 05435 TC UPFLAG
016812,000111: 27,2103 00024 ADRES TARG1FLG # FOR R52
016813,000112:
016814,000113: 27,2104 34714 CAF ZERO # RESET TO ZERO, SINCE
016815,000114: # # Page 383
016816,000115: 27,2105 55303 TS OPTIND # OPTIND WAS SET TO -1 BY V379
016817,000116:
016818,000117: 27,2106 34761 CAF PRIO14 # RESTORE ORIGINAL PRIORITY
016819,000118: 27,2107 05103 TC PRIOCHNG
016820,000119:
016821,000120: 27,2110 01053 TC TBASE1
016822,000121:
016823,000122: 27,2111 05301 GOREDO20 TC PHASCHNG
016824,000123: 27,2112 00111 OCT 111 # 1.11 FOR PIKUP20
016825,000124:
016826,000125: 27,2113 05112 TC ENDOFJOB
016827,000126:
016828,000127: 27,2114 31011 R61TEST CA MODREG # ARE WE IN P00. IF YES THIS MUST BE
016829,000128: 27,2115 00006 EXTEND # VERB49 OR VERB89 SO DO ENDEXT.
016830,000129: 27,2116 12052 BZF ENDMANU1 # RESET 3-AXIS & RETURN. USER DOES ENDEXT
016831,000130: 27,2117 30100 CA FLAGWRD4 # ARE WE IN R61 (P20)
016832,000131: 27,2120 74677 MASK BIT12
016833,000132: 27,2121 00006 EXTEND
016834,000133: 27,2122 14106 BZF GOTOPOOH # NO
016835,000134: 27,2123 04550 TC GOTOV56 # YES
016836,000135:
016837,000136: 27,2124 20100 BIT14+7 OCT 20100 # -
016838,000137: 27,2125 01422 V06N18 VN 0618
016839,000138:
016840,000139: # # Page 384
016841,000140: # PROGRAM DESCRIPTION - VECPOINT
016842,000141:
016843,000142:
016844,000143: # THIS INTERPRETIVE SUBROUTINE MAY BE USED TO POINT A SPACECRAFT AXIS IN A DESIRED DIRECTION. THE AXIS
016845,000144: # TO BE POINTED MUST APPEAR AS A HALF UNIT DOUBLE PRECISION VECTOR IN SUCCESSIVE LOCATIONS OF ERASABLE MEMORY
016846,000145: # BEGINNING WITH THE LOCATION CALLED SCAXIS. THE COMPONENTS OF THIS VECTOR ARE GIVEN IN SPACECRAFT COORDINATES.
016847,000146: # THE DIRECTION IN WHICH THIS AXIS IS TO BE POINTED MUST APPEAR AS A HALF UNIT DOUBLE PRECISION VECTOR IN
016848,000147: # SUCCESSIVE LOCATIONS OF ERASABLE MEMORY BEGINNING WITH THE ADDRESS CALLED POINTVSM. THE COMPONENTS OF THIS
016849,000148: # VECTOR ARE GIVEN IN STABLE MEMBER COORDINATES. WITH THIS INFORMTION VECPOINT COMPUTES A SET OF THREE GIMBAL
016850,000149: # ANGLES (2S COMPLEMENT) CORRESPONDING TO THE CROSS-PRODUCT ROTATION BETWEEN SCAXIS AND POINTVSM AND STORES THEM
016851,000150: # IN T(MPAC) BEFORE RETURNING TO THE CALLER.
016852,000151: # THIS ROTATION, HOWEVER, MAY BRING THE S/C INTO GIMBAL LOCK. WHEN POINTING A VECTOR IN THE Y-Z PLANE,
016853,000152: # THE TRANSPONDER AXIS, OR THE AOT FOR THE LEM, THE PROGRAM WILL CORRECT THIS PROBLEM BY ROTATING THE CROSS-
016854,000153: # PRODUCT ATTITUDE ABOUT POINTVSM BY A FIXED AMOUNT SUFFICIENT TO ROTATE THE DESIRED S/C ATTITUDE OUT OF GIMBAL
016855,000154: # LOCK. IF THE AXIS TO BE POINTED IS MORE THAN 40.6 DEGREES BUT LESS THAN 60.5 DEG FROM THE +X (OR-X) AXIS,
016856,000155: # THE ADDITIONAL ROTATION TO AVOID GIMBAL LOCK IS 35 DEGREES. IF THE AXIS IS MORE THAN 60.5 DEGREES FROM +X (OR -X)
016857,000156: # THE ADDITIONAL ROTATION IS 35 DEGREES. THE GIMBAL ANGLES CORRESPONDING TO THIS ATTITUDE ARE THEN COMPUTED AND
016858,000157: # STORED AS 2S COMPLIMENT ANGLES IN T(MPAC) BEFORE RETURNING TO THE CALLER.
016859,000158: # WHEN POINTING THE X-AXIS, OR THE THRUST VECTOR, OR ANY VECTOR WITHIN 40.6 DEG OF THE X-AXIS, VECPOINT
016860,000159: # CANNOT CORRECT FOR A CROSS-PRODUCT ROTATION INTO GIMBAL LOCK. IN THIS CASE A PLATFORM REALIGNMENT WOULD BE
016861,000160: # REQUIRED TO POINT THE VECTOR IN THE DESIRED DIRECTION. AT PRESENT NO INDICATION IS GIVEN FOR THIS SITUATION
016862,000161: # EXCEPT THAT THE FINAL MIDDLE GIMBAL ANGLE IN MPAC +2 IS GREATER THAN 59 DEGREES.
016863,000162:
016864,000163: # CALLING SEQUENCE -
016865,000164: # 1) LOAD SCAXIS, POINTVSM
016866,000165: # 2) CALL
016867,000166: # VECPOINT
016868,000167:
016869,000168: # RETURNS WITH
016870,000169:
016871,000170: # 1) DESIRED OUTER GIMBAL ANGLE IN MPAC
016872,000171: # 2) DESIRED INNER GIMBAL ANGLE IN MPAC +1
016873,000172: # 3) DESIRED MIDDLE GIMBAL ANGLE IN MPAC +2
016874,000173:
016875,000174:
016876,000175: # ERASABLES USED -
016877,000176:
016878,000177: # 1) SCAXIS 6
016879,000178: # 2) POINTVSM 6
016880,000179: # 3) MIS 18
016881,000180: # 4) DEL 18
016882,000181: # 5) COF 6
016883,000182: # 6) VECQTEMP 1
016884,000183: # 7) ALL OF VAC AREA 43
016885,000184:
016886,000185: # TOTAL 99
016887,000186:
016888,000187:
016889,000188: 27,2000 SETLOC VECPT
016890,000189: 27,2000 BANK
016891,000190: # # Page 385
016892,000191: 27,2126 E6,1661 EBANK= BCDU
016893,000192:
016894,000193: 27,2126 COUNT 27/VECPT
016895,000194:
016896,000195: 27,2126 40020 VECPOINT STQ BOV # SAVE RETURN ADDRESS
016897,000196: 27,2127 03310 VECQTEMP
016898,000197: 27,2130 56131 VECLEAR # AND CLEAR OVFIND
016899,000198: 27,2131 47164 VECLEAR AXC,2 RTB
016900,000199: 27,2132 03320 MIS # READ THE PRESENT CDU ANGLES AND
016901,000200: 27,2133 44376 READCDUK # STORE THEM IN PD25, 26, 27
016902,000201: 27,2134 34032 STORANG STCALL 25D
016903,000202: 27,2135 44405 CDUTODCM # S/C AXES TO STABLE MEMBER AXES (MIS)
016904,000203: 27,2136 61375 VLOAD VXM
016905,000204: 27,2137 03357 POINTVSM # RESOLVE THE POINTING DIRECTION VF INTO
016906,000205: 27,2140 03321 MIS # INITIAL S/C AXES ( VF = POINTVSM)
016907,000206: 27,2141 77656 UNIT
016908,000207: 27,2142 00035 STORE 28D
016909,000208: # PD 28 29 30 31 32 33
016910,000209: 27,2143 53435 VXV UNIT # TAKE THE CROSS PRODUCT VF X VI
016911,000210: 27,2144 03351 SCAXIS # WHERE VI = SCAXIS
016912,000211: 27,2145 57400 BOV VCOMP
016913,000212: 27,2146 56256 PICKAXIS
016914,000213: 27,2147 17343 STODL COF # CHECK MAGNITUDE
016915,000214: 27,2150 00045 36D # OF CROSS PRODUCT
016916,000215: 27,2151 50025 DSU BMN # VECTOR, IF LESS
016917,000216: 27,2152 16327 DPB-14 # THAN B-14 ASSUME
016918,000217: 27,2153 56256 PICKAXIS # UNIT OPERATION
016919,000218: 27,2154 50375 VLOAD DOT # INVALID.
016920,000219: 27,2155 03351 SCAXIS
016921,000220: 27,2156 00035 28D
016922,000221: 27,2157 65552 SL1 ARCCOS
016923,000222: 27,2160 77624 COMPMATX CALL # NOW COMPUTE THE TRANSFORMATION FROM
016924,000223: 27,2161 44530 DELCOMP # FINAL S/C AXES TO INITIAL S/C AXES MFI
016925,000224: 27,2162 75160 AXC,1 AXC,2
016926,000225: 27,2163 03320 MIS # COMPUTE THE TRANSFORMATION FROM FINAL
016927,000226: 27,2164 03425 DEL # S/C AXES TO STABLE MEMBER AXES
016928,000227: 27,2165 77624 CALL # MFS = MIS MFI
016929,000228: 27,2166 44304 MXM3 # (IN PD LIST)
016930,000229:
016931,000230: 27,2167 51545 DLOAD ABS
016932,000231: 27,2170 00007 6 # MFS6 = SIN(CPSI) $2
016933,000232: 27,2171 50025 DSU BMN
016934,000233: 27,2172 16314 SINGIMLC # = SIN(59 DEGS) $2
016935,000234: 27,2173 56246 FINDGIMB # /CPSI/ LESS THAN 59 DEGS
016936,000235: # I.E. DESIRED ATTITUDE NOT IN GIMBAL LOCK
016937,000236:
016938,000237: 27,2174 51545 DLOAD ABS # CHECK TO SEE IF WE ARE POINTING
016939,000238: 27,2175 03351 SCAXIS # THE THRUST AXIS
016940,000239: 27,2176 51025 DSU BPL
016941,000240: 27,2177 16316 SINVEC1 # SIN 49.4 DEGS $2
016942,000241: # # Page 386
016943,000242: 27,2200 56246 FINDGIMB # IF SO, WE ARE TRYING TO POINT IT INTO
016944,000243: 27,2201 77775 VLOAD # GIMBAL LOCK, ABORT COULD GO HERE
016945,000244: 27,2202 77626 STADR
016946,000245: 27,2203 50442 STOVL MIS +12D
016947,000246: 27,2204 77626 STADR # STORE MFS (IN PD LIST) IN MIS
016948,000247: 27,2205 50450 STOVL MIS +6
016949,000248: 27,2206 77626 STADR
016950,000249: 27,2207 50456 STOVL MIS
016951,000250: 27,2210 03327 MIS +6 # INNER GIMBAL AXIS IN FINAL S/C AXES
016952,000251: 27,2211 57444 BPL VCOMP # LOCATE THE IG AXIS DIRECTION CLOSEST TO
016953,000252: 27,2212 56213 IGSAMEX # FINAL X S/C AXIS
016954,000253:
016955,000254: 27,2213 50035 IGSAMEX VXV BMN # FIND THE SHORTEST WAY OF ROTATING THE
016956,000255: 27,2214 03351 SCAXIS # S/C OUT OF GIMBAL LOCK BY A ROTATION
016957,000256: 27,2215 56222 U=SCAXIS # ABOUT +- SCAXIS, I.E. IF (IG (SGN MFS3)
016958,000257: # X SCAXIS . XF) LESS THAN 0, U = SCAXIS
016959,000258: # OTHERWISE U = -SCAXIS
016960,000259:
016961,000260: 27,2216 57575 VLOAD VCOMP
016962,000261: 27,2217 03351 SCAXIS
016963,000262: 27,2220 37343 STCALL COF # ROTATE ABOUT -SCAXIS
016964,000263: 27,2221 56225 CHEKAXIS
016965,000264: 27,2222 77775 U=SCAXIS VLOAD
016966,000265: 27,2223 03351 SCAXIS
016967,000266: 27,2224 03343 STORE COF # ROTATE ABOUT + SCAXIS
016968,000267: 27,2225 51545 CHEKAXIS DLOAD ABS
016969,000268: 27,2226 03351 SCAXIS # SEE IF WE ARE POINTING THE AOT
016970,000269: 27,2227 51025 DSU BPL
016971,000270: 27,2230 16320 SINVEC2 # SIN 29.5 DEGS $2
016972,000271: 27,2231 56235 PICKANG1 # IF SO, ROTATE 50 DEGS ABOUT +- SCAXIS
016973,000272: 27,2232 52145 DLOAD GOTO # IF NOT, MUST BE POINTING THE TRANSPONDER
016974,000273: 27,2233 16324 VECANG2 # OR SOME VECTOR IN THE Y, OR Z PLANE
016975,000274: 27,2234 56237 COMPMFSN # IN THIS CASE ROTATE 35 DEGS TO GET OUT
016976,000275: # OF GIMBAL LOCK (VECANG2 $360)
016977,000276: 27,2235 77745 PICKANG1 DLOAD
016978,000277: 27,2236 16322 VECANG1 # = 50 DEGS $ 360
016979,000278: 27,2237 77624 COMPMFSN CALL
016980,000279: 27,2240 44530 DELCOMP # COMPUTE THE ROTATION ABOUT SCAXIS TO
016981,000280: 27,2241 75160 AXC,1 AXC,2 # BRING MFS OUT OF GIMBAL LOCK
016982,000281: 27,2242 03320 MIS
016983,000282: 27,2243 03425 DEL
016984,000283: 27,2244 77624 CALL # COMPUTE THE NEW TRANSFORMATION FROM
016985,000284: 27,2245 44304 MXM3 # DESIRED S/C AXES TO STABLE MEMBER AXES
016986,000285: # WHICH WILL ALIGN VI WITH VF AND AVOID
016987,000286: # GIMBAL LOCK
016988,000287: 27,2246 45160 FINDGIMB AXC,1 CALL
016989,000288: 27,2247 00000 0 # EXTRACT THE COMMANDED CDU ANGLES FROM
016990,000289: 27,2250 44655 DCMTOCDU # THIS MATRIX
016991,000290: 27,2251 40234 RTB SETPD
016992,000291: 27,2252 45547 V1STO2S # CONVERT TO 2:S COMPLEMENT
016993,000292: # # Page 386
016994,000293: 27,2253 00001 0
016995,000294: 27,2254 77650 GOTO
016996,000295: 27,2255 03310 VECQTEMP # RETURN TO CALLER
016997,000296:
016998,000297: 27,2256 50375 PICKAXIS VLOAD DOT # IF VF X VI = 0, FIND VF . VI
016999,000298: 27,2257 00035 28D
017000,000299: 27,2260 03351 SCAXIS
017001,000300: 27,2261 72240 BMN TLOAD
017002,000301: 27,2262 56266 ROT180
017003,000302: 27,2263 00032 25D
017004,000303: 27,2264 77650 GOTO # IF VF = VI, CDU DESIRED = PRESENT CDU
017005,000304: 27,2265 03310 VECQTEMP # PRESENT CDU ANGLES
017006,000305:
017007,000306: 27,2266 47375 ROT180 VLOAD VXV # IF VF, VI ANTIPARALLEL, 180 DEG ROTATION
017008,000307: 27,2267 03327 MIS +6 # IS REQUIRED. Y STABLE MEMBER AXIS IN
017009,000308: 27,2270 15330 HIUNITX # INITIAL S/C AXIS.
017010,000309: 27,2271 47256 UNIT VXV # FIND Y(SM) X X(I)
017011,000310: 27,2272 03351 SCAXIS # FIND UNIT(VI X UNIT(Y(SM) X X(I)))
017012,000311: 27,2273 40056 UNIT BOV # I.E. PICK A VECTOR IN THE PLANE OF X(I),
017013,000312: 27,2274 56310 PICKX # Y(SM) PERPENDICULAR TO VI
017014,000313: 27,2275 17343 STODL COF
017015,000314: 27,2276 00045 36D # CHECK MAGNITUDE
017016,000315: 27,2277 50025 DSU BMN # OF THIS VECTOR.
017017,000316: 27,2300 16327 DPB-14 # IF LESS THAN B-14,
017018,000317: 27,2301 56310 PICKX # PICK X-AXIS.
017019,000318: 27,2302 77775 VLOAD
017020,000319: 27,2303 03343 COF
017021,000320: 27,2304 17343 XROT STODL COF
017022,000321: 27,2305 15330 HIDPHALF
017023,000322: 27,2306 77650 GOTO
017024,000323: 27,2307 56160 COMPMATX
017025,000324: 27,2310 52175 PICKX VLOAD GOTO # PICK THE XAXIS IN THIS CASE
017026,000325: 27,2311 15330 HIUNITX
017027,000326: 27,2312 56304 XROT
017028,000327: 35,2000 BANK 35
017029,000328: 27,2000 SETLOC MANUVER1
017030,000329: 27,2000 BANK
017031,000330:
017032,000331: 27,2313 15555 35172 SINGIMLC 2DEC .4285836003 # =SIN(59) $2
017033,000332: 27,2315 14113 36326 SINVEC1 2DEC .3796356537 # =SIN(49.4) $2
017034,000333: 27,2317 07701 35703 SINVEC2 2DEC .2462117800 # =SIN(29.5) $2
017035,000334: 27,2321 04343 21616 VECANG1 2DEC .1388888889 # = 50 DEGREES $360
017036,000335: 27,2323 03070 34344 VECANG2 2DEC .09722222222 # = 35 DEGREES $360
017037,000336: 27,2325 00000 1BITDP OCT 0 # KEEP THIS BEFORE DPB(-14) *********
017038,000337: 27,2326 00001 DPB-14 OCT 00001
017039,000338: # # Page 388
017040,000339: 27,2327 00000 OCT 00000
017041,000340: 34,2002 BANK 34
017042,000341: 27,2000 SETLOC MANUVER
017043,000342: 27,2000 BANK
017044,000343:
017045,000344: # # Page 389
017046,000345: # ROUTINE FOR INITIATING AUTOMATIC MANEUVER VIA KEYBOARD (V49)
017047,000346:
017048,000347:
017049,000348: 27,2330 1155 EBANK= CPHI
017050,000349:
017051,000350: 27,2330 COUNT 27/R62
017052,000351:
017053,000352: 27,2330 34745 R62DISP CAF V06N22 # DISPLAY COMMAND ICDUS CPHI, CTHETA, CPHI
017054,000353: 27,2331 04555 TC BANKCALL
017055,000354: 27,2332 20624 CADR GOFLASH
017056,000355: 27,2333 15423 TCF ENDEXT
017057,000356: 27,2334 12336 TCF GOMOVE # PROCEED
017058,000357: 27,2335 12330 TCF R62DISP # ENTER
017059,000358:
017060,000359:
017061,000360: # ASTRONAUT MAY LOAD NEW ICDUS AT THIS
017062,000361: # POINT
017063,000362: 27,2336 05435 GOMOVE TC UPFLAG # SET 3-AXIS FLAG
017064,000363: 27,2337 00124 ADRES 3AXISFLG # BIT 6 FLAG 5
017065,000364:
017066,000365: 27,2340 04555 TC BANKCALL
017067,000366: 27,2341 56000 CADR R60CSM
017068,000367: 27,2342 15423 TCF ENDEXT
End of include-file R60,R62.agc. Parent file is MAIN.agc