Source Code
016931,000001: # Copyright: Public domain.
016932,000002: # Filename: R60_62.agc
016933,000003: # Purpose: Part of the source code for Colossus 2A, AKA Comanche 055.
016934,000004: # It is part of the source code for the Command Module's (CM)
016935,000005: # Apollo Guidance Computer (AGC), for Apollo 11.
016936,000006: # Assembler: yaYUL
016937,000007: # Contact: Ron Burkey <info@sandroid.org>.
016938,000008: # Website: www.ibiblio.org/apollo.
016939,000009: # Pages: 390-398
016940,000010: # Mod history: 2009-05-09 RSB Adapted from the Colossus249/ file
016941,000011: # of the same name, using Comanche055 page
016942,000012: # images.
016943,000013:
016944,000014: # This source code has been transcribed or otherwise adapted from digitized
016945,000015: # images of a hardcopy from the MIT Museum. The digitization was performed
016946,000016: # by Paul Fjeld, and arranged for by Deborah Douglas of the Museum. Many
016947,000017: # thanks to both. The images (with suitable reduction in storage size and
016948,000018: # consequent reduction in image quality as well) are available online at
016949,000019: # www.ibiblio.org/apollo. If for some reason you find that the images are
016950,000020: # illegible, contact me at info@sandroid.org about getting access to the
016951,000021: # (much) higher-quality images which Paul actually created.
016952,000022:
016953,000023: # Notations on the hardcopy document read, in part:
016954,000024:
016955,000025: # Assemble revision 055 of AGC program Comanche by NASA
016956,000026: # 2021113-051. 10:28 APR. 1, 1969
016957,000027:
016958,000028: # This AGC program shall also be referred to as
016959,000029: # Colossus 2A
016960,000030:
016961,000031: # Page 390
016962,000032: 34,2002 BANK 34
016963,000033: 27,2000 SETLOC MANUVER
016964,000034: 27,2000 BANK
016965,000035:
016966,000036: 27,2000 1146 EBANK= TEMPR60
016967,000037:
016968,000038: 27,2000 COUNT 27/R60
016969,000039:
016970,000040: # CONFORMS TO GSOP CHAPTER FOUR REVISION LOGIC 09 JAN 18, 1968
016971,000041:
016972,000042: 27,2000 04711 R60CSM TC MAKECADR
016973,000043: 27,2001 55146 TS TEMPR60
016974,000044:
016975,000045: # INSERT PRIODSP CHECK WITH R22 (V06N49) WITH JENNINGS BRODEUR
016976,000046:
016977,000047: 27,2002 35012 REDOMANN CAF BIT6
016978,000048: 27,2003 70101 MASK FLAGWRD5 # IS 3-AXIS FLAG SET
016979,000049: 27,2004 10000 CCS A
016980,000050: 27,2005 12013 TCF TOBALL # YES
016981,000051: 27,2006 06006 TC INTPRET
016982,000052: 27,2007 77624 CALL
016983,000053: 27,2010 56126 VECPOINT # TO COMPUTE FINAL ANGLES
016984,000054: 27,2011 01156 STORE CPHI # STORE FINAL ANGLES -- CPHI, CTHETA, CPSI
016985,000055: 27,2012 77776 EXIT
016986,000056:
016987,000057: 27,2013 32125 TOBALL CAF V06N18
016988,000058: 27,2014 04662 TC BANKCALL
016989,000059: 27,2015 21132 CADR GOPERF2R # DISPLAY PLEASE PERFORM AUTO MANEUVER
016990,000060: 27,2016 02114 TC R61TEST
016991,000061: 27,2017 02023 TC REDOMANC # PROCEED
016992,000062: 27,2020 12052 TCF ENDMANU1 # ENTER I.E., FINISHED WITH R60
016993,000063:
016994,000064: 27,2021 02056 TC CHKLINUS # TO CHECK FOR PRIORITY DISPLAYS
016995,000065: 27,2022 05217 TC ENDOFJOB
016996,000066:
016997,000067: 27,2023 35012 REDOMANC CAF BIT6
016998,000068: 27,2024 70101 MASK FLAGWRD5 # IS 3-AXIS FLAG SET
016999,000069: 27,2025 10000 CCS A
017000,000070: 27,2026 12034 TCF TOBALLC # YES
017001,000071: 27,2027 06006 TC INTPRET
017002,000072: 27,2030 77624 CALL
017003,000073: 27,2031 56126 VECPOINT # TO COMPUTE FINAL ANGLES
017004,000074: 27,2032 01156 STORE CPHI # STORE ANGLES
017005,000075: 27,2033 77776 EXIT
017006,000076:
017007,000077: 27,2034 34371 TOBALLC CAF PRIO30 # IS MODE AUTO AND CTL GNC
017008,000078: # Page 391
017009,000079: 27,2035 00006 EXTEND
017010,000080: 27,2036 06031 RXOR CHAN31
017011,000081: 27,2037 77707 MASK 13,14,15
017012,000082: 27,2040 00006 EXTEND
017013,000083: 27,2041 12043 BZF +2 # AUTO, NON-FLASH N18
017014,000084: 27,2042 12013 TCF TOBALL # NOT AUTO
017015,000085:
017016,000086: 27,2043 32125 CAF V06N18 # STATIC UP NON-FLASHING V06 N18
017017,000087: 27,2044 04662 TC BANKCALL
017018,000088: 27,2045 20676 CADR GODSPR
017019,000089: 27,2046 02056 TC CHKLINUS
017020,000090:
017021,000091: 27,2047 04662 STARTMNV TC BANKCALL
017022,000092: 27,2050 17627 CADR GOMANUR
017023,000093: 27,2051 12013 ENDMANUV TCF TOBALL # FINISHED MANEUVER.
017024,000094:
017025,000095: 27,2052 05560 ENDMANU1 TC DOWNFLAG # RESET 3-AXIS FLAG
017026,000096: 27,2053 00124 ADRES 3AXISFLG # BIT 6 FLAG 5
017027,000097: 27,2054 31146 CAE TEMPR60
017028,000098: 27,2055 04704 TC BANKJUMP
017029,000099:
017030,000100: 27,2056 40100 CHKLINUS CS FLAGWRD4
017031,000101: 27,2057 75004 MASK BIT12 # IS PRIORITY DISPLAY FLAG SET?
017032,000102: 27,2060 10000 CCS A
017033,000103: 27,2061 00002 TC Q # NO -- EXIT
017034,000104: 27,2062 30002 CA Q
017035,000105: 27,2063 54156 TS MPAC +2 # SAVE RETURN
017036,000106: 27,2064 46214 CS THREE # OBTAIN LOCATION FOR RESTART
017037,000107: 27,2065 60133 AD BUF2 # HOLD Q OF LAST DISPLAY
017038,000108: 27,2066 55053 TS TBASE1
017039,000109:
017040,000110: 27,2067 05412 TC PHASCHNG
017041,000111: 27,2070 00071 OCT 71 # 1.7SPOT FOR RELINUS
017042,000112:
017043,000113: 27,2071 35011 CAF BIT7
017044,000114: 27,2072 05526 TC LINUS # GO SET BITS FOR PRIORITY DISPLAY
017045,000115: 27,2073 00156 TC MPAC +2
017046,000116:
017047,000117: 27,2074 35013 RELINUS CAF BIT5 # IS TRACK FLAG ON
017048,000118: 27,2075 70075 MASK FLAGWRD1
017049,000119: 27,2076 00006 EXTEND
017050,000120: 27,2077 12111 BZF GOREDO20 # NO
017051,000121:
017052,000122: 27,2100 05546 TC UPFLAG
017053,000123: 27,2101 00077 ADRES PDSPFLAG # R60 PRIODSP FLAG
017054,000124:
017055,000125: 27,2102 05546 TC UPFLAG
017056,000126: 27,2103 00024 ADRES TARG1FLG # FOR R52
017057,000127:
017058,000128: 27,2104 35021 CAF ZERO # RESET TO ZERO, SINCE
017059,000129: # Page 392
017060,000130: 27,2105 55303 TS OPTIND # OPTIND WAS SET TO -1 BY V379
017061,000131:
017062,000132: 27,2106 35066 CAF PRIO14 # RESTORE ORIGINAL PRIORITY
017063,000133: 27,2107 05210 TC PRIOCHNG
017064,000134:
017065,000135: 27,2110 01053 TC TBASE1
017066,000136:
017067,000137: 27,2111 05412 GOREDO20 TC PHASCHNG
017068,000138: 27,2112 00111 OCT 111 # 1.11 FOR PIKUP20
017069,000139:
017070,000140: 27,2113 05217 TC ENDOFJOB
017071,000141:
017072,000142: 27,2114 31011 R61TEST CA MODREG # ARE WE IN P00. IF YES THIS MUST BE
017073,000143: 27,2115 00006 EXTEND # VERB49 OR VERB89 SO DO ENDEXT.
017074,000144: 27,2116 12052 BZF ENDMANU1 # RESET 3-AXIS & RETURN. USER DOES ENDEXT
017075,000145: 27,2117 30100 CA FLAGWRD4 # ARE WE IN R61 (P20)
017076,000146: 27,2120 75004 MASK BIT12
017077,000147: 27,2121 00006 EXTEND
017078,000148: 27,2122 14106 BZF GOTOP00H # NO
017079,000149: 27,2123 04622 TC GOTOV56 # YES
017080,000150:
017081,000151: 27,2124 20100 BIT14+7 OCT 20100
017082,000152: 27,2125 01422 V06N18 VN 0618
017083,000153:
017084,000154: # Page 393
017085,000155: # PROGRAM DESCRIPTION -- VECPOINT
017086,000156:
017087,000157: # THIS INTERPRETIVE SUBROUTINE MAY BE USED TO POINT A SPACECRAFT AXIS IN A DESIRED DIRECTION. THE AXIS
017088,000158: # TO BE POINTED MUST APPEAR AS A HALF UNIT DOUBLE PRECISION VECTOR IN SUCCESSIVE LOCATIONS OF ERASABLE MEMORY
017089,000159: # BEGINNING WITH THE LOCATION CALLED SCAXIS. THE COMPONENTS OF THIS VECTOR ARE GIVEN IN SPACECRAFT COORDINATES.
017090,000160: # THE DIRECTION IN WHICH THIS AXIS IS TO BE POINTED MUST APPEAR AS A HALF UNIT DOUBLE PRECISION VECTOR IN
017091,000161: # SUCCESSIVE LOCATIONS OF ERASABLE MEMORY BEGINNING WITH THE ADDRESS CALLED POINTVSM. THE COMPONENTS OF THIS
017092,000162: # VECTOR ARE GIVEN IN STABLE MEMBER COORDINATES. WITH THIS INFORMTION VECPOINT COMPUTES A SET OF THREE GIMBAL
017093,000163: # ANGLES (2'S COMPLEMENT) CORRESPONDING TO THE CROSS-PRODUCT ROTATION BETWEEN SCAXIS AND POINTVSM AND STORES THEM
017094,000164: # IN T(MPAC) BEFORE RETURNING TO THE CALLER.
017095,000165:
017096,000166: # THIS ROTATION, HOWEVER, MAY BRING THE S/C INTO GIMBAL LOCK. WHEN POINTING A VECTOR IN THE Y-Z PLANE,
017097,000167: # THE TRANSPONDER AXIS, OR THE AOT FOR THE LEM, THE PROGRAM WILL CORRECT THIS PROGLEM BY ROTATING THE CROSS-
017098,000168: # PRODUCT ATTITUDE ABOUT POINTVSM BY A FIXED AMOUNT SUFFICIENT TO ROTATE THE DESIRED S/C ATTITUDE OUT OF GIMBAL
017099,000169: # 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,
017100,000170: # THE ADDITIONAL ROTATION TO AVOID GIMBAL LOCK IS 35 DEGREES. IF THE AXIS IS MORE THAN 60.5 DEGREES FROM +X (OR -X)
017101,000171: # THE ADDITIONAL ROTATION IS 35 DEGREES. THE GIMBAL ANGLES CORRESPONDING TO THIS ATTITUDE ARE THEN COMPUTED AND
017102,000172: # STORED AS 2'S COMPLEMENT ANGLES N T(MPAC) BEFORE RETURNING TO THE CALLER.
017103,000173:
017104,000174: # WHEN POINTING THE X-AXIS, OR THE THRUST VECTOR, OR ANY VECTOR WITHIN 40.6 DEG OF THE X-AXIS, VECPOINT
017105,000175: # CANNOT CORRECT FOR A CROSS-PRODUCT ROTATION INTO GIMBAL LOCK. IN THIS CASE A PLATFORM REALIGNMENT WOULD BE
017106,000176: # REQUIRED TO POINT THE VECTOR IN THE DESIRED DIRECTION. AT PRESENT NO INDICATION IS GIVEN FOR THIS SITUATION
017107,000177: # EXCEPT THAT THE FINAL MIDDLE GIMBAL ANGLE IN MPAC +2 IS GREATER THAN 59 DEGREES.
017108,000178:
017109,000179: # CALLING SEQUENCE
017110,000180:
017111,000181: # 1) LOAD SCAXIS, POINTVSM
017112,000182: # 2) CALL
017113,000183: # VECPOINT
017114,000184:
017115,000185: # RETURNS WITH
017116,000186:
017117,000187: # 1) DESIRED OUTER GIMBAL ANGLE IN MPAC
017118,000188: # 2) DESIRED INNER GIMBAL ANGLE IN MPAC +1
017119,000189: # 3) DESIRED MIDDLE GIMBAL ANGLE IN MPAC +2
017120,000190:
017121,000191: # ERASABLES USED --
017122,000192:
017123,000193: # 1) SCAXIS 6
017124,000194: # 2) POINTVSM 6
017125,000195: # 3) MIS 18
017126,000196: # 4) DEL 18
017127,000197: # 5) COF 6
017128,000198: # 6) VECQTEMP 1
017129,000199: # 7) ALL OF VAC AREA 43
017130,000200:
017131,000201: # TOTAL 99
017132,000202:
017133,000203: 27,2000 SETLOC VECPT
017134,000204: 27,2000 BANK
017135,000205: # Page 394
017136,000206: 27,2126 E6,1661 EBANK= BCDU
017137,000207:
017138,000208: 27,2126 COUNT 27/VECPT
017139,000209:
017140,000210: 27,2126 40020 VECPOINT STQ BOV # SAVE RETURN ADDRESS
017141,000211: 27,2127 03310 VECQTEMP
017142,000212: 27,2130 56131 VECLEAR # AND CLEAR OVFIND
017143,000213: 27,2131 47164 VECLEAR AXC,2 RTB
017144,000214: 27,2132 03320 MIS # READ THE PRESENT CDU ANGLES AND
017145,000215: 27,2133 44376 READCDUK # STORE THEM IN PD25, 26, 27
017146,000216: 27,2134 34032 STCALL 25D
017147,000217: 27,2135 44405 CDUTODCM # S/C AXES TO STABLE MEMBER AXES (MIS)
017148,000218: 27,2136 61375 VLOAD VXM
017149,000219: 27,2137 03357 POINTVSM # RESOLVE THE POINTING DIRECTION VF INTO
017150,000220: 27,2140 03321 MIS # INITIAL S/C AXES (VF = POINTVSM)
017151,000221: 27,2141 77656 UNIT
017152,000222: 27,2142 00035 STORE 28D
017153,000223: # PD 28 29 30 31 32 33
017154,000224: 27,2143 53435 VXV UNIT # TAKE THE CROSS PRODUCT VF X VI
017155,000225: 27,2144 03351 SCAXIS # WHERE VI = SCAXIS
017156,000226: 27,2145 57400 BOV VCOMP
017157,000227: 27,2146 56256 PICKAXIS
017158,000228: 27,2147 17343 STODL COF # CHECK MAGNITUDE
017159,000229: 27,2150 00045 36D # OF CROSS PRODUCT
017160,000230: 27,2151 50025 DSU BMN # VECTOR, IF LESS
017161,000231: 27,2152 16327 DPB-14 # THAN B-14 ASSUME
017162,000232: 27,2153 56256 PICKAXIS # UNIT OPERATION
017163,000233: 27,2154 50375 VLOAD DOT # INVALID.
017164,000234: 27,2155 03351 SCAXIS
017165,000235: 27,2156 00035 28D
017166,000236: 27,2157 65552 SL1 ARCCOS
017167,000237: 27,2160 77624 COMPMATX CALL # NO COMPUTE THE TRANSFORMATION FROM
017168,000238: 27,2161 44530 DELCOMP # FINAL S/C AXES TO INITIAL S/C AXES MFI
017169,000239: 27,2162 75160 AXC,1 AXC,2
017170,000240: 27,2163 03320 MIS # COMPUTE THE TRANSFORMATION FROM FINAL
017171,000241: 27,2164 03425 DEL # S/C AXES TO STABLE MEMBER AXES
017172,000242: 27,2165 77624 CALL # MFS = MIS MFI
017173,000243: 27,2166 44304 MXM3 # (IN PD LIST)
017174,000244:
017175,000245: 27,2167 51545 DLOAD ABS
017176,000246: 27,2170 00007 6 # MFS6 = SIN(CPSI) $2
017177,000247: 27,2171 50025 DSU BMN
017178,000248: 27,2172 16314 SINGIMLC # = SIN(59 DEGS) $2
017179,000249: 27,2173 56246 FINDGIMB # /CPSI/ LESS THAN 59 DEGS.
017180,000250: # I.E., DESIRED ATTITUDE NOT IN GIMBAL LOCK
017181,000251:
017182,000252: 27,2174 51545 DLOAD ABS # CHECK TO SEE IF WE ARE POINTING
017183,000253: 27,2175 03351 SCAXIS # THE THRUST AXIS
017184,000254: 27,2176 51025 DSU BPL
017185,000255: 27,2177 16316 SINVEC1 # SIN 49.4 DEGS $2
017186,000256: # Page 395
017187,000257: 27,2200 56246 FINDGIMB # IF SO, WE ARE TRYING TO POINT IT INTO
017188,000258: 27,2201 77775 VLOAD # GIMBAL LOCK, ABORT COULD GO HERE
017189,000259: 27,2202 77626 STADR
017190,000260: 27,2203 50442 STOVL MIS +12D
017191,000261: 27,2204 77626 STADR # STORE MFS (IN PD LIST) IN MIS
017192,000262: 27,2205 50450 STOVL MIS +6
017193,000263: 27,2206 77626 STADR
017194,000264: 27,2207 50456 STOVL MIS
017195,000265: 27,2210 03327 MIS +6 # INNER GIMBAL AXIS IN FINAL S/C AXES
017196,000266: 27,2211 57444 BPL VCOMP # LOCATE THE IG AXIS DIRECTION CLOSEST TO
017197,000267: 27,2212 56213 IGSAMEX # FINAL X S/C AXIS
017198,000268:
017199,000269: 27,2213 50035 IGSAMEX VXV BMN # FIND THE SHORTEST WAY OF ROTATING THE
017200,000270: 27,2214 03351 SCAXIS # S/C OUT OF GIMBAL LOCK BY A ROTATION
017201,000271: 27,2215 56222 U=SCAXIS # ABOUT +- SCAXIS, I.E., IF (IG (SGN MFS3)
017202,000272: # X SCAXIS . XF) LESS THAN Q, U = SCAXIS
017203,000273: # OTHERWISE U = -SCAXIS.
017204,000274:
017205,000275: 27,2216 57575 VLOAD VCOMP
017206,000276: 27,2217 03351 SCAXIS
017207,000277: 27,2220 37343 STCALL COF # ROTATE ABOUT -SCAXIS
017208,000278: 27,2221 56225 CHEKAXIS
017209,000279: 27,2222 77775 U=SCAXIS VLOAD
017210,000280: 27,2223 03351 SCAXIS
017211,000281: 27,2224 03343 STORE COF # ROTATE ABOUT + SCAXIS
017212,000282: 27,2225 51545 CHEKAXIS DLOAD ABS
017213,000283: 27,2226 03351 SCAXIS # SEE IF WE ARE POINTING THE AOT
017214,000284: 27,2227 51025 DSU BPL
017215,000285: 27,2230 16320 SINVEC2 # SIN 29.5 DEGS $2
017216,000286: 27,2231 56235 PICKANG1 # IF SO, ROTATE 50 DEGS ABOUT +- SCAXIS
017217,000287: 27,2232 52145 DLOAD GOTO # IF NOT, MUST BE POINTING THE TRANSPONDER
017218,000288: 27,2233 16324 VECANG2 # OR SOME VECTOR IN THE Y, OR Z PLANE
017219,000289: 27,2234 56237 COMPMFSN # IN THIS CASE ROTATE 35 DEGS TO GET OUT
017220,000290: # OF GIMBAL LOCK (VECANG2 $360)
017221,000291: 27,2235 77745 PICKANG1 DLOAD
017222,000292: 27,2236 16322 VECANG1 # = 50 DEGS. $360
017223,000293: 27,2237 77624 COMPMFSN CALL
017224,000294: 27,2240 44530 DELCOMP # COMPUTE THE ROTATION ABOUT SCAXIS TO
017225,000295: 27,2241 75160 AXC,1 AXC,2 # BRING MFS OUT OF GIMBAL LOCK
017226,000296: 27,2242 03320 MIS
017227,000297: 27,2243 03425 DEL
017228,000298: 27,2244 77624 CALL # COMPUTE THE NEW TRANSFORMATION FROM
017229,000299: 27,2245 44304 MXM3 # DESIRED S/C AXES TO STABLE MEMBER AXES
017230,000300: # WHICH WILL ALIGN VI WITH VF AND AVOID
017231,000301: # GIMBAL LOCK
017232,000302: 27,2246 45160 FINDGIMB AXC,1 CALL
017233,000303: 27,2247 00000 0 # EXTRACT THE COMMANDED CDU ANGLES FROM
017234,000304: 27,2250 44655 DCMTOCDU # THIS MATRIX
017235,000305: 27,2251 40234 RTB SETPD
017236,000306: 27,2252 45552 V1STO2S # CONVERT TO 2'S COMPLEMENT
017237,000307: # Page 396
017238,000308: 27,2253 00001 0
017239,000309: 27,2254 77650 GOTO
017240,000310: 27,2255 03310 VECQTEMP # RETURN TO CALLER
017241,000311:
017242,000312: 27,2256 50375 PICKAXIS VLOAD DOT # IF VF X VI = 0, FIND VF, VI
017243,000313: 27,2257 00035 28D
017244,000314: 27,2260 03351 SCAXIS
017245,000315: 27,2261 72240 BMN TLOAD
017246,000316: 27,2262 56266 ROT180
017247,000317: 27,2263 00032 25D
017248,000318: 27,2264 77650 GOTO # IF VF = VI, CDU DESIRED = PRESENT CDU
017249,000319: 27,2265 03310 VECQTEMP # PRESENT CDU ANGLES
017250,000320:
017251,000321: 27,2266 47375 ROT180 VLOAD VXV # IF VF, VI ANTI-PARALLEL, 180 DEG ROTATION
017252,000322: 27,2267 03327 MIS +6 # IS REQUIRED. Y STABLE MEMBER AXIS IN
017253,000323: 27,2270 15333 HIUNITX # INITIAL S/C AXES.
017254,000324: 27,2271 47256 UNIT VXV # FIND Y(SM) X X(I)
017255,000325: 27,2272 03351 SCAXIS # FIND UNIT(VI X UNIT(Y(SM) X X(I)))
017256,000326: 27,2273 40056 UNIT BOV # I.E., PICK A VECTOR IN THE PLANE OF X(I),
017257,000327: 27,2274 56310 PICKX # Y(SM) PERPENDICULAR TO VI
017258,000328: 27,2275 17343 STODL COF
017259,000329: 27,2276 00045 36D # CHECK MAGNITUDE
017260,000330: 27,2277 50025 DSU BMN # OF THIS VECTOR.
017261,000331: 27,2300 16327 DPB-14 # IF LESS THAN B-14,
017262,000332: 27,2301 56310 PICKX # PICK X-AXIS.
017263,000333: 27,2302 77775 VLOAD
017264,000334: 27,2303 03343 COF
017265,000335: 27,2304 17343 XROT STODL COF
017266,000336: 27,2305 15333 HIDPHALF
017267,000337: 27,2306 77650 GOTO
017268,000338: 27,2307 56160 COMPMATX
017269,000339: 27,2310 52175 PICKX VLOAD GOTO # PICK THE XAXIS IN THIS CASE
017270,000340: 27,2311 15333 HIUNITX
017271,000341: 27,2312 56304 XROT
017272,000342: 35,2000 BANK 35
017273,000343: 27,2000 SETLOC MANUVER1
017274,000344: 27,2000 BANK
017275,000345:
017276,000346: 27,2313 15555 35172 SINGIMLC 2DEC .4285836003 # = SIN(59) $2
017277,000347:
017278,000348: 27,2315 14113 36326 SINVEC1 2DEC .3796356537 # = SIN(49.4) $2
017279,000349:
017280,000350: 27,2317 07701 35703 SINVEC2 2DEC .2462117800 # = SIN(29.5) $2
017281,000351:
017282,000352: 27,2321 04343 21616 VECANG1 2DEC .1388888889 # = 50 DEGREES $360
017283,000353:
017284,000354: 27,2323 03070 34344 VECANG2 2DEC .09722222222 # = 35 DEGREES $360
017285,000355:
017286,000356:
017287,000357: 27,2325 00000 1BITDP OCT 0 # KEEP THIS BEFORE DPB(-14) ********
017288,000358: 27,2326 00001 DPB-14 OCT 00001
017289,000359: # Page 397
017290,000360: 27,2327 00000 OCT 00000
017291,000361: 34,2002 BANK 34
017292,000362: 27,2000 SETLOC MANUVER
017293,000363: 27,2000 BANK
017294,000364:
017295,000365: # Page 398
017296,000366: # ROUTINE FOR INITIATING AUTOMATIC MANEUVER VIA KEYBOARD (V49)
017297,000367:
017298,000368: 27,2330 1155 EBANK= CPHI
017299,000369:
017300,000370: 27,2330 COUNT 27/R62
017301,000371:
017302,000372: 27,2330 35052 R62DISP CAF V06N22 # DISPLAY COMMAND ICDUS CPHI, CTHETA, CPHI
017303,000373: 27,2331 04662 TC BANKCALL
017304,000374: 27,2332 20720 CADR GOFLASH
017305,000375: 27,2333 15534 TCF ENDEXT
017306,000376: 27,2334 12336 TCF GOMOVE # PROCEED
017307,000377: 27,2335 12330 TCF R62DISP # ENTER
017308,000378:
017309,000379: # ASTRONAUT MAY LOAD NEW ICDUS AT THIS
017310,000380: # POINT.
017311,000381: 27,2336 05546 GOMOVE TC UPFLAG # SET FOR 3-AXIS MANEUVER
017312,000382: 27,2337 00124 ADRES 3AXISFLG
017313,000383:
017314,000384: 27,2340 04662 TC BANKCALL
017315,000385: 27,2341 56000 CADR R60CSM
017316,000386: 27,2342 15534 TCF ENDEXT
017317,000387:
End of include-file R60_62.agc. Parent file is MAIN.agc