Source Code
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These source-code files are part of a reconstructed copy of Artemis 071, the
first release of the Apollo 15 through 17 Command Module (CM) Apollo Guidance
Computer (AGC) software.
The reconstruction began with source code of Artemis 072 previously transcribed
from a digitized copy of that program. The code was then updated by undoing
changes between the two versions. The reconstruction was verified by matching
memory-bank checksums to those listed in drawing 2021154-. Note that page
numbers in the reconstructed code match those on the Artemis 072 printout,
although the changed code would likely have changed page numbers for a real
Artemis 071 listing.
Comments from 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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053923,000002: ## Copyright: Public domain.
053924,000003: ## Filename: CONIC_SUBROUTINES.agc
053925,000004: ## Purpose: A section of Artemis revision 071.
053926,000005: ## It is part of the reconstructed source code for the first
053927,000006: ## release of the flight software for the Command Module's
053928,000007: ## (CM) Apollo Guidance Computer (AGC) for Apollo 15 through
053929,000008: ## 17. The code has been recreated from a copy of Artemis 072.
053930,000009: ## It has been adapted such that the resulting bugger words
053931,000010: ## exactly match those specified for Artemis 071 in NASA
053932,000011: ## drawing 2021154-, which gives relatively high confidence
053933,000012: ## that the reconstruction is correct.
053934,000013: ## Reference: 1262
053935,000014: ## Assembler: yaYUL
053936,000015: ## Contact: Ron Burkey <info@sandroid.org>.
053937,000016: ## Website: www.ibiblio.org/apollo/index.html
053938,000017: ## Mod history: 2019-08-14 MAS Created from Artemis 072.
053939,000018:
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Page 1262
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053941,000020:
053942,000021: # PROGRAM DESCRIPTION - ENTIRE CONIC SUBROUTINE LOG SECTION DATE - 1 SEPTEMBER 1967
053943,000022: # MOD NO. - 0 LOG SECTION - CONIC SUBROUTINES
053944,000023: # MOD BY KRAUSE ASSEMBLY - COLOSSUS REVISION 88
053945,000024:
053946,000025:
053947,000026:
053948,000027: # FUNCTIONAL DESCRIPTION -
053949,000028:
053950,000029: # THE FOLLOWING SET OF SUBROUTINES SOLVE VARIOUS PROBLEMS INVOLVING THE TRAJECTORY PRODUCED BY A CENTRAL
053951,000030: # INVERSE-SQUARE FORCE ACTING ON A POINT MASS, AS OUTLINED IN THE CMC AND LGC LUNAR LANDING MISSION GSOP, SECTION
053952,000031: # 5.5.1.2. A GENERAL USAGE POINT-OF-VIEW WAS TAKEN IN FORMULATING, MECHANIZING, AND SCALING THE SUBROUTINES,
053953,000032: # RATHER THAN OPTIMIZING EACH FOR A PARTICULAR USE. THEREFORE, MULTIPLE USAGE CAN BE MADE OF THE SUBROUTINES
053954,000033: # INVOLVING ANY REALISTIC SET OF CONSTRAINTS. IT SHOULD BE NOTED THAT ONLY ONE SET OF CODING IS USED, WHETHER THE
053955,000034: # EARTH, MOON, OR ANY OTHER CELESTIAL BODY IS SPECIFIED AS THE CENTRAL BODY OF THE PROBLEM, PROVIDED ONE OBSERVES
053956,000035: # THE INHERENT SCALE CHANGE REQUIRED IN POSITION, VELOCITY, MU, AND TIME, AS OUTLINED IN MISSION PROGRAMMING
053957,000036: # DEFINITION MEMO NO. 10. THIS CAN BE ACCOMPLISHED BY SIMPLY ADDING TO THE MUTABLE AND INITIALIZING THE SUBROU-
053958,000037: # TINES APPROPRIATELY.
053959,000038:
053960,000039: # DUE TO THE UNIFORMITY OF THE EQUATIONS INVOLVED, CODING WAS MINIMIZED BY TREATING INDIVIDUAL EQUATIONS AND
053961,000040: # BLOCKS OF EQUATIONS AS SUBROUTINES OF LOWER RANK WHENEVER POSSIBLE. AS A RESULT, THREE BY-PRODUCTS SUBROUTINES,
053962,000041: # DIRECTLY USABLE AS INDEPENDENT SUBROUTINES, WERE GENERATED.
053963,000042:
053964,000043:
053965,000044: # RESTRICTIONS -
053966,000045:
053967,000046: # THE ONLY LIMITATION IN THE SCOPE OF PROBLEM WHICH CAN BE SOLVED BY A PARTICULAR SUBROUTINE IS THE SCALING
053968,000047: # LIMIT OF EACH PARAMETER AS SPECIFIED IN THE GSOP. THESE SCALING LIMITS WERE CHOSEN SO THAT ALL FEASIBLE TRAJEC-
053969,000048: # TORIES COULD BE HANDLED.
053970,000049: # SINCE THE SUBROUTINES (EXCEPT KEPLER) USE COMMON SUBROUTINES OF LOWER RANK WHICH USE ERASABLE OTHER THAN
053971,000050: # THE PUSHLIST (DUE TO ITS LIMITED SIZE) AND COMMON INTERPRETIVE SWITCHES, THE CONIC SUBROUTINES CANNOT BE ALLOWED
053972,000051: # TO INTERRUPT EACH OTHER. IT IS UP TO THE USER TO GUARANTEE THIS CONDITION.
053973,000052:
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Page 1263
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053975,000054:
053976,000055: # PROGRAM DESCRIPTION - KEPLER SUBROUTINE DATE - 11 OCTOBER 1967
053977,000056: # MOD NO. -1 LOG SECTION - CONIC SUBROUTINES
053978,000057: # MOD BY KRAUSE ASSEMBLY - COLOSSUS 103 AND SUNDANCE 222
053979,000058: # MOD NO. - 2 (AUGUST 1968) BY ROBERTSON: TO PERMIT BACKDATING BY MORE THAN ONE ORBITAL PERIOD.
053980,000059:
053981,000060:
053982,000061: # MOD NO. - 3 (DEC 1968) BY ROBERTSON: SUPPRESSION OF X-MODULO-ING
053983,000062:
053984,000063:
053985,000064: # MOD. NO. - 4 (JAN 1969) BY ROBERTSON: CLEAR OVFIND AT KEPLER ENTRY
053986,000065:
053987,000066:
053988,000067: # FUNCTIONAL DESCRIPTION -
053989,000068: # THIS SUBROUTINE, GIVEN AN INITIAL STATE VECTOR AND THE DESIRED TRANSFER TIME THROUGH WHICH THE STATE IS TO
053990,000069: # BE UPDATED ALONG A CONIC TRAJECTORY, COMPUTES THE NEW, UPDATED STATE VECTOR. THE TRAJECTORY MAY BE ANY CONIC
053991,000070: # SECTION - CIRCULAR, ELLIPTIC, PARABOLIC, HYPERBOLIC, OR RECTILINEAR WITH RESPECT TO THE EARTH OR THE MOON. THE
053992,000071: # USE OF THE SUBROUTINE CAN BE EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT
053993,000072: # INTRODUCING ANY CODING CHANGES, ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY. AN ITERA-
053994,000073: # TION TECHNIQUE IS UTILIZED IN THE COMPUTATION.
053995,000074: # IF A NEGATIVE TIME-OF-FLIGHT IS INPUT, THE PROGRAM WILL SOLVE FOR THE STATE WHICH WOULD BE PRODUCED BY
053996,000075: # EXTRAPOLATING THE POSITION BACKWARD IN TIME.
053997,000076: # IF THE ABSOLUTE VALUE OF THE DESIRED TRANSFER TIME EXCEEDS THE ORBITAL PERIOD, THE SUBROUTINE, THROUGH A
053998,000077: # MODULAR TECHNIQUE, WILL COMPUTE THE STATE CORRESPONDING TO THE DESIRED TIME (WHETHER POSITIVE OR NEGATIVE).
053999,000078:
054000,000079:
054001,000080: # THE RESTRICTIONS ARE -
054002,000081: # 1. (PREVIOUS RESTRICTION ON THE NEGATIVE DESIRED TRANSFER TIME IS NOW DELETED.)
054003,000082: # 2. THE PARAMETERS IN THE PROBLEM CANNOT EXCEED THEIR SCALING LIMITS AS SPECIFIED IN THE GSOP. IF
054004,000083: # ANY OF THESE LIMITS ARE EXCEEDED, THE RESULTING SOLUTION WILL BE MEANINGLESS.
054005,000084:
054006,000085:
054007,000086: # THE NUMBER OF ITERATIONS AND, THEREFORE, THE COMPUTATION SPEED IS DEPENDENT ON THE ACCURACY OF THE
054008,000087: # GUESS, XKFPNEW. THE AGC COMPUTATION TIME IS APPROXIMATELY .061 SECONDS FOR INITIALIZATION, .065 SECONDS FOR THE
054009,000088: # FINAL COMPUTATIONS, PLUS .083 SECONDS FOR EACH ITERATION.
054010,000089:
054011,000090:
054012,000091:
054013,000092: # REFERENCES -
054014,000093: # R-479, MISSION PROGRAMMING DEFINITION MEMO NO. 10, LUNAR LANDING MISSION GSOP, SECTION 5.5, SGA
054015,000094: # MEMO 67-4.
054016,000095:
054017,000096:
054018,000097:
054019,000098: # INPUT - ERASABLE INITIALIZATION REQUIRED
054020,000099:
054021,000100: # * SCALE FACTOR *
054022,000101: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054023,000102: # --------*--------------* -----------------------
054024,000103: # RRECT * +29 FOR EARTH*DP INITIAL POSITION VECTOR IN METERS
054025,000104: # * +27 FOR MOON *
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Page 1264
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054027,000106: # VRECT * +7 FOR EARTH *DP INITIAL VELOCITY VECTOR IN METERS/CENTISECOND
054028,000107: # * +5 FOR MOON *
054029,000108: # X1 (38D)* NONE *INDEX REGISTER SET TO -2D OR -10D ACCORDING TO WHETHER THE EARTH OR MOON,
054030,000109: # * *RESPECTIVELY, IS THE CENTRAL BODY
054031,000110: # TAU. * +28 *DESIRED TRANSFER TIME IN CENTISECONDS (DP)
054032,000111: # * * MAY BE POS OR NEG AND ABSOLUTE VALUE MAY BE GREATER OR LESS THAN ONE ORBITAL PERIOD.
054033,000112: # XKEPNEW * +17 FOR EARTH*DP GUESS OF ROOT X OF KEPLERS EQN IN SQRT(METERS). SIGN SHOULD AGREE WITH THAT OF TAU.
054034,000113: # * +16 FOR MOON * AND ABS VALUE SHOULD BE LESS THAN THAT CORRESPONDING TO A PERIOD, VIZ, 2PI SQRT(SEMI-
054035,000114: # * * MAJOR AXIS), FOR SPEED OF CONVERGENCE, BUT IF EITHER CONDITION FAILS, XKEPNEW IS RESET
054036,000115: # * * BY KEPLER TO A POOR BUT VALID GUESS.
054037,000116: # TC * +28 *DP PREV. VALUE OF TIME IN CENTISECS. MUST BE LESS THAN ONE ORBITAL PERIOD.
054038,000117: # XPREV * +17 FOR EARTH*DP PREV. VALUE OF X IN SQRT(METERS). MUST BE LESS THAN AN X CORRESPONDING TO ONE
054039,000118: # * +16 FOR MOON * ORBITAL PERIOD, VIZ, 2PI SQRT(SEMI-MAJOR AXIS)
054040,000119:
054041,000120:
054042,000121:
054043,000122: # SUBROUTINES CALLED -
054044,000123: # DELTIME
054045,000124:
054046,000125:
054047,000126:
054048,000127: # CALLING SEQUENCE AND NORMAL EXIT MODES -
054049,000128:
054050,000129: # KEPRTN-2 GOTO MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
054051,000130: # KEPRTN-1 KEPLER RETURNS WITH XPREV IN MPAC. PL IS AT 0.
054052,000131: # KEPRTN ... CONTINUE
054053,000132:
054054,000133: # KEPLER MUST NOT BE CALLED DIRECTLY SINCE AN INTERRUPTION OF IT WOULD DESTROY THE ERASABLES IT NEEDS TO COMPLETE
054055,000134: # THE INTERRUPTED JOB. THEREFORE THE USER MUST CALL CSMCONIC OR LEMCONIC WHICH GUARANTEES NO INTERRUPTS AND WHICH
054056,000135: # ALSO CALLS KEPPREP TO COMPUTE A GUESS OF XKEPNEW.
054057,000136:
054058,000137:
054059,000138:
054060,000139: # ABORT EXIT MODES -
054061,000140: # NONE
054062,000141:
054063,000142:
054064,000143: # OUTPUT -
054065,000144:
054066,000145: # * SCALE FACTOR *
054067,000146: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054068,000147: # --------*--------------* -----------------------
054069,000148: # RCV * +29 FOR EARTH*DP TERMINAL POSITION VECTOR IN METERS
054070,000149: # * +27 FOR MOON *
054071,000150: # VCV * +7 FOR EARTH *DP TERMINAL VELOCITY VECTOR IN METERS/CENTISEC
054072,000151: # * +5 FOR MOON *
054073,000152: # TC * +28 *DP TRANSFER TIME IN CENTISECS TO WHICH KEPLER CONVERGED. ALWAYS LESS THAN ONE PERIOD.
054074,000153: # XPREV * +17 FOR EARTH*DP VALUE OF X IN SQRT(METERS) TO WHCIH KEPLER CONVERGED. ALWAYS LESS THAN THE X
054075,000154: # * +16 FOR MOON * CORRESPONDING TO ONE PERIOD.
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Page 1265
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054077,000156: # FOR OTHER OUTPUT WHICH MAY BE OF USE, SEE DEBRIS.
054078,000157:
054079,000158:
054080,000159: # DEBRIS -
054081,000160:
054082,000161: # PARAMETERS WHICH MAY BE OF USE -
054083,000162:
054084,000163: # * SCALE FACTOR *
054085,000164: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054086,000165: # --------*--------------* -----------------------
054087,000166: # URRECT * +1 *DP UNIT VECTOR OF INITIAL POSITION
054088,000167: # R1 * +29 FOR EARTH*DP MAGNITUDE OF INITIAL POSITION IN METERS
054089,000168: # * +27 FOR MOON *
054090,000169: # ALPHA * -22 FOR EARTH*DP INVERSE OF SEMIMAJOR AXIS IN 1/METERS
054091,000170: # * -20 FOR MOON *
054092,000171: # TMODULO * +28 *DP INTEGRAL NUMBER OF PERIODS IN CENTISECS. WHICH WAS SUBTRACTED FROM TAU. TO PRODUCE A
054093,000172: # * *TAU. OF LESS THAN ONE PERIOD.
054094,000173:
054095,000174: # PARAMETERS OF NO USE -
054096,000175: # DP PARAMETERS - EPSILONT, DELX, DELT, RCNORM, XMODULO, PLUS PUSHLIST REGISTERS 0 THROUGH 39D.
054097,000176:
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Page 1266
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054099,000178:
054100,000179: # PROGRAM DESCRIPTION - LAMBERT SUBROUTINE DATE - 1 SEPTEMBER 1967
054101,000180: # MOD NO. - 0 LOG SECTION - CONIC SUBROUTINES
054102,000181: # MOD BY KRAUSE ASSEMBLY - COLOSSUS REVISION 88
054103,000182:
054104,000183:
054105,000184:
054106,000185: # FUNCTIONAL DESCRIPTION -
054107,000186:
054108,000187: # THIS SUBROUTINE CALCULATES THE INITIAL VELOCITY REQUIRED TO TRANSFER A POINT-MASS ALONG A CONIC TRAJECTORY
054109,000188: # FROM AN INITIAL POSITION TO A TERMINAL POSITION IN A PRESCRIBED TIME INTERVAL. THE RESULTING TRAJECTORY MAY BE
054110,000189: # A SECTION OF A CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON. THE USE OF THE
054111,000190: # SUBROUTINE CAN BE EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY
054112,000191: # CODING CHANGES, ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY. AN ITERATION TECHNIQUE IS
054113,000192: # UTILIZED IN THE COMPUTATION.
054114,000193:
054115,000194:
054116,000195: # THE RESTRICTIONS ARE -
054117,000196: # 1. RECTILINEAR TRAJECTORIES CANNOT BE COMPUTED.
054118,000197: # 2. AN ACCURACY DEGRADATION OCCURS AS THE COSINE OF THE TRUE ANOMALY DIFFERENCE APPROACHES +1.0.
054119,000198: # 3. THE ANGLE BETWEEN ANY POSITION VECTOR AND ITS VELOCITY VECTOR MUST BE GREATER THAN 1 DEGREE 47.5 MINUTES
054120,000199: # AND LESS THAN 178 DEGREES 12.5 MINUTES.
054121,000200: # 4. NEGATIVE TRANSFER TIME IS AMBIGUOUS AND WILL RESULT IN NO SOLUTION.
054122,000201: # 5. THE PARAMETERS IN THE PROBLEM MUST NOT EXCEED THEIR SCALING LIMITS SPECIFIED IN THE GSOP. IF THE
054123,000202: # LIMITS ARE EXCEEDED, THE RESULTING SOLUTION WILL BE MEANINGLESS.
054124,000203: # THE NUMBER OF ITERATIONS AND, THEREFORE, THE COMPUTATIONS SPEED IS DEPENDENT ON THE ACCURACY OF THE FIRST
054125,000204: # GUESS OF THE INDEPENDENT VARIABLE, COGA. THE AGC COMPUTATION TIME IS APPROXIMATE-
054126,000205: # LY .105 SECONDS FOR INITIALIZATION, .069 SECONDS FOR FINAL COMPUTATIONS, PLUS .205 SECONDS FOR EACH ITERATION.
054127,000206:
054128,000207:
054129,000208:
054130,000209: # REFERENCES -
054131,000210: # R-479, MISSION PROGRAMMING DEFINITION MEMO NO. 10, LUNAR LANDING MISSION GSOP-SECTION 5.5, SGA MEMO 67-8,
054132,000211: # SGA MEMO 67-4.
054133,000212:
054134,000213:
054135,000214:
054136,000215: # INPUT - ERASABLE INITIALIZATION REQUIRED
054137,000216:
054138,000217: # * SCALE FACTOR *
054139,000218: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054140,000219: # --------*--------------* -----------------------
054141,000220: # R1VEC * +29 FOR EARTH*DP INITIAL POSITION VECTOR IN METERS
054142,000221: # * +27 FOR MOON *
054143,000222: # R2VEC * +29 FOR EARTH*DP TARGET OR TERMINAL POSITION VECTOR IN METERS
054144,000223: # * +27 FOR MOON *
054145,000224: # TDESIRED* +28 *DP DESIRED TRANSFER TIME IN CENTISECONDS
054146,000225: # X1 (38D)* NONE *INDEX REGISTER SET TO -2D OR -10D ACCORDING TO WHETHER THE EARTH OR MOON,
054147,000226: # * *RESPECTIVELY, IS THE CENTRAL BODY
054148,000227: # GEOMSGN * NONE *SP +.5 IF DESIRED TRANSFER ANGLE IS LESS THAN 180 DEGREES, -.5 IF GREATER THAN 180 DEG.
054149,000228: # GUESSW * NONE *AN INTERPRETER SWITCH TO BE SET IF NO GUESS OF COGA IS AVAILABLE, CLEAR IF A GUESS OF
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Page 1267
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054151,000230: # * *COGA IS TO BE USED BY LAMBERT
054152,000231: # COGA * +5 *DP GUESS OF COTANGNT OF FLIGHT PATH ANGLE (MEASURED FROM VERTICAL). THIS WILL BE
054153,000232: # *IGNORED IF GUESSW IS SET.
054154,000233: # NORMSW * NONE *AN INTERPRETER SWITCH TO BE SET IF UN IS TO BE AN INPUT TO THE SUBROUTINE, CLEAR IF
054155,000234: # * *LAMBERT IS TO COMPUTE ITS OWN NORMAL (UN).
054156,000235: # UN * +1 *DP UNIT NORMAL TO THE DESIRED ORBIT PLANE IN THE DIRECTION OF THE RESULTING ANGULAR
054157,000236: # * *MOMENTUM VECTOR. THIS WILL BE IGNORED IF NORMSW IS CLEAR.
054158,000237: # VTARGTAG* NONE *A S.P. TAG TO BE SET TO ZERO IF LAMBERT IS TO COMPUTE THE VELOCITY AT R2VEC AS WELL AS
054159,000238: # * *AT R1VEC.
054160,000239:
054161,000240:
054162,000241:
054163,000242: # SUBROUTINES CALLED -
054164,000243: # GEOM, GETX, DELTIME, ITERATOR, LAMENTER (PART OF NEWSTATE)
054165,000244:
054166,000245:
054167,000246:
054168,000247: # CALLING SEQUENCE AND NORMAL EXIT MODES -
054169,000248:
054170,000249: # L CALL MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
054171,000250: # L+1 LAMBERT RETURNS WITH PL AT 0 AND WITH VVEC IN MPAC IF VTARGTAG WAS NON-ZERO OR VTARGET
054172,000251: # IN MPAC IF VTARGTAG WAS ZERO
054173,000252: # L+2 BON CONTINUE IF SOLNSW CLEAR SINCE SOLUTION IS ACCEPTABLE
054174,000253: # L+3 SOLNSW
054175,000254: # L+4 LAMABORT
054176,000255:
054177,000256: # IF A LAMBERT RESULT IS TO BE A FIRST GUESS FOR THE NEXT LAMBERT CALCULATION, COGA MUST BE PRESERVED AND
054178,000257: # GUESSW MUST BE CLEAR FOR EACH SUCCEEDING LAMBERT CALL.
054179,000258:
054180,000259:
054181,000260:
054182,000261: # ABORT EXIT MODES -
054183,000262: # IF SOLNSW WAS SET UPON EXITING, EITHER LAMBERT WAS ASKED TO COMPUTE A TRANSFER TOO NEAR 0 OR 360 DEG, OR T
054184,000263: # WAS TOO SMALL TO PRODUCE A REALISTIC TRANSFER BETWEEN R1VEC AND R2VEC. IN EITHER CASE THE FIX MUST BE MADE
054185,000264: # ACCORDING TO THE NEEDS OF THE PARTICULAR USER. THE ABORT EXIT MODE MAY BE CODED AS ...
054186,000265: # LAMABORT DLOAD ABS A MEASURE OF PROXIMITY TO 0 OR
054187,000266: # 1-CSTH 360 DEGREES.
054188,000267: # DSU BMN
054189,000268: # ONEBIT
054190,000269: # CHANGER2 CHANGE R2VEC DIRECTION SLIGHTLY.
054191,000270: # DLOAD DAD
054192,000271: # TDESIRED
054193,000272: # SOMETIME
054194,000273: # STCALL TDESIRED INCREASE TDESIRED
054195,000274: # LAMBERT
054196,000275:
054197,000276:
054198,000277:
054199,000278: # OUTPUT -
054200,000279: # * SCALE FACTOR *
054201,000280: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
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Page 1268
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054203,000282: # --------*--------------* -----------------------
054204,000283: # VVEC * +7 FOR EARTH *DP INITIAL VELOCITY VECTOR IN METERS/CENTISECOND REQUIRED TO SATISFY THE BOUNDARY VALUE
054205,000284: # * +5 FOR MOON *PROBLEM.
054206,000285: # VTARGET * +7 FOR EARTH *DP RESULTANT VELOCITY VECTOR AT R2VEC IN METERS/CENTISECOND.
054207,000286: # * +5 FOR MOON *
054208,000287: # SOLNSW * NONE *INTERPRETER SWITCH WHICH IS SET IF THE SUBROUTINE CANNOT SOLVE THE PROBLEM, CLEAR IF THE
054209,000288: # * *SOLUTION EXISTS.
054210,000289: # FOR OTHER OUTPUT WHICH MAY BE OF USE, SEE DEBRIS.
054211,000290:
054212,000291:
054213,000292:
054214,000293: # DEBRIS -
054215,000294: # PARAMETERS WHICH MAY BE OF USE -
054216,000295:
054217,000296: # * SCALE FACTOR *
054218,000297: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054219,000298: # --------*--------------* -----------------------
054220,000299: # SNTH * +1 *DP SIN OF ANGLE BETWEEN R1VEC AND R2VEC
054221,000300: # CSTH * +1 *DP COSINE OF ANGLE
054222,000301: # 1-CSTH * +2 *DP 1-CSTH
054223,000302: # COGA * +5 *DP COTAN OF INITIAL REQUIRED FLIGHT PATH ANGLE MEASURED FROM VERTICAL
054224,000303: # P * +4 *DP RATIO OF SEMILATUS RECTUM TO INITIAL RADIUS
054225,000304: # R1A * +6 *DP RATIO OF INITIAL RADIUS TO SEMIMAJOR AXIS
054226,000305: # R1 (32D)* +29 FOR EARTH*DP INITIAL RADIUS IN METERS
054227,000306: # * +27 FOR MOON *
054228,000307: # UR1 * +1 *DP UNIT VECTOR OF R1VEC
054229,000308: # U2 * +1 *DP UNIT VECTOR OF R2VEC
054230,000309:
054231,000310: # PARAMETERS OF NO USE
054232,000311: # DP PARAMETERS - EPSILONL, CSTH-RHO, TPREV, TERRLAMB, R2, RTNLAMB (SP), PLUS PUSHLIST REGISTER 0 THROUGH 41D
054233,000312: # ADDITIONAL INTERPRETIVE SWITCHES USED - INFINFLG, 360SW, SLOPESW, ORDERSW
054234,000313:
054235,000314:
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Page 1269
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054237,000316:
054238,000317: # PROGRAM DESCRIPTION - TIME-THETA SUBROUTINE DATE - 1 SEPTEMBER 1967
054239,000318: # MOD NO. - 0 LOG SECTION - CONIC SUBROUTINES
054240,000319: # MOD BY KRAUSE ASSEMBLY - COLOSSUS REVISION 88
054241,000320:
054242,000321:
054243,000322:
054244,000323: # FUNCTIONAL DESCRIPTION -
054245,000324:
054246,000325: # THIS SUBROUTINE, GIVEN AN INITIAL STATE VECTOR AND A DESIRED TRUE-ANOMALY-DIFFERENCE THROUGH WHICH THE
054247,000326: # STATE IS TO BE UPDATED ALONG A CONIC TRAJECTORY, CALCULATES THE CORRESPONDING TIME-OF-FLIGHT AND, IN ADDITION,
054248,000327: # PROVIDES THE OPTION OF COMPUTING THE NEW UPDATED STATE VECTOR. THE RESULTING TRAJECTORY MAY BE A SECTION OF A
054249,000328: # CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON. THE USE OF THE SUBROUTINE CAN BE
054250,000329: # EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY CODING CHANGES,
054251,000330: # ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY.
054252,000331:
054253,000332:
054254,000333: # THE RESTRICTIONS ARE -
054255,000334: # 1. THE ANGLE BETWEEN ANY POSITION VECTOR AND ITS VELOCITY VECTOR MUST BE GREATER THAN 1 DEGREE 47.5 MINUTES
054256,000335: # AND LESS THAN 178 DEGREES 12.5 MINUTES.
054257,000336: # 2. THE PARAMETERS IN THE PROBLEM MUST NOT EXCEED THEIR SCALING LIMITS SPECIFIED IN THE GSOP. IF THE LIMITS
054258,000337: # ARE EXCEEDED, THE RESULTING SOLUTION WILL BE MEANINGLESS.
054259,000338:
054260,000339: # THE AGC COMPUTATION TIME IS APPROXIMATELY .292 SECONDS.
054261,000340:
054262,000341:
054263,000342: # REFERENCES -
054264,000343: # R-479, MISSION PROGRAMMING DEFINITION MEMO NO. 10, LUNAR LANDING MISSION GSOP-SECTION 5.5, SGA MEMO 67-8.
054265,000344:
054266,000345:
054267,000346: # INPUT - ERASABLE INITIALIZATION REQUIRED
054268,000347:
054269,000348: # * SCALE FACTOR *
054270,000349: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054271,000350: # --------*--------------* -----------------------
054272,000351: # RVEC * +29 FOR EARTH*DP INITIAL POSITION VECTOR IN METERS
054273,000352: # * +27 FOR MOON *
054274,000353: # VVEC * +7 FOR EARTH *DP INITIAL VELOCITY VECTOR IN METERS/CENTISECOND
054275,000354: # * +5 FOR MOON *
054276,000355: # SNTH * +1 *DP SINE OF TRUE-ANOMALY-DIFFERENCE THROUGH WHICH THE STATE IS TO BE UPDATED
054277,000356: # CSTH * +1 *DP COSINE OF THE ANGLE
054278,000357: # RVSW * NONE *AN INTERPRETIVE SWITCH TO BE SET IF ONLY TIME IS TO BE AN OUTPUT, CLEAR IF THE NEW STATE
054279,000358: # * *IS TO BE COMPUTED ALSO.
054280,000359: # X1 (38D)*NONE *INDEX REGISTER TO BE SET TO -2D OR -10D ACCORDING TO WHETHER THE EARTH OR MOON,
054281,000360: # * *RESPECTIVELY, IS THE CENTRAL BODY.
054282,000361:
054283,000362:
054284,000363:
054285,000364: # SUBROUTINES CALLED -
|
|
Page 1270
|
054287,000366: # PARAM, GEOM, GETX, DELTIME, NEWSTATE
054288,000367:
054289,000368:
054290,000369:
054291,000370: # CALLING SEQUENCE AND NORMAL EXIT MODES -
054292,000371:
054293,000372: # IF ONLY TIME IS DESIRED AS OUTPUT -
054294,000373: # L SET CALL MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
054295,000374: # L+1 RVSW
054296,000375: # L+2 TIMETHET RETURN WITH PL AT 0 AND T IN MPAC
054297,000376: # L+3 ... CONTINUE
054298,000377:
054299,000378:
054300,000379: # IF THE UPDATE STATE VECTOR IS DESIRED AS WELL -
054301,000380: # L CLEAR CALL MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
054302,000381: # L+1 RVSW
054303,000382: # L+2 TIMETHET RETURNS WITH PL AT 6. THE INITIAL POSITION VECTOR IS IN 0D OF THE PUSHLIST AND
054304,000383: # THE INITIAL VELOCITY VECTOR IN MPAC.
054305,000384: # L+3 STOVL NEWVVEC
054306,000385: # L+4 STADR
054307,000386: # L+5 STORE NEWRVEC NEWVVEC AND NEWRVEC ARE SYMBOLIC REPRESENTATIONS OF THE USERS LOCATIONS.
054308,000387: # L+6 ... CONTINUE
054309,000388:
054310,000389:
054311,000390:
054312,000391: # ABORT EXIT MODES -
054313,000392: # IF COGAFLAG AND/OR INFINFLG IS SET AT THE EXIT TO TIME-THETA, TIME-THETA WILL TRANSFER TO POODOO WITH
054314,000393: # AN ALARM CODE (ORIGINALLY 00607), AND NOT RETURN TO THE CALLING PROGRAM. (PCR 692 AND 721).
054315,000394:
054316,000395:
054317,000396:
054318,000397: # OUTPUT -
054319,000398: # * SCALE FACTOR *
054320,000399: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054321,000400: # --------*--------------* -----------------------
054322,000401: # T(30D) * +28 *DP TRANSFER TIME IN CENTISECONDS
054323,000402: # INFINFLG* NONE *AN INTERPRETIVE SWITCH WHICH IS SET IF THE TRANSFER ANGLE REQUIRES CLOSURE THROUGH
054324,000403: # * *INFINITY (NO SOLUTION), CLEAR IF A PHYSICAL SOLUTION IS POSSIBLE.
054325,000404: # COGAFLAG* NONE *AN INTERPRETIVE SWITCH WHICH IS SET IF RESTRICTION 1 HAS BEEN VIOLATED (NO SOLUTION),
054326,000405: # * *CLEAR IF NOT.
054327,000406:
054328,000407: # IN ADDITION, IF RVSW IS CLEAR, THE FOLLOWING ARE OUTPUT -
054329,000408:
054330,000409: # MPAC - * +7 FOR EARTH *DP TERMINAL VELOCITY VECTOR IN METERS/CENTISEC.
054331,000410: # MPAC +5* +5 FOR MOON *
054332,000411: # 0D - 5D * +29 FOR EARTH*DP TERMINAL POSITION VECTOR IN METERS (PL AT 6D)
054333,000412: # * +27 FOR MOON *
054334,000413:
054335,000414: # FOR OTHER OUTPUT WHICH MAY BE OF USE, SEE DEBRIS.
054336,000415:
|
|
Page 1271
|
054338,000417:
054339,000418: # DEBRIS -
054340,000419:
054341,000420: # PARAMETERS WHICH MAY BE OF USE -
054342,000421:
054343,000422: # * SCALE FACTOR *
054344,000423: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054345,000424: # --------*--------------* -----------------------
054346,000425: # R1 (32D)* +29 FOR EARTH*DP MAGNITUDE OF INITIAL POSITION VECTOR, RVEC, IN METERS
054347,000426: # * +27 FOR MOON *
054348,000427: # R1A * +6 *DP RATIO OF R1 TO SEMIMAJOR AXIS (NEG. FOR HYPERBOLIC TRAJECTORIES)
054349,000428: # P * +4 *DP RATIO OF SEMILATUS RECTUM TO R1
054350,000429: # COGA * +5 *DP COTAN OF ANGLE BETWEEN RVEC AND VVEC
054351,000430: # UR1 * +1 *DP UNIT VECTOR OF RVEC
054352,000431: # U2 * +1 *DP UNIT VECTOR OF VVEC
054353,000432: # UN * +1 *DP UNIT VECTOR OF UR1*U2
054354,000433:
054355,000434: # PARAMETERS OF NO USE -
054356,000435: # SP PARAMETERS - RTNTT, GEOMSGN, RTNPRM, MAGVEC2=R2 (DP), PLUS PUSHLIST LOCATIONS 0-11D, 14D-21D, 24D-39D, 41D
054357,000436: # ADDITIONAL INTERPRETIVE SWITCHES USED - NORMSW, 360SW
054358,000437:
054359,000438:
|
|
Page 1272
|
054361,000440:
054362,000441: # PROGRAM DESCRIPTION - TIME-RADIUS SUBROUTINE DATE - 11 OCTOBER 1967
054363,000442: # MOD NO. -1 LOG SECTION - CONIC SUBROUTINES
054364,000443: # MOD BY KRAUSE ASSEMBLY - COLOSSUS REVISION 88
054365,000444:
054366,000445:
054367,000446:
054368,000447: # FUNCTIONAL DESCRIPTION -
054369,000448:
054370,000449: # THIS SUBROUTINE, GIVEN AN INITIAL STATE VECTOR AND A DESIRED RADIUS TO WHICH THE
054371,000450: # STATE IS TO BE UPDATED ALONG A CONIC TRAJECTORY, CALCULATES THE CORRESPONDING TIME-OF-FLIGHT AND, IN ADDITION,
054372,000451: # PROVIDES THE OPTION OF COMPUTING THE NEW UPDATED STATE VECTOR. THE RESULTING TRAJECTORY MAY BE A SECTION OF A
054373,000452: # CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON. THE USE OF THE SUBROUTINE CAN BE
054374,000453: # EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY CODING CHANGES,
054375,000454: # ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY.
054376,000455: # IF THE DESIRED RADIUS IS BEYOND THE RADIUS OF APOCENTER OF THE CONIC OR BELOW THE RADIUS OF PERICENTER,
054377,000456: # APSESW WILL BE SET AND THE SUBROUTINE WILL RETURN THE APOCENTER OR PERICENTER SOLUTION, RESPECTIVELY.
054378,000457:
054379,000458:
054380,000459: # THE RESTRICTIONS ARE -
054381,000460: # 1. THE ANGLE BETWEEN ANY POSITION VECTOR AND ITS VELOCITY VECTOR MUST BE GREATER THAN 1 DEGREE 47.5 MINUTES
054382,000461: # AND LESS THAN 178 DEGREES 12.5 MINUTES.
054383,000462: # 2. THE PARAMETERS IN THE PROBLEM MUST NOT EXCEED THEIR SCALING LIMITS SPECIFIED IN THE GSOP. IF THE LIMITS
054384,000463: # ARE EXCEEDED, THE RESULTING SOLUTION WILL BE MEANINGLESS.
054385,000464: # 3. AN ACCURACY DEGRADATION OCCURS AS THE SENSITIVITIES OF TIME AND UPDATED STATE VECTOR TO CHANGES IN
054386,000465: # RDESIRED INCREASE. THIS WILL OCCUR NEAR EITHER APSIS OF THE CONIC AND WHEN THE CONIC IS NEARLY CIRCULAR. IN
054387,000466: # PARTICULAR, IF THE CONIC IS AN EXACT CIRCLE, THE PROBLEM IS UNDEFINED AND THE SUBROUTINE WILL ABORT.
054388,000467:
054389,000468:
054390,000469: # THE AGC COMPUTATION TIME IS APPROXIMATELY .363 SECONDS
054391,000470:
054392,000471:
054393,000472:
054394,000473: # REFERENCES -
054395,000474: # R-479, MISSION PROGRAMMING DEFINITION MEMO NO. 10, LUNAR LANDING MISSION GSOP-SECTION 5.5, SGA MEMO 67-8.
054396,000475:
054397,000476:
054398,000477:
054399,000478: # INPUT - ERASABLE INITIALIZATION REQUIRED
054400,000479:
054401,000480: # * SCALE FACTOR *
054402,000481: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054403,000482: # --------*--------------* -----------------------
054404,000483: # RVEC * +29 FOR EARTH*DP INITIAL POSITION VECTOR IN METERS
054405,000484: # * +27 FOR MOON *
054406,000485: # VVEC * +7 FOR EARTH *DP INITIAL VELOCITY VECTOR IN METERS/CENTISECOND
054407,000486: # * +5 FOR MOON *
054408,000487: # RDESIRED* +29 FOR EARTH*DP TERMINAL RADIAL DISTANCE ON CONIC TRAJECTORY FOR WHICH TRANSFER TIME IS TO BE
054409,000488: # * +27 FOR MOON *COMPUTED.
054410,000489: # SGNRDOT * NONE *SP TAG SET TO +.5 OR -.5 ACCORDING TO WHETHER THE RADIAL VELOCITY AT RDESIRED IS TO BE
054411,000490: # * *POSITIVE OR NEGATIVE, RESPECTIVELY. THIS TAG REDUCES THE DOUBLE-VALUED PROBLEM TO A
|
|
Page 1273
|
054413,000492: # * *SINGLE-VALUED PROBLEM.
054414,000493: # X1 (38D)* NONE *INDEX REGISTER TO BE SET TO -2D OR -10D ACCORDING TO WHETHER THE EARTH OR MOON,
054415,000494: # * *RESPECTIVELY, IS THE CENTRAL BODY.
054416,000495: # RVSW * NONE *AN INTERPRETIVE SWITCH TO BE SET IF ONLY TIME IS TO BE AN OUTPUT, CLEAR IF THE NEW STATE
054417,000496: # * *IS TO BE COMPUTED ALSO.
054418,000497:
054419,000498:
054420,000499:
054421,000500: # SUBROUTINES CALLED -
054422,000501: # PARAM, GEOM, GETX, DELTIME, NEWSTATE
054423,000502:
054424,000503:
054425,000504:
054426,000505: # CALLING SEQUENCE AND NORMAL EXIT MODES -
054427,000506:
054428,000507: # IF ONLY TIME IS DESIRED AS OUTPUT -
054429,000508: # L SET CALL MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
054430,000509: # L+1 RVSW
054431,000510: # L+2 TIMERAD RETURN WITH PL AT 0 AND T IN MPAC
054432,000511: # L+3 ... CONTINUE
054433,000512:
054434,000513: # IF THE UPDATE STATE VECTOR IS DESIRED AS WELL -
054435,000514: # L CLEAR CALL MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
054436,000515: # L+1 RVSW
054437,000516: # L+2 TIMERAD RETURNS WITH PL AT 6. THE INITIAL POSITION VECTOR IS IN 0D OF THE PUSHLIST AND
054438,000517: # THE INITIAL VELOCITY VECTOR IN MPAC.
054439,000518: # L+3 STOVL NEWVVEC
054440,000519: # L+4 STADR
054441,000520: # L+5 STORE NEWRVEC NEWVVEC AND NEWRVEC ARE SYMBOLIC REPRESENTATIONS OF THE USERS LOCATIONS.
054442,000521: # L+6 ... CONTINUE
054443,000522:
054444,000523:
054445,000524:
054446,000525: # ABORT EXIT MODES -
054447,000526: # IF SOLNSW AND/OR COGAFLAG AND/OR INFINFLG IS SET AT THE EXIT TO TIME-RADIUS, TIME-RADIUS WILL TRANSFER
054448,000527: # TO POODOO WITH AN ALARM CODE (ORIGINALLY 00607), AND NOT RETURN TO THE CALLING PROGRAM. (PCR 692 & 721)
054449,000528:
054450,000529:
054451,000530:
054452,000531: # OUTPUT -
054453,000532: # * SCALE FACTOR *
054454,000533: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054455,000534: # --------*--------------* -----------------------
054456,000535: # T (30D) * +28 *DP TRANSFER TIME IN CENTISECONDS
054457,000536: # INFINFLG* NONE *AN INTERPRETIVE SWITCH WHICH IS SET IF RDESIRED AND SGNRDOT REQUIRE CLOSURE THROUGH
054458,000537: # * *INFINITY (NO SOLUTION), CLEAR IF A PHYSICAL SOLUTION IS POSSIBLE.
054459,000538: # COGAFLAG* NONE *AN INTERPRETIVE SWITCH WHICH IS SET IF RESTRICTION 1 HAS BEEN VIOLATED (NO SOLUTION),
054460,000539: # * *CLEAR IF NOT.
054461,000540: # APSESW * NONE *AN INTERPRETIVE SWITCH WHICH IS SET IF RDESIRED WAS GREATER THAN RADIUS OF APOCENTER OR
|
|
Page 1274
|
054463,000542: # * *LESS THAN RADIUS OF PERICENTER. THE APOCENTER OR PERICENTER SOLUTION, RESPECTIVELY,
054464,000543: # * *WILL THEN BE RETURNED. THE SWITCH IS CLEAR IF RDESIRED WAS BETWEEN PERICENTER AND
054465,000544: # * *APOCENTER.
054466,000545: # SOLNSW * NONE *AN INTERPRETIVE SWITCH WHICH IS SET IF THE CONIC IS SO CLOSE TO A CIRCLE THAT THE TERMIN
054467,000546: # *POINT IS AMBIGUOUS, VIOLATING RESTRICTION 3. IF ECCENTRICITY IS GREATER THAN 2-TO-THE-
054468,000547: # *MINUS-18, THE SWITCH IS CLEAR.
054469,000548:
054470,000549:
054471,000550: # IN ADDITION, IF RVSW IS CLEAR, THE FOLLOWING ARE OUTPUT -
054472,000551:
054473,000552: # MPAC - * +7 FOR EARTH *DP TERMINAL VELOCITY VECTOR IN METERS/CENTISEC.
054474,000553: # MPAC +5* +5 FOR MOON *
054475,000554: # 0D - 5D * +29 FOR EARTH*DP TERMINAL POSITION VECTOR IN METERS (PL AT 6D)
054476,000555: # * +27 FOR MOON *
054477,000556:
054478,000557: # FOR OTHER OUTPUT WHICH MAY BE OF USE, SEE DEBRIS.
054479,000558:
054480,000559:
054481,000560:
054482,000561: # DEBRIS -
054483,000562:
054484,000563: # PARAMETERS WHICH MAY BE OF USE -
054485,000564:
054486,000565: # * SCALE FACTOR *
054487,000566: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054488,000567: # --------*--------------* -----------------------
054489,000568: # R1 (32D)* +29 FOR EARTH*DP MAGNITUDE OF INITIAL POSITION VECTOR, RVEC, IN METERS
054490,000569: # * +27 FOR MOON *
054491,000570: # R1A * +6 *DP RATIO OF R1 TO SEMIMAJOR AXIS (NEG. FOR HYPERBOLIC TRAJECTORIES)
054492,000571: # P * +4 *DP RATIO OF SEMILATUS RECTUM TO R1
054493,000572: # COGA * +5 *DP COTAN OF ANGLE BETWEEN RVEC AND VVEC
054494,000573: # UR1 * +1 *DP UNIT VECTOR OF RVEC
054495,000574: # U2 * +1 *DP UNIT VECTOR OF VVEC
054496,000575: # UN * +1 *DP UNIT VECTOR OF UR1*U2
054497,000576: # CSTH * +1 *DP COSINE OF TRUE ANOMALY DIFFERENCE BETWEEN RVEC AND RDESIRED.
054498,000577: # SNTH * +1 *DP SINE OF TRUE ANOMALY DIFFERENCE.
054499,000578:
054500,000579:
054501,000580: # PARAMETERS OF NO USE -
054502,000581: # SP PARAMETERS - RTNTT, GEOMSGN, RTNPRM, MAGVEC2=R2 (DP), PLUS PUSHLIST LOCATIONS 0-11D, 14D-21D, 24D-39D, 41D
054503,000582: # ADDITIONAL INTERPRETIVE SWITCHES USED - NORMSW, 360SW
054504,000583:
054505,000584:
|
|
Page 1275
|
054507,000586:
054508,000587: # PROGRAM DESCRIPTION - APSIDES SUBROUTINE DATE - 1 SEPTEMBER 1967
054509,000588: # MOD NO. - 0 LOG SECTION - CONIC SUBROUTINES
054510,000589: # MOD BY KRAUSE ASSEMBLY - COLOSSUS REVISION 88
054511,000590:
054512,000591:
054513,000592:
054514,000593: # FUNCTIONAL DESCRIPTION -
054515,000594:
054516,000595: # THIS SUBROUTINE, GIVEN AN INITIAL STATE VECTOR CALCULATES THE RADIUS OF PERICENTER AND OF APOCENTER AND THE
054517,000596: # ECCENTRICITY OF THE RESULTING CONIC TRAJECTORY, WHICH MAY BE A STRAIGHT LINE,
054518,000597: # CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON. THE USE OF THE SUBROUTINE CAN BE
054519,000598: # EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY CODING CHANGES,
054520,000599: # ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY.
054521,000600:
054522,000601:
054523,000602: # THE RESTRICTIONS ARE -
054524,000603: # 1. IF APOCENTER IS BEYOND THE SCALING OF POSITION, THE SCALE FACTOR LIMIT (536,870,910 METERS WITH RESPECT
054525,000604: # TO THE EARTH OR 134,217,727.5 METERS WITH RESPECT TO THE MOON) WILL BE RETURNED.
054526,000605: # 2. THE PARAMETERS IN THE PROBLEM MUST NOT EXCEED THEIR SCALING LIMITS SPECIFIED IN THE GSOP. IF THE LIMITS
054527,000606: # ARE EXCEEDED, THE RESULTING SOLUTION WILL BE MEANINGLESS.
054528,000607:
054529,000608: # THE AGC COMPUTATION TIME IS APPROXIMATELY .103 SECONDS.
054530,000609:
054531,000610:
054532,000611:
054533,000612: # REFERENCES -
054534,000613: # MISSION PROGRAMMING DEFINITION MEMO NO. 10, LUNAR LANDING MISSION GSOP-SECTION 5.5
054535,000614:
054536,000615:
054537,000616:
054538,000617: # INPUT - ERASABLE INITIALIZATION REQUIRED
054539,000618:
054540,000619: # * SCALE FACTOR *
054541,000620: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054542,000621: # --------*--------------* -----------------------
054543,000622: # RVEC * +29 FOR EARTH*DP INITIAL POSITION VECTOR IN METERS
054544,000623: # * +27 FOR MOON *
054545,000624: # VVEC * +7 FOR EARTH *DP INITIAL VELOCITY VECTOR IN METERS/CENTISECOND
054546,000625: # * +5 FOR MOON *
054547,000626: # X1 (38D)* NONE *INDEX REGISTER TO BE SET TO -2D OR -10D ACCORDING TO WHETHER THE EARTH OR MOON,
054548,000627: # * *RESPECTIVELY, IS THE CENTRAL BODY.
054549,000628:
054550,000629:
054551,000630:
054552,000631: # SUBROUTINES CALLED -
054553,000632: # PARAM, GEOM
054554,000633:
054555,000634:
054556,000635:
054557,000636: # CALLING SEQUENCE AND NORMAL EXIT MODES -
054558,000637:
|
|
Page 1276
|
054560,000639: # IF ONLY TIME IS DESIRED AS OUTPUT -
054561,000640: # L CALL MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
054562,000641: # L+1 APSIDES RETURNS WITH PL AT 0, RADIUS OF APOCENTER IN MPAC AND RADIUS OF PERICENTER IN 0D
054563,000642: # L+2 STODL APOAPSE
054564,000643: # L+3 0D
054565,000644: # L+4 STORE PERIAPSE APOAPSE AND PERIAPSE ARE SYMBOLIC REPRESENTATIONS OF THE USERS LOCATIONS
054566,000645: # L+5 ... CONTINUE
054567,000646:
054568,000647: # OUTPUT -
054569,000648: # * SCALE FACTOR *
054570,000649: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054571,000650: # --------*--------------* -----------------------
054572,000651: # MPAC * +29 FOR EARTH*DP RADIUS OF APOCENTER IN METERS
054573,000652: # * +27 FOR MOON *
054574,000653: # 0D-1D * +29 FOR EARTH*DP RADIUS OF PERICENTER IN METERS
054575,000654: # * +27 FOR MOON *
054576,000655: # ECC * +3 *DP ECCENTRICITY OF CONIC TRAJECTORY.
054577,000656:
054578,000657: # FOR OTHER OUTPUT WHICH MAY BE OF USE, SEE DEBRIS.
054579,000658:
054580,000659:
054581,000660:
054582,000661: # DEBRIS -
054583,000662:
054584,000663: # PARAMETERS WHICH MAY BE OF USE -
054585,000664:
054586,000665: # * SCALE FACTOR *
054587,000666: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054588,000667: # --------*--------------* -----------------------
054589,000668: # R1 (32D)* +29 FOR EARTH*DP MAGNITUDE OF INITIAL POSITION VECTOR, RVEC, IN METERS
054590,000669: # * +27 FOR MOON *
054591,000670: # R1A * +6 *DP RATIO OF R1 TO SEMIMAJOR AXIS (NEG. FOR HYPERBOLIC TRAJECTORIES)
054592,000671: # P * +4 *DP RATIO OF SEMILATUS RECTUM TO R1
054593,000672: # COGA * +5 *DP COTAN OF ANGLE BETWEEN RVEC AND VVEC
054594,000673: # UR1 * +1 *DP UNIT VECTOR OF RVEC
054595,000674: # U2 * +1 *DP UNIT VECTOR OF VVEC
054596,000675: # UN * +1 *DP UNIT VECTOR OF UR1*U2
054597,000676: # MAGVEC2 * +7 FOR EARTH *DP MAGNITUDE OF VVEC
054598,000677: # * +5 FOR MOON *
054599,000678:
054600,000679:
054601,000680: # PARAMETERS OF NO USE -
054602,000681: # SP PARAMETERS - RTNAPSE, GEOMSGN, RTNPRM, PLUS PUSHLIST LOCATIONS 0-5,10D-11D, 14D-21D, 31D-38D.
054603,000682: # ADDITIONAL INTERPRETIVE SWITCHES USED - NORMSW
054604,000683:
054605,000684:
054606,000685:
054607,000686: 12,2000 SETLOC CONICS
|
|
Page 1277
|
054609,000688: 12,2000 BANK
054610,000689:
054611,000690: 12,2077 COUNT* $$/CONIC
054612,000691: 12,2077 E5,1723 EBANK= UR1
054613,000692:
054614,000693: 12,2077 77624 KEPLERN CALL
054615,000694: 12,2100 24577 COMSETUP
054616,000695: 12,2101 53575 VLOAD UNIT
054617,000696: 12,2102 01503 RRECT
054618,000697: 12,2103 16647 STODL URRECT
054619,000698: 12,2104 00045 36D
054620,000699: 12,2105 24041 STOVL R1
054621,000700: 12,2106 01503 RRECT
054622,000701: 12,2107 76441 DOT SL1R
054623,000702: 12,2110 01511 VRECT
054624,000703: 12,2111 76405 DMP SL1R
054625,000704: 12,2112 00023 1/ROOTMU # 1/ROOTMU (-17 OR -14)
054626,000705: 12,2113 24043 STOVL KEPC1 # C1=R.V/ROOTMU (+17 OR +16)
054627,000706:
054628,000707: 12,2114 01511 VRECT
054629,000708: 12,2115 57236 VSQ DMPR
054630,000709: 12,2116 00017 1/MU # 1/MU (-34 OR -28)
054631,000710: 12,2117 52405 DMP SL3
054632,000711: 12,2120 00041 R1
054633,000712: 12,2121 61425 DSU ROUND
054634,000713: 12,2122 33410 D1/64
054635,000714: 12,2123 00045 STORE KEPC2 # C2=RV.V/MU -1 (+6)
054636,000715:
054637,000716: 12,2124 74421 BDSU SR1R
054638,000717: 12,2125 33410 D1/64
054639,000718: 12,2126 77671 DDV
054640,000719: 12,2127 00041 R1
054641,000720: 12,2130 00011 STORE ALPHA # ALPHA=(1-C2)/R1 (-22 OR -20)
054642,000721:
054643,000722: 12,2131 71244 BPL DLOAD # MAXIMUM X DEPENDS ON TYPE OF CONIC
054644,000723: 12,2132 24141 1REV
054645,000724: 12,2133 33426 -50SC # -50SC (+12)
054646,000725: 12,2134 40071 DDV BOV
054647,000726: 12,2135 00011 ALPHA
054648,000727: 12,2136 24145 STOREMAX
054649,000728: 12,2137 52166 SQRT GOTO
054650,000729: 12,2140 24145 STOREMAX
054651,000730:
054652,000731: 12,2141 55366 1REV SQRT BDDV
054653,000732: 12,2142 33430 2PISC # 2PISC (+6)
054654,000733: 12,2143 77600 BOV
054655,000734: 12,2144 24145 STOREMAX
054656,000735: 12,2145 00013 STOREMAX STORE XMAX
054657,000736: 12,2146 65205 DMP PDDL
054658,000737: 12,2147 00023 1/ROOTMU
|
|
Page 1278
|
054660,000739: 12,2150 00011 ALPHA
054661,000740: 12,2151 65301 NORM PDDL
054662,000741: 12,2152 00047 X1
054663,000742: 12,2153 56257 SL* DDV
054664,000743: 12,2154 20173 0 -6,1
054665,000744: 12,2155 50000 BOV BMN
054666,000745: 12,2156 24172 MODDONE
054667,000746: 12,2157 24172 MODDONE # MPAC=PERIOD
054668,000747: 12,2160 51525 PERIODCH PDDL ABS # 0D=PERIOD
054669,000748: 12,2161 02303 TAU.
054670,000749: 12,2162 50025 DSU BMN
054671,000750: 12,2163 00001 0D
054672,000751: 12,2164 24172 MODDONE
054673,000752: 12,2165 77765 SIGN
054674,000753: 12,2166 02303 TAU.
054675,000754: 12,2167 16303 STODL TAU.
054676,000755: 12,2170 77650 GOTO
054677,000756: 12,2171 24160 PERIODCH
054678,000757: 12,2172 71201 MODDONE SETPD DLOAD
054679,000758: 12,2173 00001 0
054680,000759: 12,2174 02277 XKEPNEW
054681,000760: 12,2175 00025 STORE X
054682,000761: 12,2176 53165 SIGN BZE
054683,000762: 12,2177 02303 TAU.
054684,000763: 12,2200 24347 BADX
054685,000764: 12,2201 51440 BMN ABS
054686,000765: 12,2202 24347 BADX
054687,000766: 12,2203 51025 DSU BPL
054688,000767: 12,2204 00013 XMAX
054689,000768: 12,2205 24347 BADX
054690,000769: 12,2206 51145 STORBNDS DLOAD BPL
054691,000770: 12,2207 02303 TAU.
054692,000771: 12,2210 24217 STOREMIN
054693,000772: 12,2211 57545 DLOAD DCOMP
054694,000773: 12,2212 00013 XMAX
054695,000774: 12,2213 14015 STODL XMIN
054696,000775: 12,2214 11762 KEPZERO
054697,000776: 12,2215 34013 STCALL XMAX
054698,000777: 12,2216 24222 DXCOMP
054699,000778: 12,2217 77745 STOREMIN DLOAD
054700,000779: 12,2220 11762 KEPZERO
054701,000780: 12,2221 00015 STORE XMIN
054702,000781: 12,2222 57345 DXCOMP DLOAD DMPR
054703,000782: 12,2223 02303 TAU.
054704,000783: 12,2224 33421 BEE22
054705,000784: 12,2225 77646 ABS
054706,000785: 12,2226 15026 STODL EPSILONT
054707,000786: 12,2227 01553 XPREV
054708,000787: 12,2230 77621 XDIFF BDSU
054709,000788: 12,2231 00025 X
|
|
Page 1279
|
054711,000790: 12,2232 02643 STORE DELX
054712,000791:
054713,000792:
054714,000793: 12,2233 63545 KEPLOOP DLOAD DSQ
054715,000794: 12,2234 00025 X # X=XKEP
054716,000795: 12,2235 41501 NORM PUSH # 0D=XSQ (+34 OR +32 -N1) PL AT 2
054717,000796: 12,2236 00047 X1
054718,000797: 12,2237 53605 DMP SRR*
054719,000798: 12,2240 00011 ALPHA
054720,000799: 12,2241 21573 0 -6,1
054721,000800: 12,2242 34031 STCALL XI # XI=ALPHA XSQ (+6)
054722,000801: 12,2243 24462 DELTIME
054723,000802: 12,2244 44200 BOV BDSU
054724,000803: 12,2245 24355 TIMEOVFL # UNLIKELY
054725,000804: 12,2246 02303 TAU.
054726,000805: 12,2247 02645 STORE DELT # DELT=DELINDEP
054727,000806: 12,2250 44246 ABS BDSU
054728,000807: 12,2251 01026 EPSILONT
054729,000808: 12,2252 71244 BPL DLOAD
054730,000809: 12,2253 24375 KEPCONVG
054731,000810: 12,2254 00037 T
054732,000811: 12,2255 60225 DSU NORM
054733,000812: 12,2256 01551 TC
054734,000813: 12,2257 00047 X1
054735,000814: 12,2260 60325 PDDL NORM
054736,000815: 12,2261 02643 DELX
054737,000816: 12,2262 00050 X2
054738,000817: 12,2263 41260 XSU,1 DMP
054739,000818: 12,2264 00047 X2
054740,000819: 12,2265 02645 DELT
054741,000820: 12,2266 56257 SLR* DDV
054742,000821: 12,2267 21202 1,1
054743,000822: 12,2270 41542 SR1 PUSH # 0D=TRIAL DELX PL AT 2
054744,000823: 12,2271 71244 BPL DLOAD
054745,000824: 12,2272 24313 POSDELX
054746,000825: 12,2273 00025 X
054747,000826: 12,2274 00013 STORE XMAX # MOVE MAX BOUND IN
054748,000827: 12,2275 45221 BDSU DSU # PL AT 0
054749,000828: 12,2276 00015 XMIN
054750,000829: 12,2277 51000 BOV BPL
054751,000830: 12,2300 24305 NDXCHNGE
054752,000831: 12,2301 24305 NDXCHNGE
054753,000832: 12,2302 52145 DLOAD GOTO
054754,000833: 12,2303 00001 0D
054755,000834: 12,2304 24325 NEWDELX
054756,000835:
054757,000836:
054758,000837: 12,2305 45345 NDXCHNGE DLOAD DSU
054759,000838: 12,2306 00015 XMIN
054760,000839: 12,2307 00025 X
|
|
Page 1280
|
054762,000841: 12,2310 52075 DMPR GOTO # TO FORCE MPAC +2 TO ZERO
054763,000842: 12,2311 33424 DP9/10
054764,000843: 12,2312 24325 NEWDELX
054765,000844:
054766,000845:
054767,000846: 12,2313 77745 POSDELX DLOAD
054768,000847: 12,2314 00025 X
054769,000848: 12,2315 00015 STORE XMIN # MOVE MIN BOUND IN
054770,000849: 12,2316 45221 BDSU DSU # PL AT 0
054771,000850: 12,2317 00013 XMAX
054772,000851: 12,2320 50000 BOV BMN
054773,000852: 12,2321 24341 PDXCHNGE
054774,000853: 12,2322 24341 PDXCHNGE
054775,000854: 12,2323 77745 DLOAD
054776,000855: 12,2324 00001 0D
054777,000856: 12,2325 02643 NEWDELX STORE DELX
054778,000857: 12,2326 43254 BZE DAD
054779,000858: 12,2327 24375 KEPCONVG
054780,000859: 12,2330 00025 X
054781,000860: 12,2331 14025 STODL X
054782,000861: 12,2332 00037 T
054783,000862: 12,2333 01551 STORE TC
054784,000863: 12,2334 46034 BRNCHCTR RTB BHIZ
054785,000864: 12,2335 24716 CHECKCTR
054786,000865: 12,2336 24375 KEPCONVG
054787,000866: 12,2337 77650 GOTO
054788,000867: 12,2340 24233 KEPLOOP # ITERATE
054789,000868:
054790,000869:
054791,000870: 12,2341 45345 PDXCHNGE DLOAD DSU
054792,000871: 12,2342 00013 XMAX
054793,000872: 12,2343 00025 X
054794,000873: 12,2344 52075 DMPR GOTO # TO FORCE MPAC +2 TO ZERO
054795,000874: 12,2345 33424 DP9/10
054796,000875: 12,2346 24325 NEWDELX
054797,000876:
054798,000877:
054799,000878: 12,2347 70545 BADX DLOAD SR1
054800,000879: 12,2350 00013 XMAX
054801,000880: 12,2351 77765 SIGN
054802,000881: 12,2352 02303 TAU.
054803,000882: 12,2353 34025 STCALL X
054804,000883: 12,2354 24206 STORBNDS
054805,000884: 12,2355 50145 TIMEOVFL DLOAD BMN # X WAS TOO BIG
054806,000885: 12,2356 00025 X
054807,000886: 12,2357 24373 NEGTOVFL
054808,000887: 12,2360 00013 STORE XMAX
054809,000888: 12,2361 70545 CMNTOVFL DLOAD SR1
054810,000889: 12,2362 02643 DELX
054811,000890: 12,2363 02643 STORE DELX
|
|
Page 1281
|
054813,000892: 12,2364 44254 BZE BDSU
054814,000893: 12,2365 02267 KEPRTN
054815,000894: 12,2366 00025 X
054816,000895: 12,2367 14025 STODL X
054817,000896: 12,2370 01551 TC
054818,000897: 12,2371 34037 STCALL T
054819,000898: 12,2372 24334 BRNCHCTR
054820,000899: 12,2373 34015 NEGTOVFL STCALL XMIN
054821,000900: 12,2374 24361 CMNTOVFL
054822,000901: 12,2375 44545 KEPCONVG DLOAD SR4R
054823,000902: 12,2376 00041 R1
054824,000903: 12,2377 74225 DSU VXSC
054825,000904: 12,2400 00035 XSQC(XI)
054826,000905: 12,2401 02647 URRECT
054827,000906: 12,2402 65372 VSL1 PDDL # 0D=(R1-XSQC(XI))URRECT (+33 OR +31)
054828,000907: 12,2403 00025 X
054829,000908: 12,2404 60316 DSQ NORM
054830,000909: 12,2405 00047 X1
054831,000910: 12,2406 57275 DMPR DMPR
054832,000911: 12,2407 00023 1/ROOTMU
054833,000912: 12,2410 00025 X
054834,000913: 12,2411 53605 DMP SRR*
054835,000914: 12,2412 00033 S(XI)
054836,000915: 12,2413 21572 0 -7,1
054837,000916: 12,2414 77621 BDSU
054838,000917: 12,2415 00037 T
054839,000918: 12,2416 74352 SL1 VXSC
054840,000919: 12,2417 01511 VRECT
054841,000920: 12,2420 53372 VSL1 VAD # PL AT 0
054842,000921: 12,2421 77712 VSL4
054843,000922: 12,2422 01535 STORE RCV # RCV (+29 OR +27)
054844,000923:
054845,000924:
054846,000925: 12,2423 60246 ABVAL NORM
054847,000926: 12,2424 00050 X2
054848,000927: 12,2425 16655 STODL RCNORM
054849,000928: 12,2426 00031 XI
054850,000929: 12,2427 45275 DMPR DSU
054851,000930: 12,2430 00033 S(XI)
054852,000931: 12,2431 33406 D1/128
054853,000932: 12,2432 76405 DMP SL1R
054854,000933: 12,2433 00021 ROOTMU
054855,000934: 12,2434 53605 DMP SLR*
054856,000935: 12,2435 00025 X
054857,000936: 12,2436 56601 0 -3,2
054858,000937: 12,2437 74271 DDV VXSC
054859,000938: 12,2440 02655 RCNORM
054860,000939: 12,2441 02647 URRECT
054861,000940: 12,2442 65372 VSL1 PDDL # 0D=URRECT(XI S(XI)-1)X ROOTMU/RCV (+15
054862,000941: 12,2443 00035 XSQC(XI) # OR +13) PL AT 6
|
|
Page 1282
|
054864,000943: 12,2444 56257 SLR* DDV
054865,000944: 12,2445 56602 0 -4,2
054866,000945: 12,2446 02655 RCNORM
054867,000946: 12,2447 74221 BDSU VXSC
054868,000947: 12,2450 33422 D1/256
054869,000948: 12,2451 01511 VRECT
054870,000949: 12,2452 42455 VAD VSL8 # PL AT 0
054871,000950: 12,2453 77626 STADR
054872,000951: 12,2454 62234 STODL VCV # VCV (+7 OR +5)
054873,000952: 12,2455 00037 T
054874,000953: 12,2456 15551 STODL TC
054875,000954: 12,2457 00025 X
054876,000955: 12,2460 35553 STCALL XPREV
054877,000956: 12,2461 02267 KEPRTN
054878,000957:
|
|
Page 1283
|
054880,000959: 12,2462 77776 DELTIME EXIT # MPAC=XI (+6), 0D=XSQ (+34 OR +32 -N1)
054881,000960: 12,2463 07171 TC POLY
054882,000961: 12,2464 00010 DEC 8 B-14
054883,000962: 12,2465 02525 12526 2DEC .083333334
054884,000963: 12,2467 67356 75666 2DEC -.266666684
054885,000964: 12,2471 15001 23771 2DEC .406349155
054886,000965: 12,2473 64342 43674 2DEC -.361198675
054887,000966: 12,2475 06563 04645 2DEC .210153242
054888,000967: 12,2477 75173 52672 2DEC -.086221951
054889,000968: 12,2501 00656 14331 2DEC .026268812
054890,000969: 12,2503 77633 40512 2DEC -.006163316
054891,000970: 12,2505 00023 11210 2DEC .001177342
054892,000971: 12,2507 77774 67506 2DEC -.000199055
054893,000972: 12,2511 06006 TC INTPRET
054894,000973: 12,2512 14033 STODL S(XI)
054895,000974: 12,2513 00031 XI
054896,000975: 12,2514 77776 EXIT
054897,000976: 12,2515 07171 TC POLY
054898,000977: 12,2516 00010 DEC 8 B-14
054899,000978: 12,2517 01000 00000 2DEC .031250001
054900,000979: 12,2521 72525 52506 2DEC -.166666719
054901,000980: 12,2523 13301 15337 2DEC .355555413
054902,000981: 12,2525 62776 54733 2DEC -.406347410
054903,000982: 12,2527 11176 13267 2DEC .288962094
054904,000983: 12,2531 73410 51674 2DEC -.140117894
054905,000984: 12,2533 01446 33641 2DEC .049247387
054906,000985: 12,2535 77451 65233 2DEC -.013081923
054907,000986: 12,2537 00055 37266 2DEC .002806389
054908,000987: 12,2541 77767 52336 2DEC -.000529414
054909,000988: 12,2543 06006 TC INTPRET
|
|
Page 1284
|
054911,000990: 12,2544 53605 DMP SRR* # PL AT 0
054912,000991: 12,2545 00001 0D
054913,000992: 12,2546 21574 0 -5,1
054914,000993: 12,2547 00035 STORE XSQC(XI) # XSQC(XI) (+33 OR +31)
054915,000994: 12,2550 72405 DMP SL1
054916,000995: 12,2551 00043 KEPC1
054917,000996: 12,2552 65234 RTB PDDL # XCH WITH PL. 0D=C1 XSQ C(XI) (+49 OR +46
054918,000997: 12,2553 45657 TPMODE # PL AT 0,3
054919,000998: 12,2554 53605 DMP SRR*
054920,000999: 12,2555 00033 S(XI)
054921,001000: 12,2556 21574 0 -5,1
054922,001001: 12,2557 72405 DMP SL1
054923,001002: 12,2560 00045 KEPC2
054924,001003: 12,2561 65234 RTB PDDL # 3D=C2 XSQ S(XI) (+35 OR +33) PL AT 6
054925,001004: 12,2562 45657 TPMODE
054926,001005: 12,2563 00041 R1
054927,001006: 12,2564 76261 SR TAD # PL AT 3
054928,001007: 12,2565 20607 6
054929,001008: 12,2566 41301 NORM DMP # TO PRESERVE SIGNIF.
054930,001009: 12,2567 00047 X1
054931,001010: 12,2570 00025 X
054932,001011: 12,2571 76257 SR* TAD # X(C2 XSQ S(XI) +R1) (+49 OR +46) PL AT 0
054933,001012: 12,2572 20576 0 -3,1
054934,001013: 12,2573 57232 SL4R DMPR
054935,001014: 12,2574 00023 1/ROOTMU
054936,001015: 12,2575 00037 STORE T
054937,001016: 12,2576 77616 RVQ
054938,001017:
|
|
Page 1285
|
054940,001019: 12,2577 40001 COMSETUP SETPD BOV
054941,001020: 12,2600 00001 0D
054942,001021: 12,2601 24602 +1
054943,001022: 12,2602 76731 SSP VLOAD*
054944,001023: 12,2603 00027 ITERCTR
054945,001024: 12,2604 00024 20D
054946,001025: 12,2605 22301 MUTABLE,1
054947,001026: 12,2606 00017 STORE 1/MU
054948,001027: 12,2607 77616 RVQ
054949,001028:
054950,001029: 12,2610 71214 ITERATOR BONCLR DLOAD
054951,001030: 12,2611 00614 SLOPESW
054952,001031: 12,2612 24660 FIRSTIME
054953,001032: 12,2613 00037 DEP
054954,001033: 12,2614 60225 DSU NORM
054955,001034: 12,2615 02764 DEPREV
054956,001035: 12,2616 00047 X1
054957,001036: 12,2617 60325 PDDL NORM
054958,001037: 12,2620 00015 DELINDEP
054959,001038: 12,2621 00050 X2
054960,001039: 12,2622 41260 XSU,1 DMP
054961,001040: 12,2623 00047 X2
054962,001041: 12,2624 02762 DELDEP
054963,001042: 12,2625 56257 SLR* DDV # PL UP 2
054964,001043: 12,2626 21202 1,1
054965,001044: 12,2627 43142 SR1 BOFF
054966,001045: 12,2630 04351 ORDERSW
054967,001046: 12,2631 24634 SGNCHECK
054968,001047: 12,2632 75246 ABS SIGN # IN CASE 2ND DERIV. CHANGED SIGN, MUST
054969,001048: 12,2633 02762 DELDEP # DISREGARD IT TO FIND MIN.
054970,001049:
054971,001050: 12,2634 51006 SGNCHECK PUSH BPL # TRIAL DELINDEP PL DOWN 2
054972,001051: 12,2635 24672 POSDEL
054973,001052: 12,2636 43145 DLOAD BON
054974,001053: 12,2637 03770 INDEP
054975,001054: 12,2640 04311 ORDERSW
054976,001055: 12,2641 24643 MINCHECK
054977,001056: 12,2642 00017 STORE MAX # IF NOT 2ND ORDER, CAN MOVE MAX BOUND IN.
054978,001057:
054979,001058: 12,2643 45221 MINCHECK BDSU DSU
054980,001059: 12,2644 00011 MIN
054981,001060: 12,2645 51000 BOV BPL
054982,001061: 12,2646 24652 MODNGDEL
054983,001062: 12,2647 24652 MODNGDEL
054984,001063: 12,2650 77650 GOTO
054985,001064: 12,2651 24704 DELOK
054986,001065:
054987,001066:
054988,001067: 12,2652 45345 MODNGDEL DLOAD DSU # TRIAL DELINDEP WOULD EXCEED MIN BOUND
054989,001068: 12,2653 00011 MIN
|
|
Page 1286
|
054991,001070: 12,2654 03770 INDEP
054992,001071: 12,2655 52005 DMP GOTO
054993,001072: 12,2656 33424 DP9/10
054994,001073: 12,2657 24706 NEWDEL
054995,001074:
054996,001075:
054997,001076: 12,2660 41335 FIRSTIME SLOAD DMP
054998,001077: 12,2661 00051 TWEEKIT
054999,001078: 12,2662 00011 MIN
055000,001079: 12,2663 67206 PUSH SLOAD
055001,001080: 12,2664 00051 TWEEKIT
055002,001081: 12,2665 45205 DMP DSU
055003,001082: 12,2666 00017 MAX
055004,001083: 12,2667 52165 SIGN GOTO
055005,001084: 12,2670 02762 DELDEP
055006,001085: 12,2671 24634 SGNCHECK
055007,001086:
055008,001087:
055009,001088: 12,2672 43145 POSDEL DLOAD BON
055010,001089: 12,2673 03770 INDEP
055011,001090: 12,2674 04311 ORDERSW
055012,001091: 12,2675 24677 MAXCHECK
055013,001092: 12,2676 00011 STORE MIN # IF NOT 2ND ORDER, CAN MOVE MIN BOUND IN.
055014,001093:
055015,001094: 12,2677 45221 MAXCHECK BDSU DSU
055016,001095: 12,2700 00017 MAX
055017,001096: 12,2701 50000 BOV BMN
055018,001097: 12,2702 24710 MODPSDEL
055019,001098: 12,2703 24710 MODPSDEL
055020,001099: 12,2704 77745 DELOK DLOAD
055021,001100: 12,2705 00001 0D
055022,001101: 12,2706 00015 NEWDEL STORE DELINDEP
055023,001102: 12,2707 77616 RVQ
055024,001103:
055025,001104:
055026,001105: 12,2710 45345 MODPSDEL DLOAD DSU
055027,001106: 12,2711 00017 MAX
055028,001107: 12,2712 03770 INDEP
055029,001108: 12,2713 52005 DMP GOTO
055030,001109: 12,2714 33424 DP9/10
055031,001110: 12,2715 24706 NEWDEL
055032,001111:
055033,001112: 12,2716 44770 CHECKCTR CS ONE
055034,001113: 12,2717 50120 INDEX FIXLOC
055035,001114: 12,2720 26026 ADS ITERCTR
055036,001115: 12,2721 54154 TS MPAC
055037,001116: 12,2722 06030 TC DANZIG
055038,001117:
|
|
Page 1287
|
055040,001119: 12,2723 44545 NEWSTATE DLOAD SR4R
055041,001120: 12,2724 00041 R1
055042,001121: 12,2725 74225 DSU VXSC
055043,001122: 12,2726 00035 XSQC(XI)
055044,001123: 12,2727 02724 UR1
055045,001124: 12,2730 65372 VSL1 PDDL # 0D=(R1-XSQC(XI))UR1 (+33 OR 31) PL AT 6
055046,001125: 12,2731 00025 X
055047,001126: 12,2732 60316 DSQ NORM
055048,001127: 12,2733 00047 X1
055049,001128: 12,2734 57275 DMPR DMPR
055050,001129: 12,2735 00023 1/ROOTMU
055051,001130: 12,2736 00025 X
055052,001131: 12,2737 53605 DMP SRR*
055053,001132: 12,2740 00033 S(XI)
055054,001133: 12,2741 21572 0 -7,1
055055,001134: 12,2742 77621 BDSU
055056,001135: 12,2743 00037 T
055057,001136: 12,2744 74352 SL1 VXSC
055058,001137: 12,2745 02746 VVEC
055059,001138: 12,2746 53372 VSL1 VAD # PL AT 0
055060,001139: 12,2747 41512 VSL4 PUSH
055061,001140: 12,2750 77646 ABVAL
055062,001141: 12,2751 77701 LAMENTER NORM
055063,001142: 12,2752 00047 X1
055064,001143: 12,2753 16722 STODL R2
055065,001144: 12,2754 00031 XI
055066,001145: 12,2755 45205 DMP DSU
055067,001146: 12,2756 00033 S(XI)
055068,001147: 12,2757 33406 D1/128
055069,001148: 12,2760 76405 DMP SL1R
055070,001149: 12,2761 00021 ROOTMU
055071,001150: 12,2762 53605 DMP SLR*
055072,001151: 12,2763 00025 X
055073,001152: 12,2764 21176 0 -3,1
055074,001153: 12,2765 74271 DDV VXSC
055075,001154: 12,2766 02722 R2
055076,001155: 12,2767 02724 UR1
055077,001156: 12,2770 65372 VSL1 PDDL # 6D=V2VEC PART (+15 OR 13) PL AT 12
055078,001157: 12,2771 00035 XSQC(XI)
055079,001158: 12,2772 56257 SLR* DDV
055080,001159: 12,2773 21175 0 -4,1
055081,001160: 12,2774 02722 R2
055082,001161: 12,2775 77621 BDSU
055083,001162: 12,2776 33422 D1/256
055084,001163: 12,2777 53361 VXSC VAD
055085,001164: 12,3000 02746 VVEC # PL AT 6
055086,001165: 12,3001 43412 VSL8 RVQ
055087,001166:
|
|
Page 1288
|
055089,001168: 15,2000 SETLOC CONICS1
055090,001169: 15,2000 BANK
055091,001170:
055092,001171: 15,3402 COUNT* $$/CONIC
055093,001172: # DO NOT DISTURB THE ORDER OF THESE CDS, OVERLAYS HAVE BEEN MADE.
055094,001173: 15,3402 00000 BEE17 DEC 0 B-14 # KEEP WITH D1/8 2DEC 1.0B-17 (0000004000)
055095,001174: 15,3403 04000 00000 D1/8 2DEC 1.0 B-3
055096,001175: 15,3405 00200 00000 D1/128 2DEC 1.0 B-7
055097,001176: 15,3407 00400 00000 D1/64 2DEC 1.0 B-6
055098,001177: 15,3411 10000 00000 D1/4 2DEC 1.0 B-2
055099,001178: 15,3413 02000 00000 D1/16 2DEC 1.0 B-4
055100,001179: 15,3415 01000 00000 D1/32 2DEC 1.0 B-5
055101,001180: 15,3417 00020 00000 D1/1024 2DEC 1.0 B-10
055102,001181: 15,3421 00100 00000 D1/256 2DEC 1.0 B-8
055103,001182: 15,3423 34631 23146 DP9/10 2DEC .9
055104,001183: 15,3425 04,3761 KEPZERO EQUALS LO6ZEROS
055105,001184: 15,3425 77467 77777 -50SC 2DEC -50.0 B-12
055106,001185: 15,3427 03110 17665 2PISC 2DEC 6.28318530 B-6
055107,001186: 15,3431 15,3414 BEE19 EQUALS D1/32 -1 # 2DEC 1.0 B-19 (00000 01000)
055108,001187: 15,3431 15,3420 BEE22 EQUALS D1/256 -1 # 2DEC 1.0 B-22 (00000 00100)
055109,001188: 15,3431 00000 00001 ONEBIT 2DEC 1.0 B-28
055110,001189: 15,3433 37767 37737 COGUPLIM 2DEC .999511597
055111,001190: 15,3435 40010 40040 COGLOLIM 2DEC -.999511597
055112,001191:
|
|
Page 1289
|
055114,001193: 12,2000 SETLOC CONICS
055115,001194: 12,2000 BANK
055116,001195:
055117,001196: 12,3002 COUNT* $$/CONIC
055118,001197: 12,3002 45020 TIMETHET STQ CALL
055119,001198: 12,3003 02712 RTNTT
055120,001199: 12,3004 25763 PRAMSET
055121,001200: 12,3005 77624 CALL
055122,001201: 12,3006 37727 PARAM
055123,001202: 12,3007 45000 BOV CALL # PL AT 0
055124,001203: 12,3010 25027 COGAOVFL
055125,001204: 12,3011 25032 GETX
055126,001205: 12,3012 43145 COMMNOUT DLOAD BON
055127,001206: 12,3013 00031 XI
055128,001207: 12,3014 04310 INFINFLG
055129,001208: 12,3015 25760 ABTCONIC
055130,001209: 12,3016 45014 CLEAR CALL
055131,001210: 12,3017 04273 COGAFLAG
055132,001211: 12,3020 24462 DELTIME
055133,001212: 12,3021 45014 BON CALL
055134,001213: 12,3022 03706 RVSW
055135,001214: 12,3023 02712 RTNTT
055136,001215: 12,3024 24723 NEWSTATE
055137,001216: 12,3025 77650 GOTO
055138,001217: 12,3026 02712 RTNTT
055139,001218:
055140,001219: 12,3027 77614 COGAOVFL SETGO
055141,001220: 12,3030 04033 COGAFLAG
055142,001221: 12,3031 25760 ABTCONIC
055143,001222: 17,2000 SETLOC CONICS2
055144,001223: 17,2000 BANK
055145,001224: 17,3727 COUNT* $$/CONIC
055146,001225: 17,3727 43020 PARAM STQ CLEAR # MPAC=V1VEC, 0D=R1VEC PL AT 6
055147,001226: 17,3730 02755 RTNPRM
055148,001227: 17,3731 03665 NORMSW
055149,001228: 17,3732 77614 CLEAR
055150,001229: 17,3733 04273 COGAFLAG
055151,001230: 17,3734 45131 SSP CALL
055152,001231: 17,3735 02675 GEOMSGN
055153,001232: 17,3736 27777 37777 # GAMMA ALWAYS LESS THAN 180DEG
055154,001233: 17,3737 13717 GEOM # MPAC=SNGA (+1), 0D=CSGA (+1) PL AT 2
055155,001234: 17,3740 14045 STODL 36D # 36D=SIN GAMMA (+1) PL AT 0
055156,001235: 17,3741 56261 SR DDV
055157,001236: 17,3742 20606 5
055158,001237:
055159,001238: 17,3743 00045 36D
055160,001239: 17,3744 33770 STOVL* COGA
055161,001240: 17,3745 22301 MUTABLE,1
055162,001241: 17,3746 14017 STODL 1/MU
|
|
Page 1290
|
055164,001243: 17,3747 02722 MAGVEC2
055165,001244: 17,3750 60316 DSQ NORM
055166,001245: 17,3751 00047 X1
055167,001246: 17,3752 41275 DMPR DMP
055168,001247: 17,3753 00017 1/MU
055169,001248: 17,3754 00041 R1
055170,001249: 17,3755 77657 SRR*
055171,001250: 17,3756 21576 0 -3,1
055172,001251: 17,3757 44206 PUSH BDSU # 0D=R1 V1SQ/MU (+6) PL AT 2
055173,001252: 17,3760 33416 D1/32
055174,001253: 17,3761 16744 STODL R1A # R1A (+6) PL AT 0
055175,001254:
055176,001255: 17,3762 60205 DMP NORM
055177,001256: 17,3763 00045 36D
055178,001257: 17,3764 00047 X1
055179,001258: 17,3765 53605 DMP SR*
055180,001259: 17,3766 00045 36D
055181,001260: 17,3767 20575 0 -4,1
055182,001261: 17,3770 36742 STCALL P # P (+4)
055183,001262: 17,3771 02755 RTNPRM
055184,001263:
|
|
Page 1291
|
055186,001265: 05,2000 SETLOC CONICS4
055187,001266: 05,2000 BANK
055188,001267:
055189,001268: 05,3717 COUNT* $$/CONIC
055190,001269: 05,3717 77656 GEOM UNIT # MPAC=V2VEC, 0D=R1VEC PL AT 6
055191,001270: 05,3720 16714 STODL U2 # U2 (+1)
055192,001271: 05,3721 00045 36D
055193,001272: 05,3722 26722 STOVL MAGVEC2 # PL AT 0
055194,001273: 05,3723 77656 UNIT
055195,001274: 05,3724 02724 STORE UR1 # UR1 (+1)
055196,001275: 05,3725 72441 DOT SL1
055197,001276: 05,3726 02714 U2
055198,001277: 05,3727 77725 PDDL # OD=CSTH (+1) PL AT 2
055199,001278: 05,3730 00045 36D
055200,001279: 05,3731 24041 STOVL R1 # R1 (+29 OR +27)
055201,001280: 05,3732 02724 UR1
055202,001281: 05,3733 76435 VXV VSL1
055203,001282: 05,3734 02714 U2
055204,001283: 05,3735 75214 BON SIGN
055205,001284: 05,3736 03705 NORMSW
055206,001285: 05,3737 13751 HAVENORM
055207,001286: 05,3740 02675 GEOMSGN
055208,001287: 05,3741 40056 UNIT BOV
055209,001288: 05,3742 13747 COLINEAR
055210,001289: 05,3743 16676 UNITNORM STODL UN # UN (+1)
055211,001290: 05,3744 00045 36D
055212,001291: 05,3745 43565 SIGN RVQ # MPAC=SNTH (+1), 34D=SNTH.SNTH (+2)
055213,001292: 05,3746 02675 GEOMSGN
055214,001293:
055215,001294:
055216,001295: 05,3747 52162 COLINEAR VSR1 GOTO
055217,001296: 05,3750 13743 UNITNORM
055218,001297:
055219,001298: 05,3751 75246 HAVENORM ABVAL SIGN
055220,001299: 05,3752 02675 GEOMSGN
055221,001300: 05,3753 77616 RVQ # MPAC=SNTH (+1), 34D=SNTH.SNTH (+2)
055222,001301:
|
|
Page 1292
|
055224,001303: 12,2000 SETLOC CONICS
055225,001304: 12,2000 BANK
055226,001305:
055227,001306: 12,3032 COUNT* $$/CONIC
055228,001307: 12,3032 66374 GETX AXT,2 SSP # ASSUMES P (+4) IN MPAC
055229,001308: 12,3033 00003 3
055230,001309: 12,3034 00052 S2
055231,001310: 12,3035 00001 1
055232,001311: 12,3036 77614 CLEAR
055233,001312: 12,3037 04276 360SW
055234,001313: 12,3040 65366 SQRT PDDL # 0D=SQRT(P) PL AT 2
055235,001314: 12,3041 02734 CSTH
055236,001315: 12,3042 44342 SR1 BDSU
055237,001316: 12,3043 33412 D1/4
055238,001317: 12,3044 54325 PDDL SRR # PL AT 4D
055239,001318: 12,3045 02732 SNTH
055240,001319: 12,3046 21607 6
055241,001320: 12,3047 77671 DDV # PL AT 2
055242,001321: 12,3050 77600 BOV
055243,001322: 12,3051 25165 360CHECK
055244,001323: 12,3052 41225 DSU DMP
055245,001324: 12,3053 03770 COGA # PL AT 0
055246,001325: 12,3054 40132 SL2R BOV
055247,001326: 12,3055 25165 360CHECK
055248,001327: 12,3056 63406 WLOOP PUSH DSQ # 0D=W (+5) PL AT 2
055249,001328: 12,3057 65351 TLOAD PDDL # 2D=WSQ (+10) PL AT 5
055250,001329: 12,3060 00155 MPAC
055251,001330: 12,3061 02744 R1A
055252,001331: 12,3062 76202 SR4 TAD # PL AT 2
055253,001332: 12,3063 75440 BMN SQRT
055254,001333: 12,3064 25250 INFINITY
055255,001334: 12,3065 43306 ROUND DAD # PL AT 0D
055256,001335: 12,3066 61000 BOV TIX,2
055257,001336: 12,3067 25163 RESETX2
055258,001337: 12,3070 25056 WLOOP
055259,001338:
055260,001339:
055261,001340: 12,3071 40065 BDDV BOV
055262,001341: 12,3072 33406 D1/128
055263,001342: 12,3073 25250 INFINITY
055264,001343: 12,3074 41440 POLYCOEF BMN PUSH # 0D=1/W (+2) OR 16/W (+6) PL AT 2
055265,001344: 12,3075 25250 INFINITY
055266,001345: 12,3076 77716 DSQ
055267,001346: 12,3077 41301 NORM DMP
055268,001347: 12,3100 00047 X1
055269,001348: 12,3101 02744 R1A
055270,001349: 12,3102 77457 SRR* EXIT
055271,001350: 12,3103 21567 0 -10D,1
055272,001351: 12,3104 07171 TC POLY
055273,001352: 12,3105 00005 DEC 5 B-14
|
|
Page 1293
|
055275,001354: 12,3106 20000 00000 2DEC .5
055276,001355: 12,3110 72525 52471 2DEC -.166666770
055277,001356: 12,3112 03146 15003 2DEC .100000392
055278,001357: 12,3114 75556 45210 2DEC -.071401086
055279,001358: 12,3116 01615 13553 2DEC .055503292
055280,001359: 12,3120 76371 63777 2DEC -.047264098
055281,001360: 12,3122 01232 27367 2DEC .040694204
055282,001361:
055283,001362: 12,3124 06006 TC INTPRET
055284,001363: 12,3125 76405 DMP SL1R # PL AT 0D
055285,001364: 12,3126 43006 PUSH BON
055286,001365: 12,3127 04316 360SW
055287,001366: 12,3130 25235 TRUE360X
055288,001367: 12,3131 60316 XCOMMON DSQ NORM
055289,001368: 12,3132 00047 X1
055290,001369: 12,3133 53605 DMP SRR*
055291,001370: 12,3134 02744 R1A
055292,001371: 12,3135 21565 0 -12D,1
055293,001372: 12,3136 14031 STODL XI # XI (+6)
055294,001373:
055295,001374:
055296,001375: 12,3137 00041 R1
055297,001376: 12,3140 75542 SR1 SQRT
055298,001377: 12,3141 41306 ROUND DMP
055299,001378: 12,3142 77632 SL4R # PL AT 0
055300,001379: 12,3143 00025 STORE X # X (+17 OR +16)
055301,001380:
055302,001381:
055303,001382: 12,3144 60316 DSQ NORM
055304,001383: 12,3145 00047 X1
055305,001384: 12,3146 41325 PDDL DMP # 0D=XSQ (+34 OR +32 -N1) PL AT 2
055306,001385: 12,3147 02742 P
055307,001386: 12,3150 00041 R1
055308,001387: 12,3151 75452 SL3 SQRT
055309,001388: 12,3152 56405 DMP SL3R
055310,001389: 12,3153 03770 COGA
055311,001390: 12,3154 14043 STODL KEPC1
055312,001391: 12,3155 02744 R1A
055313,001392: 12,3156 43021 BDSU CLEAR
055314,001393: 12,3157 33410 D1/64
055315,001394: 12,3160 04270 INFINFLG
055316,001395: 12,3161 00045 STORE KEPC2
055317,001396: 12,3162 77616 RVQ
055318,001397:
|
|
Page 1294
|
055320,001399:
055321,001400: 12,3163 77774 RESETX2 AXT,2
055322,001401: 12,3164 00003 3
055323,001402:
055324,001403: 12,3165 51001 360CHECK SETPD BPL
055325,001404: 12,3166 00001 0D
055326,001405: 12,3167 25172 INVRSEQN
055327,001406: 12,3170 77614 SET
055328,001407: 12,3171 04076 360SW
055329,001408:
055330,001409:
055331,001410: 12,3172 75545 INVRSEQN DLOAD SQRT
055332,001411: 12,3173 02742 P
055333,001412: 12,3174 41325 PDDL DMP # 0D=SQRT(P) (+2) PL AT 2
055334,001413: 12,3175 02732 SNTH
055335,001414: 12,3176 03770 COGA
055336,001415: 12,3177 65352 SL1 PDDL # 2D=SNTH COGA (+5) PL AT 4
055337,001416: 12,3200 02734 CSTH
055338,001417: 12,3201 43202 SR4 DAD
055339,001418: 12,3202 33416 D1/32
055340,001419: 12,3203 41225 DSU DMP # PL AT 2,0
055341,001420: 12,3204 55301 NORM BDDV
055342,001421: 12,3205 00047 X1
055343,001422: 12,3206 02732 SNTH
055344,001423: 12,3207 51457 SLR* ABS # NOTE: NEAR 360 CASE TREATED DIFFERENTLY
055345,001424: 12,3210 21174 0 -5,1
055346,001425: 12,3211 63406 PUSH DSQ # 0D=1/W (-1) PL AT 2
055347,001426: 12,3212 14043 STODL 34D
055348,001427: 12,3213 33414 D1/16
055349,001428: 12,3214 63406 1/WLOOP PUSH DSQ # 2D=G (+4) PL AT 4
055350,001429: 12,3215 65234 RTB PDDL # PL AT 7
055351,001430: 12,3216 45657 TPMODE
055352,001431: 12,3217 02744 R1A
055353,001432: 12,3220 40405 DMP SR4
055354,001433: 12,3221 00043 34D
055355,001434: 12,3222 77771 TAD # PL AT 4
055356,001435: 12,3223 75440 BMN SQRT
055357,001436: 12,3224 25250 INFINITY
055358,001437: 12,3225 77615 DAD # PL AT 2
055359,001438: 12,3226 60304 TIX,2 NORM
055360,001439: 12,3227 25214 1/WLOOP
055361,001440: 12,3230 00047 X1
055362,001441: 12,3231 77665 BDDV
055363,001442: 12,3232 52057 SLR* GOTO # PL AT 0
055364,001443: 12,3233 21172 0 -7,1
055365,001444: 12,3234 25074 POLYCOEF
055366,001445:
055367,001446:
055368,001447: 12,3235 50145 TRUE360X DLOAD BMN
055369,001448: 12,3236 02744 R1A
|
|
Page 1295
|
055371,001450: 12,3237 25250 INFINITY
055372,001451: 12,3240 60366 SQRT NORM
055373,001452: 12,3241 00047 X1
055374,001453: 12,3242 53665 BDDV SL*
055375,001454: 12,3243 33430 2PISC
055376,001455: 12,3244 20176 0 -3,1
055377,001456: 12,3245 41425 DSU PUSH # 0D=2PI/SQRT(R1A) -X PL AT 0,2
055378,001457: 12,3246 77650 GOTO
055379,001458: 12,3247 25131 XCOMMON
055380,001459: 12,3250 40001 INFINITY SETPD BOV # NO SOLUTION EXISTS SINCE CLOSURE THROUGH
055381,001460: 12,3251 00001 0 # INFINITY IS REQUIRED
055382,001461: 12,3252 25253 OVFLCLR
055383,001462: 12,3253 43414 OVFLCLR SET RVQ
055384,001463: 12,3254 04070 INFINFLG
055385,001464:
|
|
Page 1296
|
055387,001466: 12,3255 45020 LAMBERT STQ CALL
055388,001467: 12,3256 02712 RTNLAMB
055389,001468: 12,3257 24577 COMSETUP
055390,001469: 12,3260 57345 DLOAD DMPR
055391,001470: 12,3261 02673 TDESIRED
055392,001471: 12,3262 33415 BEE19
055393,001472: 12,3263 03772 STORE EPSILONL
055394,001473: 12,3264 77214 SET VLOAD
055395,001474: 12,3265 00474 SLOPESW
055396,001475: 12,3266 02657 R1VEC
055397,001476: 12,3267 45115 PDVL CALL # 0D=R1VEC (+29 OR +27) PL AT 6
055398,001477: 12,3270 02665 R2VEC # MPAC=R2VEC (+29 OR +27)
055399,001478: 12,3271 13717 GEOM
055400,001479: 12,3272 16732 STODL SNTH # 0D=CSTH (+1) PL AT 2
055401,001480: 12,3273 02722 MAGVEC2
055402,001481: 12,3274 65301 NORM PDDL # PL AT 4
055403,001482: 12,3275 00047 X1
055404,001483: 12,3276 00041 R1
055405,001484: 12,3277 56342 SR1 DDV # PL AT 2
055406,001485: 12,3300 65257 SL* PDDL # DXCH WITH 0D, 0D=R1/R2 (+7) PL AT 0,2
055407,001486: 12,3301 20173 0 -6,1
055408,001487: 12,3302 77626 STADR
055409,001488: 12,3303 75043 STORE CSTH # CSTH (+1)
055410,001489: 12,3304 44342 SR1 BDSU
055411,001490: 12,3305 33412 D1/4
055412,001491: 12,3306 02736 STORE 1-CSTH # 1-CSTH (+2)
055413,001492:
055414,001493: 12,3307 53106 ROUND BZE
055415,001494: 12,3310 25524 360LAMB
055416,001495: 12,3311 65301 NORM PDDL # PL AT 4
055417,001496: 12,3312 00047 X1
055418,001497: 12,3313 00001 0D
055419,001498: 12,3314 56342 SR1 DDV # PL AT 2
055420,001499: 12,3315 75457 SL* SQRT
055421,001500: 12,3316 20176 0 -3,1
055422,001501: 12,3317 54325 PDDL SR # 2D=SQRT(2R1/R2(1-CSTH)) (+5) PL AT 4
055423,001502: 12,3320 02732 SNTH
055424,001503: 12,3321 20607 6
055425,001504: 12,3322 43271 DDV DAD # PL AT 2
055426,001505: 12,3323 02736 1-CSTH
055427,001506: 12,3324 77626 STADR
055428,001507: 12,3325 77760 STORE COGAMAX
055429,001508: 12,3326 50000 BOV BMN # IF OVFL, COGAMAX=COGUPLIM
055430,001509: 12,3327 25334 UPLIM # IF NEG, USE EVEN IF LT COGLOLIM, SINCE
055431,001510: 12,3330 25337 MAXCOGA # THIS WOULD BE RESET IN LAMBLOOP
055432,001511: 12,3331 50025 DSU BMN # IF COGAMAX GT COGUPLIM, COGAMAX=COGUPLIM
055433,001512: 12,3332 33434 COGUPLIM
055434,001513: 12,3333 25337 MAXCOGA # OTHERWISE OK, SO GO TO MAXCOGA
055435,001514: 12,3334 77745 UPLIM DLOAD
055436,001515: 12,3335 33434 COGUPLIM # COGUPLIM=.999511597 = MAX VALUE OF COGA
|
|
Page 1297
|
055438,001517: 12,3336 00017 STORE COGAMAX # NOT CAUSING OVFL IN R1A CALCULATION
055439,001518: 12,3337 54345 MAXCOGA DLOAD SR
055440,001519: 12,3340 02734 CSTH
055441,001520: 12,3341 20607 6
055442,001521: 12,3342 45425 DSU STADR
055443,001522: 12,3343 61037 STODL CSTH-RHO
055444,001523: 12,3344 02675 GEOMSGN
055445,001524: 12,3345 71240 BMN DLOAD
055446,001525: 12,3346 25543 LOLIM
055447,001526: 12,3347 02740 CSTH-RHO
055448,001527: 12,3350 56352 SL1 DDV
055449,001528: 12,3351 02732 SNTH
055450,001529: 12,3352 77600 BOV
055451,001530: 12,3353 25543 LOLIM
055452,001531: 12,3354 00011 MINCOGA STORE COGAMIN # COGAMIN (+5)
055453,001532: 12,3355 66214 BON SSP
055454,001533: 12,3356 00715 GUESSW
055455,001534: 12,3357 25530 NOGUESS
055456,001535: 12,3360 00051 TWEEKIT
055457,001536: 12,3361 00001 00001
055458,001537: 12,3362 77745 DLOAD
055459,001538: 12,3363 03770 COGA
055460,001539:
055461,001540:
055462,001541: 12,3364 77605 LAMBLOOP DMP
055463,001542: 12,3365 02732 SNTH
055464,001543: 12,3366 45342 SR1 DSU
055465,001544: 12,3367 02740 CSTH-RHO
055466,001545: 12,3370 65301 NORM PDDL # 0D=SNTH COGA-(CSTH-RHO) (+7+C(X1)) PL=2
055467,001546: 12,3371 00047 X1
055468,001547: 12,3372 02736 1-CSTH
055469,001548: 12,3373 56257 SL* DDV # 1-CSTH (+2) PL AT 0
055470,001549: 12,3374 20170 0 -9D,1
055471,001550: 12,3375 53040 BMN BZE
055472,001551: 12,3376 25462 NEGP
055473,001552: 12,3377 25462 NEGP
055474,001553: 12,3400 16742 STODL P # P=(1-CSTH)/(SNTH COGA-(CSTH-RHO)) (+4)
055475,001554: 12,3401 03770 COGA
055476,001555: 12,3402 43316 DSQ DAD
055477,001556: 12,3403 33420 D1/1024
055478,001557: 12,3404 41301 NORM DMP
055479,001558: 12,3405 00047 X1
055480,001559: 12,3406 02742 P
055481,001560: 12,3407 44257 SR* BDSU
055482,001561: 12,3410 20571 0 -8D,1
055483,001562: 12,3411 33416 D1/32
055484,001563: 12,3412 16744 STODL R1A # R1A=2-P(1+COGA COGA) (+6)
055485,001564:
055486,001565: 12,3413 02742 P
055487,001566: 12,3414 45000 BOV CALL
|
|
Page 1298
|
055489,001568: 12,3415 25465 HIENERGY
055490,001569: 12,3416 25032 GETX
055491,001570: 12,3417 77745 DLOAD
055492,001571: 12,3420 00037 T
055493,001572: 12,3421 16764 STODL TPREV
055494,001573: 12,3422 00031 XI
055495,001574: 12,3423 45014 BON CALL
055496,001575: 12,3424 04310 INFINFLG
055497,001576: 12,3425 25462 NEGP # HAVE EXCEEDED THEORETICAL BOUNDS
055498,001577: 12,3426 24462 DELTIME
055499,001578: 12,3427 44200 BOV BDSU
055500,001579: 12,3430 25501 BIGTIME
055501,001580: 12,3431 02673 TDESIRED
055502,001581: 12,3432 02762 STORE TERRLAMB
055503,001582: 12,3433 44246 ABS BDSU
055504,001583: 12,3434 03772 EPSILONL
055505,001584: 12,3435 47044 BPL RTB
055506,001585: 12,3436 25546 INITV
055507,001586: 12,3437 24716 CHECKCTR
055508,001587: 12,3440 43030 BHIZ BON
055509,001588: 12,3441 25511 SUFFCHEK
055510,001589: 12,3442 00714 SLOPESW
055511,001590: 12,3443 25451 GOITER
055512,001591: 12,3444 45345 DLOAD DSU
055513,001592: 12,3445 00037 T
055514,001593: 12,3446 02764 TPREV
055515,001594: 12,3447 77654 BZE
055516,001595: 12,3450 25511 SUFFCHEK
055517,001596: 12,3451 77624 GOITER CALL
055518,001597: 12,3452 24610 ITERATOR
055519,001598: 12,3453 53145 DLOAD BZE
055520,001599: 12,3454 00155 MPAC
055521,001600: 12,3455 25511 SUFFCHEK
055522,001601: 12,3456 77615 DAD
055523,001602: 12,3457 03770 COGA
055524,001603: 12,3460 37770 STCALL COGA
055525,001604: 12,3461 25364 LAMBLOOP
055526,001605:
055527,001606:
055528,001607: 12,3462 51145 NEGP DLOAD BPL # IMPOSSIBLE TRAJECTORY DUE TO INACCURATE
055529,001608: 12,3463 00015 DCOGA # BOUND CALCULATION. TRY NEW COGA.
055530,001609: 12,3464 25504 LOENERGY
055531,001610:
055532,001611: 12,3465 71201 HIENERGY SETPD DLOAD # HIGH ENERGY TRAJECTORY RESULTED
055533,001612: 12,3466 00001 0
055534,001613: 12,3467 03770 COGA # IN OVFL OF P OR R1A, OR XI EXCEEDING 50.
055535,001614: 12,3470 00011 STORE COGAMIN # THIS IS THE NEW BOUND.
055536,001615: 12,3471 70545 COMMONLM DLOAD SR1
055537,001616: 12,3472 00015 DCOGA
|
|
Page 1299
|
055539,001618: 12,3473 00015 STORE DCOGA # USE DCOGA/2 AS DECREMENT
055540,001619: 12,3474 44254 BZE BDSU
055541,001620: 12,3475 25511 SUFFCHEK
055542,001621: 12,3476 03770 COGA
055543,001622: 12,3477 37770 STCALL COGA
055544,001623: 12,3500 25364 LAMBLOOP
055545,001624:
055546,001625:
055547,001626: 12,3501 77745 BIGTIME DLOAD
055548,001627: 12,3502 02764 TPREV
055549,001628: 12,3503 00037 STORE T
055550,001629:
055551,001630:
055552,001631: 12,3504 71201 LOENERGY SETPD DLOAD # LOW ENERGY TRAJECTORY RESULTED
055553,001632: 12,3505 00001 0
055554,001633: 12,3506 03770 COGA # IN OVERFLOW OF TIME.
055555,001634: 12,3507 34017 STCALL COGAMAX # THIS IS THE NEW BOUND.
055556,001635: 12,3510 25471 COMMONLM
055557,001636:
055558,001637:
055559,001638: 12,3511 51545 SUFFCHEK DLOAD ABS
055560,001639: 12,3512 02762 TERRLAMB
055561,001640: 12,3513 41325 PDDL DMP # PL AT 2D
055562,001641: 12,3514 02673 TDESIRED
055563,001642: 12,3515 33412 D1/4
055564,001643: 12,3516 45215 DAD DSU # PL AT 0D
055565,001644: 12,3517 33432 ONEBIT
055566,001645: 12,3520 43044 BPL SETGO
055567,001646: 12,3521 25546 INITV
055568,001647: 12,3522 02434 SOLNSW
055569,001648: 12,3523 02712 RTNLAMB
055570,001649:
055571,001650:
055572,001651: 12,3524 43001 360LAMB SETPD SETGO # LAMBERT CANNOT HANDLE CSTH=1
055573,001652: 12,3525 00001 0
055574,001653: 12,3526 02434 SOLNSW
055575,001654: 12,3527 02712 RTNLAMB
055576,001655:
055577,001656:
055578,001657: 12,3530 71331 NOGUESS SSP DLOAD
055579,001658: 12,3531 00051 TWEEKIT
055580,001659: 12,3532 10000 20000
055581,001660: 12,3533 00011 COGAMIN
055582,001661: 12,3534 65342 SR1 PDDL # PL AT 2
055583,001662: 12,3535 00017 COGAMAX
055584,001663: 12,3536 43342 SR1 DAD
055585,001664: 12,3537 77626 STADR # PL AT 0
055586,001665: 12,3540 74007 STORE COGA
055587,001666: 12,3541 34015 STCALL DCOGA
055588,001667: 12,3542 25364 LAMBLOOP
|
|
Page 1300
|
055590,001669: 12,3543 52145 LOLIM DLOAD GOTO
055591,001670: 12,3544 33436 COGLOLIM # COGLOLIM=-.999511597
055592,001671: 12,3545 25354 MINCOGA
055593,001672:
055594,001673:
055595,001674: 12,3546 60345 INITV DLOAD NORM
055596,001675: 12,3547 00041 R1
055597,001676: 12,3550 00047 X1
055598,001677: 12,3551 70525 PDDL SR1 # PL AT 2
055599,001678: 12,3552 02742 P
055600,001679: 12,3553 77671 DDV # PL AT 0
055601,001680: 12,3554 75457 SL* SQRT
055602,001681: 12,3555 20175 0 -4,1
055603,001682: 12,3556 72405 DMP SL1
055604,001683: 12,3557 00021 ROOTMU
055605,001684: 12,3560 41206 PUSH DMP # 0D=VTAN (+7) PL AT 2
055606,001685: 12,3561 03770 COGA
055607,001686: 12,3562 74261 SL VXSC
055608,001687: 12,3563 20206 5
055609,001688: 12,3564 02724 UR1
055610,001689: 12,3565 77725 PDDL # XCH WITH 0D PL AT 0,6
055611,001690: 12,3566 76561 VXSC VSL1
055612,001691: 12,3567 02676 UN
055613,001692: 12,3570 53235 VXV VAD # PL AT 0
055614,001693: 12,3571 02724 UR1
055615,001694: 12,3572 43172 VSL1 CLEAR
055616,001695: 12,3573 02674 SOLNSW
055617,001696: 12,3574 02746 STORE VVEC
055618,001697: 12,3575 53135 SLOAD BZE
055619,001698: 12,3576 02704 VTARGTAG
055620,001699: 12,3577 25602 TARGETV
055621,001700: 12,3600 77650 GOTO
055622,001701: 12,3601 02712 RTNLAMB
055623,001702:
055624,001703:
055625,001704: 12,3602 45145 TARGETV DLOAD CALL
055626,001705: 12,3603 02722 MAGVEC2
055627,001706: 12,3604 24751 LAMENTER
055628,001707: 12,3605 36705 STCALL VTARGET
055629,001708: 12,3606 02712 RTNLAMB
055630,001709:
|
|
Page 1301
|
055632,001711: 12,3607 45020 TIMERAD STQ CALL
055633,001712: 12,3610 02712 RTNTR
055634,001713: 12,3611 25763 PRAMSET
055635,001714: 12,3612 77624 CALL
055636,001715: 12,3613 37727 PARAM
055637,001716: 12,3614 71200 BOV DLOAD # PL AT 0
055638,001717: 12,3615 25027 COGAOVFL
055639,001718: 12,3616 33416 D1/32
055640,001719: 12,3617 41225 DSU DMP
055641,001720: 12,3620 02744 R1A
055642,001721: 12,3621 02742 P
055643,001722: 12,3622 41366 SQRT DMP
055644,001723: 12,3623 03770 COGA
055645,001724: 12,3624 74212 SL4 VXSC
055646,001725: 12,3625 02714 U2
055647,001726: 12,3626 45325 PDDL DSU # PL AT 6
055648,001727: 12,3627 33410 D1/64
055649,001728: 12,3630 02744 R1A
055650,001729: 12,3631 52361 VXSC VSU # PL AT 0
055651,001730: 12,3632 02724 UR1
055652,001731: 12,3633 53512 VSL4 UNIT
055653,001732: 12,3634 77600 BOV
055654,001733: 12,3635 25713 CIRCULAR
055655,001734: 12,3636 60325 PDDL NORM # 0D=UNIT(ECC) (+3) PL AT 6
055656,001735: 12,3637 02760 RDESIRED # 36D=ECC (+3)
055657,001736: 12,3640 00047 X1
055658,001737: 12,3641 41325 PDDL DMP # PL AT 8
055659,001738: 12,3642 00041 R1
055660,001739: 12,3643 02742 P
055661,001740: 12,3644 56257 SL* DDV # PL AT 6
055662,001741: 12,3645 20201 0,1
055663,001742: 12,3646 56225 DSU DDV
055664,001743: 12,3647 33414 D1/16
055665,001744: 12,3650 00045 36D # 36D=ECC (+3)
055666,001745: 12,3651 00031 STORE COSF
055667,001746: 12,3652 63400 BOV DSQ
055668,001747: 12,3653 20453 BADR2
055669,001748: 12,3654 50021 BDSU BMN
055670,001749: 12,3655 33412 D1/4
055671,001750: 12,3656 20453 BADR2
055672,001751: 12,3657 75366 SQRT SIGN
055673,001752: 12,3660 02757 SGNRDOT
055674,001753: 12,3661 77614 CLEAR
055675,001754: 12,3662 04272 APSESW
055676,001755:
055677,001756: 12,3663 76561 TERMNVEC VXSC VSL1
055678,001757: 12,3664 02676 UN
055679,001758: 12,3665 63235 VXV PDVL # VXCH WITH 0D PL AT 0,6
055680,001759: 12,3666 00001 0D
055681,001760: 12,3667 53361 VXSC VAD # PL AT 0
|
|
Page 1302
|
055683,001762: 12,3670 00031 COSF
055684,001763: 12,3671 41572 VSL1 PUSH # 0D=U2 PL AT 6
055685,001764:
055686,001765: 12,3672 56241 DOT DDV # LIMITS RESULT TO POSMAX OR NEGMAX
055687,001766: 12,3673 02724 UR1
055688,001767: 12,3674 33412 DP1/4
055689,001768: 12,3675 40142 SR1 BOV # SCALE BACK DOWN TO NORMAL
055690,001769: 12,3676 25677 +1 # CLEAR OVFIND IF SET
055691,001770: 12,3677 26734 STOVL CSTH # CSTH (+1)
055692,001771: 12,3700 02724 UR1
055693,001772: 12,3701 76435 VXV VSL1
055694,001773: 12,3702 72441 DOT SL1
055695,001774: 12,3703 02676 UN
055696,001775: 12,3704 16732 STODL SNTH # SNTH (+1)
055697,001776: 12,3705 02742 P
055698,001777: 12,3706 77624 CALL
055699,001778: 12,3707 25032 GETX
055700,001779: 12,3710 77614 CLRGO
055701,001780: 12,3711 02634 SOLNSW
055702,001781: 12,3712 25012 COMMNOUT
055703,001782:
055704,001783:
055705,001784: 12,3713 43001 CIRCULAR SETPD SETGO
055706,001785: 12,3714 00001 0
055707,001786: 12,3715 02434 SOLNSW
055708,001787: 12,3716 25760 ABTCONIC
055709,001788:
055710,001789:
055711,001790: 10,2000 SETLOC CONICS5
055712,001791: 10,2000 BANK
055713,001792:
055714,001793: 10,2453 COUNT* $$/CONIC
055715,001794: 10,2453 75345 BADR2 DLOAD SIGN
055716,001795: 10,2454 11760 LODPHALF
055717,001796: 10,2455 00031 COSF
055718,001797: 10,2456 14031 STODL COSF
055719,001798: 10,2457 11762 KEPZERO
055720,001799: 10,2460 77614 SETGO
055721,001800: 10,2461 04032 APSESW
055722,001801: 10,2462 25663 TERMNVEC
055723,001802:
|
|
Page 1303
|
055725,001804: 12,2000 SETLOC CONICS
055726,001805: 12,2000 BANK
055727,001806:
055728,001807: 12,3717 COUNT* $$/CONIC
055729,001808: 12,3717 45020 APSIDES STQ CALL
055730,001809: 12,3720 02712 RTNAPSE
055731,001810: 12,3721 25763 PRAMSET
055732,001811: 12,3722 77624 CALL
055733,001812: 12,3723 37727 PARAM
055734,001813: 12,3724 77600 BOV # PL AT 0
055735,001814: 12,3725 25726 GETECC
055736,001815: 12,3726 42405 GETECC DMP SL4
055737,001816: 12,3727 02744 R1A
055738,001817: 12,3730 75421 BDSU SQRT
055739,001818: 12,3731 33410 D1/64
055740,001819: 12,3732 02754 STORE ECC
055741,001820: 12,3733 65215 DAD PDDL # PL AT 2
055742,001821: 12,3734 33404 D1/8
055743,001822: 12,3735 00041 R1
055744,001823: 12,3736 72405 DMP SL1
055745,001824: 12,3737 02742 P
055746,001825: 12,3740 77671 DDV # PL AT 0
055747,001826: 12,3741 60325 PDDL NORM # 0D=RP (+29 OR +27) PL AT 2
055748,001827: 12,3742 02744 R1A
055749,001828: 12,3743 00047 X1
055750,001829: 12,3744 53725 PDDL SL* # PL AT 4
055751,001830: 12,3745 00041 R1
055752,001831: 12,3746 20174 0 -5,1
055753,001832: 12,3747 45271 DDV DSU # PL AT 2,0
055754,001833: 12,3750 50000 BOV BMN
055755,001834: 12,3751 25755 INFINAPO
055756,001835: 12,3752 25755 INFINAPO
055757,001836: 12,3753 77650 GOTO
055758,001837: 12,3754 02712 RTNAPSE
055759,001838: 12,3755 52145 INFINAPO DLOAD GOTO # RETURNS WITH APOAPSIS IN MPAC,PERIAPSIS
055760,001839: 12,3756 11773 LDPOSMAX
055761,001840: 12,3757 02712 RTNAPSE # THAT PL IS AT 0.
055762,001841:
|
|
Page 1304
|
055764,001843: 12,3760 77776 ABTCONIC EXIT
055765,001844: 12,3761 05726 TC POODOO
055766,001845: 12,3762 20607 OCT 20607 # NO SOLUTION FROM TIMETHET OR TIMERAD
055767,001846:
|
|
Page 1305
|
055769,001848: 12,3763 40001 PRAMSET SETPD BOV
055770,001849: 12,3764 00001 0D
055771,001850: 12,3765 25766 +1
055772,001851: 12,3766 63375 VLOAD PDVL
055773,001852: 12,3767 02657 RVEC
055774,001853: 12,3770 02746 VVEC
055775,001854: 12,3771 77616 RVQ
055776,001855:
055777,001856: 11,2000 SETLOC CONICS3
055778,001857: 11,2000 BANK
055779,001858:
055780,001859: 11,2300 COUNT* $$/CONIC
055781,001860: 11,2300 22437 16067 MUTABLE 2DEC* 3.986032 E10 B-36* # MUE
055782,001861: 11,2302 15625 21042 2DEC* .25087606 E-10 B+34* # 1/MUE
055783,001862: 11,2304 30276 04773 2DEC* 1.99650495 E5 B-18* # SQRT(MUE)
055784,001863: 11,2306 25004 06702 2DEC* .50087529 E-5 B+17* # 1/SQRT(MUE)
055785,001864:
055786,001865: 11,2310 16471 01352 2DEC 4.902778 E8 B-30 # MUM
055787,001866: 11,2312 21412 20500 2DEC .203966 E-8 B+28 # 1/MUM
055788,001867: 11,2314 25477 03367 2DEC* 2.21422176 E4 B-15* # SQRT(MUM)
055789,001868: 11,2316 27533 07571 2DEC* .45162595 E-4 B+14* # 1/SQRT(MUM)
055790,001869:
055791,001870: 11,2320 04,3772 LDPOSMAX EQUALS LODPMAX # DPPOSMAX IN LOW MEMORY.
055792,001871:
055793,001872: # ERASABLE ASSIGNMENTS
055794,001873:
055795,001874:
055796,001875: # KEPLER SUBROUTINE
055797,001876:
055798,001877: # INPUT -
055799,001878: # RRECT ERASE +5
055800,001879: # VRECT ERASE +5
055801,001880: # TAU. ERASE +1
055802,001881: # XKEP ERASE +1
055803,001882: # TC ERASE +1
055804,001883: # XPREV ERASE +1
055805,001884: 11,2320 1/MU EQUALS 14D
055806,001885: 11,2320 ROOTMU EQUALS 16D
055807,001886: 11,2320 1/ROOTMU EQUALS 18D
055808,001887:
055809,001888: # OUTPUT -
055810,001889: # RCV ERASE +5
|
|
Page 1306
|
055812,001891: # VCV ERASE +5
055813,001892: # RC ERASE +1
055814,001893: # XPREV ERASE +1
055815,001894:
055816,001895: # DEBRIS -
055817,001896: 11,2320 ALPHA EQUALS 8D
055818,001897: 11,2320 XMAX EQUALS 10D
055819,001898: 11,2320 XMIN EQUALS 12D
055820,001899: 11,2320 X EQUALS 20D
055821,001900: 11,2320 XI EQUALS 24D
055822,001901: 11,2320 S(XI) EQUALS 26D
055823,001902: 11,2320 XSQC(XI) EQUALS 28D
055824,001903: 11,2320 T EQUALS 30D
055825,001904: 11,2320 R1 EQUALS 32D
055826,001905: 11,2320 KEPC1 EQUALS 34D
055827,001906: 11,2320 KEPC2 EQUALS 36D
055828,001907: # DELX ERASE +1
055829,001908: # DELT ERASE +1
055830,001909: # URRECT ERASE +5
055831,001910: # RCNORM ERASE +1
055832,001911: # XPREV EQUALS XKEP
055833,001912:
055834,001913:
055835,001914: # LAMBERT SUBROUTINE
055836,001915:
055837,001916: # INPUT -
055838,001917: # R1VEC ERASE +5
055839,001918: # R2VEC ERASE +5
055840,001919: # TDESIRED ERASE +1
055841,001920: # GEOMSGN ERASE +0
055842,001921: # GUESSW 0 IF COGA GUESS AVAILABLE, 1 IF NOT
055843,001922: # COGA ERASE +1 INPUT ONLY IF GUESSW IS ZERO.
055844,001923: # NORMSW 0 IF UN TO BE COMPUTED, 1 IF UN INPUT
055845,001924: # UN ERASE +5 ONLY USED IF NORMSW IS 1
055846,001925: # VTARGTAG ERASE +0
055847,001926: # TWEEKIT EQUALS 40D ONLY USED IF GUESSW IS 0
055848,001927:
055849,001928: # OUTPUT -
055850,001929: # VTARGET ERASE +5 AVAILABLE ONLY IF VTARGTAG IS ZERO.
055851,001930: # V1VEC EQUALS MPAC
055852,001931:
055853,001932: # DEBRIS -
055854,001933: # RTNLAMB ERASE +0
055855,001934: # U2 ERASE +5
055856,001935: # MAGVEC2 ERASE +1
055857,001936: # UR1 ERASE +5
055858,001937: # R1 EQUALS 31D
055859,001938: # UN ERASE +5
055860,001939: # SNTH ERASE +1
055861,001940: # CSTH ERASE +1
|
|
Page 1307
|
055863,001942: # 1-CSTH ERASE +1
055864,001943: # CSTH-RHO ERASE +1
055865,001944: 11,2320 COGAMAX EQUALS 14D # CLOBBERS 1/MU
055866,001945: 11,2320 COGAMIN EQUALS 8D
055867,001946: 11,2320 DCOGA EQUALS 12D
055868,001947: # TWEEKIT EQUALS 40D
055869,001948: # P ERASE +1
055870,001949: # COGA ERASE +1
055871,001950: # R1A ERASE +1
055872,001951: # X EQUALS 20D
055873,001952: # XSQ EQUALS 22D
055874,001953: # XI EQUALS 24D
055875,001954: # S(XI) EQUALS 26D
055876,001955: # XSQC(XI) EQUALS 28D
055877,001956: # T EQUALS 30D
055878,001957: # KEPC1 EQUALS 34D
055879,001958: # KEPC2 EQUALS 36D
055880,001959: # SLOPESW
055881,001960: # SOLNSW
055882,001961:
055883,001962: # OTHERS -
055884,001963:
055885,001964: # RVEC EQUALS R1VEC
055886,001965: # VVEC ERASE +5
055887,001966: # COGAFLAG
055888,001967: # RVSW
055889,001968: # INFINFLG
055890,001969: # APSESW
055891,001970: # 360SW
055892,001971: # RTNTT EQUALS RTNLAMB
055893,001972: # ECC ERASE +1
055894,001973: # RTNTR EQUALS RTNLAMB
055895,001974: # RTNAPSE EQUALS RTNLAMB
055896,001975: # R2 EQUALS MAGVEC2
055897,001976: 11,2320 COSF EQUALS 24D
055898,001977: # RTNPRM ERASE +0
055899,001978: # SGNRDOT ERASE +0
055900,001979: # RDESIRED ERASE +1
055901,001980:
055902,001981:
055903,001982: # ITERATOR SUBROUTINE
055904,001983:
055905,001984: # ORDERSW
055906,001985: 11,2320 MAX EQUALS 14D # CLOBBERS 1/MU
055907,001986: 11,2320 MIN EQUALS 8D
055908,001987: # INDEP ERASE +1
055909,001988: 11,2320 DELINDEP EQUALS 12D
055910,001989: 11,2320 ITERCTR EQUALS 22D
055911,001990: 11,2320 DEP EQUALS 30D
055912,001991: # DELDEP ERASE +1
055913,001992: # DEPREV ERASE +1
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Page 1308
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055915,001994: 11,2320 TWEEKIT EQUALS 40D
055916,001995:
055917,001996:
055918,001997: # MORE KEPLER
055919,001998:
055920,001999: # EPSILONT ERASE +1
055921,002000:
055922,002001:
055923,002002: # MORE LAMBERT
055924,002003:
055925,002004: # TERRLAMB EQUALS DELDEP
055926,002005: # TPREV EQUALS DEPREV
055927,002006:
055928,002007: # EPSILONL EQUALS EPSILONT +2 DOUBLE PRECISION WORD
End of include-file CONIC_SUBROUTINES.agc. Parent file is MAIN.agc