Source Code
These source-code files are part of a reconstructed copy of Comanche 51, the
initial release (though not the final mission release) of the Apollo 11
Command Module (CM) Apollo Guidance Computer (AGC) software. The flown, final
release was Comanche 55. The reconstruction is believed to be exactly accurate,
but in the absence of an actual Apollo-era listing of Comanche 51, some
explanation of the reconstruction process is needed to insure confidence in
that accuracy.
The starting point was the source code of Comanche 55, whose original source code is available. Comanche 55 source code was then modified by undoing changes known to have been made between revisions 51 and 55. The most-significant steps involved reverting changes related to the R-2 lunar potential model, the details of which were known from the previous, separate, independent reconstruction of the Apollo 10 Lunar Module software Luminary 69/2. The now-reconstructed Comanche 51 source code was verified by assembling it and checking that the assembled code had the expected known-correct memory-bank checksums. Note that page numbers in the reconstructed code match those on the Comanche 55 or Luminary 69 printouts, although the source code would likely have different page numbers in a contemporary Comanche 51 listing. Annotations that were not present in the contemporary source code have been added to the reconstructed code to justify each change relative to Comanche 55. Here's a guide to some of the Apollo documentation relevant to those annotations:
Comments expected to have been present in the original source code are prefixed with a single '#' symbol, whereas comments added later are prefixed by "##" or "###". Report any errors noted by creating an issue report at the Virtual AGC Project's GitHub repository. |
053677,000002: ## Copyright: Public domain.
053678,000003: ## Filename: CONIC_SUBROUTINES.agc
053679,000004: ## Purpose: A section of Comanche revision 051.
053680,000005: ## It is part of the reconstructed source code for the
053681,000006: ## original release of the flight software for the Command
053682,000007: ## Module's (CM) Apollo Guidance Computer (AGC) for Apollo 11.
053683,000008: ## The code has been recreated from a copy of Comanche 055. It
053684,000009: ## has been adapted such that the resulting bugger words
053685,000010: ## exactly match those specified for Comanche 51 in NASA drawing
053686,000011: ## 2021153D, which gives relatively high confidence that the
053687,000012: ## reconstruction is correct.
053688,000013: ## Reference: pp. 1262-1308
053689,000014: ## Assembler: yaYUL
053690,000015: ## Contact: Ron Burkey <info@sandroid.org>.
053691,000016: ## Website: www.ibiblio.org/apollo/index.html
053692,000017: ## Mod history: 2019-07-30 MAS Created from Comanche 55.
053693,000018:
Page 1262 |
053695,000020: # PROGRAM DESCRIPTION - ENTIRE CONIC SUBROUTINE LOG SECTION DATE - 1 SEPTEMBER 1967
053696,000021: # MOD NO. - 0 LOG SECTION - CONIC SUBROUTINES
053697,000022: # MOD BY KRAUSE ASSEMBLY - COLOSSUS REVISION 88
053698,000023:
053699,000024: # FUNCTIONAL DESCRIPTION -
053700,000025: # THE FOLLOWING SET OF SUBROUTINES SOLVE VARIOUS PROBLEMS INVOLVING THE TRAJECTORY PRODUCED BY A CENTRAL
053701,000026: # INVERSE-SQUARE FORCE ACTING ON A POINT MASS, AS OUTLINED IN THE CMC AND LGC LUNAR LANDING MISSION GSOP, SECTION
053702,000027: # 5.5.1.2. A GENERAL USAGE POINT-OF-VIEW WAS TAKEN IN FORMULATING, MECHANIZING, AND SCALING THE SUBROUTINES,
053703,000028: # RATHER THAN OPTIMIZING EACH FOR A PARTICULAR USE. THEREFORE, MULTIPLE USAGE CAN BE MADE OF THE SUBROUTINES
053704,000029: # INVOLVING ANY REALISTIC SET OF CONSTRAINTS. IT SHOULD BE NOTED THAT ONLY ONE SET OF CODING IS USED, WHETHER THE
053705,000030: # EARTH, MOON, OR ANY OTHER CELESTIAL BODY IS SPECIFIED AS THE CENTRAL BODY OF THE PROBLEM, PROVIDED ONE OBSERVES
053706,000031: # THE INHERENT SCALE CHANGE REQUIRED IN POSITION, VELOCITY, MU, AND TIME, AS OUTLINED IN MISSION PROGRAMMING
053707,000032: # DEFINITION MEMO NO. 10. THIS CAN BE ACCOMPLISHED BY SIMPLY ADDING TO THE MUTABLE AND INITIALIZING THE SUBROU-
053708,000033: # TINES APPROPRIATELY.
053709,000034:
053710,000035: # DUE TO THE UNIFORMITY OF THE EQUATIONS INVOLVED, CODING WAS MINIMIZED BY TREATING INDIVIDUAL EQUATIONS AND
053711,000036: # BLOCKS OF EQUATIONS AS SUBROUTINES OF LOWER RANK WHENEVER POSSIBLE. AS A RESULT, THREE BY-PRODUCTS SUBROUTINES,
053712,000037: # DIRECTLY USABLE AS INDEPENDENT SUBROUTINES, WERE GENERATED.
053713,000038:
053714,000039: # RESTRICTIONS -
053715,000040: # THE ONLY LIMITATION IN THE SCOPE OF PROBLEM WHICH CAN BE SOLVED BY A PARTICULAR SUBROUTINE IS THE SCALING
053716,000041: # LIMIT OF EACH PARAMETER AS SPECIFIED IN THE GSOP. THESE SCALING LIMITS WERE CHOSEN SO THAT ALL FEASIBLE TRAJEC-
053717,000042: # TORIES COULD BE HANDLED.
053718,000043:
053719,000044: # SINCE THE SUBROUTINES (EXCEPT KEPLER) USE COMMON SUBROUTINES OF LOWER RANK WHICH USE ERASABLE OTHER THAN
053720,000045: # THE PUSHLIST (DUE TO ITS LIMITED SIZE) AND COMMON INTERPRETIVE SWITCHES, THE CONIC SUBROUTINES CANNOT BE ALLOWED
053721,000046: # TO INTERRUPT EACH OTHER. IT IS UP TO THE USER TO GUARANTEE THIS CONDITION.
053722,000047:
Page 1263 |
053724,000049: # PROGRAM DESCRIPTION - KEPLER SUBROUTINE DATE - 11 OCTOBER 1967
053725,000050: # MOD NO. - 1 LOG SECTION - CONIC SUBROUTINES
053726,000051: # MOD BY KRAUSE ASSEMBLY - COLOSSUS 103 AND SUNDANCE 222
053727,000052: # MOD NO. - 2 (AUGUST 1968) BY ROBERTSON: TO PERMIT BACKDATING BY MORE THAN ONE ORBITAL PERIOD.
053728,000053: # MOD NO. - 3 (DEC 1968) BY ROBERTSON: SUPPRESSION OF X-MODULO-ING
053729,000054: # MOD. NO. - 4 (JAN 1969) BY ROBERTSON: CLEAR OVFIND AT KEPLER ENTRY
053730,000055:
053731,000056: # FUNCTIONAL DESCRIPTION -
053732,000057: # THIS SUBROUTINE, GIVEN AN INITIAL STATE VECTOR AND THE DESIRED TRANSFER TIME THROUGH WHICH THE STATE IS TO
053733,000058: # BE UPDATED ALONG A CONIC TRAJECTORY, COMPUTES THE NEW, UPDATED STATE VECTOR. THE TRAJECTORY MAY BE ANY CONIC
053734,000059: # SECTION - CIRCULAR, ELLIPTIC, PARABOLIC, HYPERBOLIC, OR RECTILINEAR WITH RESPECT TO THE EARTH OR THE MOON. THE
053735,000060: # USE OF THE SUBROUTINE CAN BE EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT
053736,000061: # INTRODUCING ANY CODING CHANGES, ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY. AN ITERA-
053737,000062: # TION TECHNIQUE IS UTILIZED IN THE COMPUTATION.
053738,000063:
053739,000064: # IF A NEGATIVE TIME-OF-FLIGHT IS INPUT, THE PROGRAM WILL SOLVE FOR THE STATE WHICH WOULD BE PRODUCED BY
053740,000065: # EXTRAPOLATING THE POSITION BACKWARD IN TIME.
053741,000066:
053742,000067: # IF THE ABSOLUTE VALUE OF THE DESIRED TRANSFER TIME EXCEEDS THE ORBITAL PERIOD, THE SUBROUTINE, THROUGH A
053743,000068: # MODULAR TECHNIQUE, WILL COMPUTE THE STATE CORRESPONDING TO THE DESIRED TIME (WHETHER POSITIVE OR NEGATIVE).
053744,000069:
053745,000070: # THE RESTRICTIONS ARE -
053746,000071: # 1. (PREVIOUS RESTRICTION ON THE NEGATIVE DESIRED TRANSFER TIME IS NOW DELETED.)
053747,000072: # 2. THE PARAMETERS IN THE PROBLEM CANNOT EXCEED THEIR SCALING LIMITS AS SPECIFIED IN THE GSOP. IF
053748,000073: # ANY OF THESE LIMITS ARE EXCEEDED, THE RESULTING SOLUTION WILL BE MEANINGLESS.
053749,000074:
053750,000075: # THE NUMBER OF ITERATIONS AND, THEREFORE, THE COMPUTATION SPEED IS DEPENDENT ON THE ACCURACY OF THE
053751,000076: # GUESS, XKFPNEW. THE AGC COMPUTATION TIME IS APPROXIMATELY .061 SECONDS FOR INITIALIZATION, .065 SECONDS FOR THE
053752,000077: # FINAL COMPUTATIONS, PLUS .083 SECONDS FOR EACH ITERATION.
053753,000078:
053754,000079: # REFERENCES -
053755,000080: # R-479, MISSION PROGRAMMING DEFINITION MEMO NO. 10, LUNAR LANDING MISSION GSOP, SECTION 5.5, SGA
053756,000081: # MEMO 67-4.
053757,000082:
053758,000083: # INPUT - ERASABLE INITIALIZATION REQUIRED
053759,000084: # * SCALE FACTOR *
053760,000085: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
053761,000086: # --------*--------------* -----------------------
053762,000087: # RRECT * +29 FOR EARTH*DP INITIAL POSITION VECTOR IN METERS
053763,000088: # * +27 FOR MOON *
Page 1264 |
053765,000090: # VRECT * +7 FOR EARTH *DP INITIAL VELOCITY VECTOR IN METERS/CENTISECOND
053766,000091: # * +5 FOR MOON *
053767,000092: # X1 (38D)* NONE *INDEX REGISTER SET TO -2D OR -10D ACCORDING TO WHETHER THE EARTH OR MOON,
053768,000093: # * *RESPECTIVELY, IS THE CENTRAL BODY
053769,000094: # TAU. * +28 *DESIRED TRANSFER TIME IN CENTISECONDS (DP)
053770,000095: # * * MAY BE POS OR NEG AND ABSOLUTE VALUE MAY BE GREATER OR LESS THAN ONE ORBITAL PERIOD.
053771,000096: # XKEPNEW * +17 FOR EARTH*DP GUESS OF ROOT X OF KEPLERS EQN IN SQRT(METERS).SIGN SHOULD AGREE WITH THAT OF TAU.
053772,000097: # * +16 FOR MOON * AND ABS VALUE SHOULD BE LESS THAN THAT CORRESPONDING TO A PERIOD, VIZ, 2PI SQRT(SEMI-
053773,000098: # * * MAJOR AXIS), FOR SPEED OF CONVERGENCE, BUT IF EITHER CONDITION FAILS, XKEPNEW IS RESET
053774,000099: # * * BY KEPLER TO A POOR BUT VALID GUESS.
053775,000100: # TC * +28 *DP PREV. VALUE OF TIME IN CENTISECS. MUST BE LESS THAN ONE ORBITAL PERIOD.
053776,000101: # XPREV * +17 FOR EARTH*DP PREV. VALUE OF X IN SQRT(METERS). MUST BE LESS THAN AN X CORRESPONDING TO ONE
053777,000102: # * +16 FOR MOON * ORBITAL PERIOD, VIZ, 2PI SQRT(SEMI-MAJOR AXIS)
053778,000103:
053779,000104: # SUBROUTINES CALLED -
053780,000105: # DELTIME
053781,000106:
053782,000107: # CALLING SEQUENCE AND NORMAL EXIT MODES -
053783,000108: # KEPRTN-2 GOTO MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
053784,000109: # KEPRTN-1 KEPLER RETURNS WITH XPREV IN MPAC. PL IS AT 0.
053785,000110: # KEPRTN ... CONTINUE
053786,000111:
053787,000112: # KEPLER MUST NOT BE CALLED DIRECTLY SINCE AN INTERRUPTION OF IT WOULD DESTROY THE ERASABLES IT NEEDS TO COMPLETE
053788,000113: # THE INTERRUPTED JOB. THEREFORE THE USER MUST CALL CSMCONIC OR LEMCONIC WHICH GUARANTEES NO INTERRUPTS AND WHICH
053789,000114: # ALSO CALLS KEPPREP TO COMPUTE A GUESS OF XKEPNEW.
053790,000115:
053791,000116: # ABORT EXIT MODES -
053792,000117: # NONE
053793,000118:
053794,000119: # OUTPUT -
053795,000120: # * SCALE FACTOR *
053796,000121: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
053797,000122: # --------*--------------* -----------------------
053798,000123: # RCV * +29 FOR EARTH*DP TERMINAL POSITION VECTOR IN METERS
053799,000124: # * +27 FOR MOON *
053800,000125: # VCV * +7 FOR EARTH *DP TERMINAL VELOCITY VECTOR IN METERS/CENTISEC
053801,000126: # * +5 FOR MOON *
053802,000127: # TC * +28 *DP TRANSFER TIME IN CENTISECS TO WHICH KEPLER CONVERGED. ALWAYS LESS THAN ONE PERIOD.
053803,000128: # XPREV * +17 FOR EARTH*DP VALUE OF X IN SQRT(METERS) TO WHCIH KEPLER CONVERGED. ALWAYS LESS THAN THE X
053804,000129: # * +16 FOR MOON * CORRESPONDING TO ONE PERIOD.
Page 1265 |
053806,000131: # FOR OTHER OUTPUT WHICH MAY BE OF USE, SEE DEBRIS.
053807,000132:
053808,000133: # DEBRIS -
053809,000134: # PARAMETERS WHICH MAY BE OF USE -
053810,000135: # * SCALE FACTOR *
053811,000136: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
053812,000137: # --------*--------------* -----------------------
053813,000138: # URRECT * +1 *DP UNIT VECTOR OF INITIAL POSITION
053814,000139: # R1 * +29 FOR EARTH*DP MAGNITUDE OF INITIAL POSITION IN METERS
053815,000140: # * +27 FOR MOON *
053816,000141: # ALPHA * -22 FOR EARTH*DP INVERSE OF SEMIMAJOR AXIS IN 1/METERS
053817,000142: # * -20 FOR MOON *
053818,000143: # TMODULO * +28 *DP INTEGRAL NUMBER OF PERIODS IN CENTISECS. WHICH WAS SUBTRACTED FROM TAU. TO PRODUCE A
053819,000144: # * *TAU. OF LESS THAN ONE PERIOD.
053820,000145:
053821,000146: # PARAMETERS OF NO USE -
053822,000147: # DP PARAMETERS - EPSILONT, DELX, DELT, RCNORM, XMODULO, PLUS PUSHLIST REGISTERS 0 THROUGH 39D.
053823,000148:
Page 1266 |
053825,000150: # PROGRAM DESCRIPTION - LAMBERT SUBROUTINE DATE - 1 SEPTEMBER 1967
053826,000151: # MOD NO. - 0 LOG SECTION - CONIC SUBROUTINES
053827,000152: # MOD BY KRAUSE ASSEMBLY - COLOSSUS REVISION 88
053828,000153:
053829,000154: # FUNCTIONAL DESCRIPTION -
053830,000155: # THIS SUBROUTINE CALCULATES THE INITIAL VELOCITY REQUIRED TO TRANSFER A POINT-MASS ALONG A CONIC TRAJECTORY
053831,000156: # FROM AN INITIAL POSITION TO A TERMINAL POSITION IN A PRESCRIBED TIME INTERVAL. THE RESULTING TRAJECTORY MAY BE
053832,000157: # A SECTION OF A CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON. THE USE OF THE
053833,000158: # SUBROUTINE CAN BE EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY
053834,000159: # CODING CHANGES, ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY. AN ITERATION TECHNIQUE IS
053835,000160: # UTILIZED IN THE COMPUTATION.
053836,000161:
053837,000162: # THE RESTRICTIONS ARE -
053838,000163: # 1. RECTILINEAR TRAJECTORIES CANNOT BE COMPUTED.
053839,000164: # 2. AN ACCURACY DEGRADATION OCCURS AS THE COSINE OF THE TRUE ANOMALY DIFFERENCE APPROACHES +1.0.
053840,000165: # 3. THE ANGLE BETWEEN ANY POSITION VECTOR AND ITS VELOCITY VECTOR MUST BE GREATER THAN 1 DEGREE 47.5 MINUTES
053841,000166: # AND LESS THAN 178 DEGREES 12.5 MINUTES.
053842,000167: # 4. NEGATIVE TRANSFER TIME IS AMBIGUOUS AND WILL RESULT IN NO SOLUTION.
053843,000168: # 5. THE PARAMETERS IN THE PROBLEM MUST NOT EXCEED THEIR SCALING LIMITS SPECIFIED IN THE GSOP. IF THE
053844,000169: # LIMITS ARE EXCEEDED, THE RESULTING SOLUTION WILL BE MEANINGLESS.
053845,000170:
053846,000171: # THE NUMBER OF ITERATIONS AND, THEREFORE, THE COMPUTATIONS SPEED IS DEPENDENT ON THE ACCURACY OF THE FIRST
053847,000172: # GUESS OF THE INDEPENDENT VARIABLE, COGA. THE AGC COMPUTATION TIME IS APPROXIMATE-
053848,000173: # LY .105 SECONDS FOR INITIALIZATION, .069 SECONDS FOR FINAL COMPUTATIONS, PLUS .205 SECONDS FOR EACH ITERATION.
053849,000174:
053850,000175: # REFERENCES -
053851,000176: # R-479, MISSION PROGRAMMING DEFINITION MEMO NO. 10, LUNAR LANDING MISSION GSOP - SECTION 5.5, SGA MEMO 67-8,
053852,000177: # SGA MEMO 67-4.
053853,000178:
053854,000179: # INPUT - ERASABLE INITIALIZATION REQUIRED
053855,000180: # * SCALE FACTOR *
053856,000181: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
053857,000182: # --------*--------------* -----------------------
053858,000183: # R1VEC * +29 FOR EARTH*DP INITIAL POSITION VECTOR IN METERS
053859,000184: # * +27 FOR MOON *
053860,000185: # R2VEC * +29 FOR EARTH*DP TARGET OR TERMINAL POSITION VECTOR IN METERS
053861,000186: # * +27 FOR MOON *
053862,000187: # TDESIRED* +28 *DP DESIRED TRANSFER TIME IN CENTISECONDS
053863,000188: # X1 (38D)* NONE *INDEX REGISTER SET TO -2D OR -10D ACCORDING TO WHETHER THE EARTH OR MOON,
053864,000189: # * *RESPECTIVELY, IS THE CENTRAL BODY
053865,000190: # GEOMSGN * NONE *SP +.5 IF DESIRED TRANSFER ANGLE IS LESS THAN 180 DEGREES, -.5 IF GREATER THAN 180 DEG.
053866,000191: # GUESSW * NONE *AN INTERPRETER SWITCH TO BE SET IF NO GUESS OF COGA IS AVAILABLE, CLEAR IF A GUESS OF
Page 1267 |
053868,000193: # * *COGA IS TO BE USED BY LAMBERT
053869,000194: # COGA * +5 *DP GUESS OF COTANGNT OF FLIGHT PATH ANGLE (MEASURED FROM VERTICAL). THIS WILL BE
053870,000195: # *IGNORED IF GUESSW IS SET.
053871,000196: # NORMSW * NONE *AN INTERPRETER SWITCH TO BE SET IF UN IS TO BE AN INPUT TO THE SUBROUTINE, CLEAR IF
053872,000197: # * *LAMBERT IS TO COMPUTE ITS OWN NORMAL (UN).
053873,000198: # UN * +1 *DP UNIT NORMAL TO THE DESIRED ORBIT PLANE IN THE DIRECTION OF THE RESULTING ANGULAR
053874,000199: # * *MOMENTUM VECTOR. THIS WILL BE IGNORED IF NORMSW IS CLEAR.
053875,000200: # VTARGTAG* NONE *A S.P. TAG TO BE SET TO ZERO IF LAMBERT IS TO COMPUTE THE VELOCITY AT R2VEC AS WELL AS
053876,000201: # * *AT R1VEC.
053877,000202:
053878,000203: # SUBROUTINES CALLED -
053879,000204: # GEOM, GETX, DELTIME, ITERATOR, LAMENTER (PART OF NEWSTATE)
053880,000205:
053881,000206: # CALLING SEQUENCE AND NORMAL EXIT MODES -
053882,000207: # L CALL MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
053883,000208: # L+1 LAMBERT RETURNS WITH PL AT 0 AND WITH VVEC IN MPAC IF VTARGTAG WAS NON-ZERO OR VTARGET
053884,000209: # IN MPAC IF VTARGTAG WAS ZERO
053885,000210: # L+2 BON CONTINUE IF SOLNSW CLEAR SINCE SOLUTION IS ACCEPTABLE
053886,000211: # L+3 SOLNSW
053887,000212: # L+4 LAMABORT
053888,000213:
053889,000214: # IF A LAMBERT RESULT IS TO BE A FIRST GUESS FOR THE NEXT LAMBERT CALCULATION, COGA MUST BE PRESERVED AND
053890,000215: # GUESSW MUST BE CLEAR FOR EACH SUCCEEDING LAMBERT CALL.
053891,000216:
053892,000217: # ABORT EXIT MODES -
053893,000218: # IF SOLNSW WAS SET UPON EXITING, EITHER LAMBERT WAS ASKED TO COMPUTE A TRANSFER TOO NEAR 0 OR 360 DEG, OR T
053894,000219: # WAS TOO SMALL TO PRODUCE A REALISTIC TRANSFER BETWEEN R1VEC AND R2VEC. IN EITHER CASE THE FIX MUST BE MADE
053895,000220: # ACCORDING TO THE NEEDS OF THE PARTICULAR USER. THE ABORT EXIT MODE MAY BE CODED AS ...
053896,000221: # LAMABORT DLOAD ABS A MEASURE OF PROXIMITY TO 0 OR
053897,000222: # 1-CSTH 360 DEGREES.
053898,000223: # DSU BMN
053899,000224: # ONEBIT
053900,000225: # CHANGER2 CHANGE R2VEC DIRECTION SLIGHTLY.
053901,000226: # DLOAD DAD
053902,000227: # TDESIRED
053903,000228: # SOMETIME
053904,000229: # STCALL TDESIRED INCREASE TDESIRED
053905,000230: # LAMBERT
053906,000231:
053907,000232: # OUTPUT -
053908,000233: # * SCALE FACTOR *
053909,000234: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
Page 1268 |
053911,000236: # --------*--------------* -----------------------
053912,000237: # VVEC * +7 FOR EARTH *DP INITIAL VELOCITY VECTOR IN METERS/CENTISECOND REQUIRED TO SATISFY THE BOUNDARY VALUE
053913,000238: # * +5 FOR MOON *PROBLEM.
053914,000239: # VTARGET * +7 FOR EARTH *DP RESULTANT VELOCITY VECTOR AT R2VEC IN METERS/CENTISECOND.
053915,000240: # * +5 FOR MOON *
053916,000241: # SOLNSW * NONE *INTERPRETER SWITCH WHICH IS SET IF THE SUBROUTINE CANNOT SOLVE THE PROBLEM, CLEAR IF THE
053917,000242: # * *SOLUTION EXISTS.
053918,000243:
053919,000244: # FOR OTHER OUTPUT WHICH MAY BE OF USE, SEE DEBRIS.
053920,000245:
053921,000246: # DEBRIS -
053922,000247: # PARAMETERS WHICH MAY BE OF USE -
053923,000248: # * SCALE FACTOR *
053924,000249: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
053925,000250: # --------*--------------* -----------------------
053926,000251: # SNTH * +1 *DP SIN OF ANGLE BETWEEN R1VEC AND R2VEC
053927,000252: # CSTH * +1 *DP COSINE OF ANGLE
053928,000253: # 1-CSTH * +2 *DP 1-CSTH
053929,000254: # COGA * +5 *DP COTAN OF INITIAL REQUIRED FLIGHT PATH ANGLE MEASURED FROM VERTICAL
053930,000255: # P * +4 *DP RATIO OF SEMILATUS RECTUM TO INITIAL RADIUS
053931,000256: # R1A * +6 *DP RATIO OF INITIAL RADIUS TO SEMIMAJOR AXIS
053932,000257: # R1 (32D)* +29 FOR EARTH*DP INITIAL RADIUS IN METERS
053933,000258: # * +27 FOR MOON *
053934,000259: # UR1 * +1 *DP UNIT VECTOR OF R1VEC
053935,000260: # U2 * +1 *DP UNIT VECTOR OF R2VEC
053936,000261:
053937,000262: # PARAMETERS OF NO USE
053938,000263: # DP PARAMETERS - EPSILONL, CSTH-RHO, TPREV, TERRLAMB, R2, RTNLAMB (SP), PLUS PUSHLIST REGISTER 0 THROUGH 41D
053939,000264: # ADDITIONAL INTERPRETIVE SWITCHES USED - INFINFLG, 360SW, SLOPESW, ORDERSW
053940,000265:
Page 1269 |
053942,000267: # PROGRAM DESCRIPTION - TIME-THETA SUBROUTINE DATE - 1 SEPTEMBER 1967
053943,000268: # MOD NO. - 0 LOG SECTION - CONIC SUBROUTINES
053944,000269: # MOD BY KRAUSE ASSEMBLY - COLOSSUS REVISION 88
053945,000270:
053946,000271: # FUNCTIONAL DESCRIPTION -
053947,000272: # THIS SUBROUTINE, GIVEN AN INITIAL STATE VECTOR AND A DESIRED TRUE-ANOMALY-DIFFERENCE THROUGH WHICH THE
053948,000273: # STATE IS TO BE UPDATED ALONG A CONIC TRAJECTORY, CALCULATES THE CORRESPONDING TIME-OF-FLIGHT AND, IN ADDITION,
053949,000274: # PROVIDES THE OPTION OF COMPUTING THE NEW UPDATED STATE VECTOR. THE RESULTING TRAJECTORY MAY BE A SECTION OF A
053950,000275: # CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON. THE USE OF THE SUBROUTINE CAN BE
053951,000276: # EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY CODING CHANGES,
053952,000277: # ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY.
053953,000278:
053954,000279: # THE RESTRICTIONS ARE -
053955,000280: # 1. THE ANGLE BETWEEN ANY POSITION VECTOR AND ITS VELOCITY VECTOR MUST BE GREATER THAN 1 DEGREE 47.5 MINUTES
053956,000281: # AND LESS THAN 178 DEGREES 12.5 MINUTES.
053957,000282: # 2. THE PARAMETERS IN THE PROBLEM MUST NOT EXCEED THEIR SCALING LIMITS SPECIFIED IN THE GSOP. IF THE LIMITS
053958,000283: # ARE EXCEEDED, THE RESULTING SOLUTION WILL BE MEANINGLESS.
053959,000284:
053960,000285: # THE AGC COMPUTATION TIME IS APPROXIMATELY .292 SECONDS.
053961,000286:
053962,000287: # REFERENCES -
053963,000288: # R-479, MISSION PROGRAMMING DEFINITION MEMO NO. 10, LUNAR LANDING MISSION GSOP-SECTION 5.5, SGA MEMO 67-8.
053964,000289:
053965,000290: # INPUT - ERASABLE INITIALIZATION REQUIRED
053966,000291: # * SCALE FACTOR *
053967,000292: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
053968,000293: # --------*--------------* -----------------------
053969,000294: # RVEC * +29 FOR EARTH*DP INITIAL POSITION VECTOR IN METERS
053970,000295: # * +27 FOR MOON *
053971,000296: # VVEC * +7 FOR EARTH *DP INITIAL VELOCITY VECTOR IN METERS/CENTISECOND
053972,000297: # * +5 FOR MOON *
053973,000298: # SNTH * +1 *DP SINE OF TRUE-ANOMALY-DIFFERENCE THROUGH WHICH THE STATE IS TO BE UPDATED
053974,000299: # CSTH * +1 *DP COSINE OF THE ANGLE
053975,000300: # RVSW * NONE *AN INTERPRETIVE SWITCH TO BE SET IF ONLY TIME IS TO BE AN OUTPUT, CLEAR IF THE NEW STATE
053976,000301: # * *IS TO BE COMPUTED ALSO.
053977,000302: # X1 (38D)* NONE *INDEX REGISTER TO BE SET TO -2D OR -10D ACCORDING TO WHETHER THE EARTH OR MOON,
053978,000303: # * *RESPECTIVELY, IS THE CENTRAL BODY.
053979,000304:
053980,000305: # SUBROUTINES CALLED -
Page 1270 |
053982,000307: # PARAM, GEOM, GETX, DELTIME, NEWSTATE
053983,000308:
053984,000309: # CALLING SEQUENCE AND NORMAL EXIT MODES -
053985,000310: # IF ONLY TIME IS DESIRED AS OUTPUT -
053986,000311: # L SET CALL MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
053987,000312: # L+1 RVSW
053988,000313: # L+2 TIMETHET RETURN WITH PL AT 0 AND T IN MPAC
053989,000314: # L+3 ... CONTINUE
053990,000315:
053991,000316: # IF THE UPDATE STATE VECTOR IS DESIRED AS WELL -
053992,000317: # L CLEAR CALL MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
053993,000318: # L+1 RVSW
053994,000319: # L+2 TIMETHET RETURNS WITH PL AT 6. THE INITIAL POSITION VECTOR IS IN 0D OF THE PUSHLIST AND
053995,000320: # THE INITIAL VELOCITY VECTOR IN MPAC.
053996,000321: # L+3 STOVL NEWVVEC
053997,000322: # L+4 STADR
053998,000323: # L+5 STORE NEWRVEC NEWVVEC AND NEWRVEC ARE SYMBOLIC REPRESENTATIONS OF THE USERS LOCATIONS.
053999,000324: # L+6 ... CONTINUE
054000,000325:
054001,000326: # ABORT EXIT MODES -
054002,000327: # IF COGAFLAG AND/OR INFINFLG IS SET AT THE EXIT TO TIME-THETA, TIME-THETA WILL TRANSFER TO POODOO WITH
054003,000328: # AN ALARM CODE (ORIGINALLY 00607), AND NOT RETURN TO THE CALLING PROGRAM. (PCR 692 AND 721).
054004,000329:
054005,000330: # OUTPUT -
054006,000331: # * SCALE FACTOR *
054007,000332: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054008,000333: # --------*--------------* -----------------------
054009,000334: # T(30D) * +28 *DP TRANSFER TIME IN CENTISECONDS
054010,000335: # INFINFLG* NONE *AN INTERPRETIVE SWITCH WHICH IS SET IF THE TRANSFER ANGLE REQUIRES CLOSURE THROUGH
054011,000336: # * *INFINITY (NO SOLUTION), CLEAR IF A PHYSICAL SOLUTION IS POSSIBLE.
054012,000337: # COGAFLAG* NONE *AN INTERPRETIVE SWITCH WHICH IS SET IF RESTRICTION 1 HAS BEEN VIOLATED (NO SOLUTION),
054013,000338: # * *CLEAR IF NOT.
054014,000339:
054015,000340: # IN ADDITION, IF RVSW IS CLEAR, THE FOLLOWING ARE OUTPUT -
054016,000341: # MPAC - * +7 FOR EARTH *DP TERMINAL VELOCITY VECTOR IN METERS/CENTISEC.
054017,000342: # MPAC +5* +5 FOR MOON *
054018,000343: # 0D - 5D * +29 FOR EARTH*DP TERMINAL POSITION VECTOR IN METERS (PL AT 6D)
054019,000344: # * +27 FOR MOON *
054020,000345:
054021,000346: # FOR OTHER OUTPUT WHICH MAY BE OF USE, SEE DEBRIS.
Page 1271 |
054023,000348:
054024,000349: # DEBRIS -
054025,000350: # PARAMETERS WHICH MAY BE OF USE -
054026,000351: # * SCALE FACTOR *
054027,000352: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054028,000353: # --------*--------------* -----------------------
054029,000354: # R1 (32D)* +29 FOR EARTH*DP MAGNITUDE OF INITIAL POSITION VECTOR, RVEC, IN METERS
054030,000355: # * +27 FOR MOON *
054031,000356: # R1A * +6 *DP RATIO OF R1 TO SEMIMAJOR AXIS (NEG. FOR HYPERBOLIC TRAJECTORIES)
054032,000357: # P * +4 *DP RATIO OF SEMILATUS RECTUM TO R1
054033,000358: # COGA * +5 *DP COTAN OF ANGLE BETWEEN RVEC AND VVEC
054034,000359: # UR1 * +1 *DP UNIT VECTOR OF RVEC
054035,000360: # U2 * +1 *DP UNIT VECTOR OF VVEC
054036,000361: # UN * +1 *DP UNIT VECTOR OF UR1*U2
054037,000362:
054038,000363: # PARAMETERS OF NO USE -
054039,000364: # SP PARAMETERS - RTNTT, GEOMSGN, RTNPRM, MAGVEC2=R2 (DP), PLUS PUSHLIST LOCATIONS 0-11D, 14D-21D, 24D-39D, 41D
054040,000365: # ADDITIONAL INTERPRETIVE SWITCHES USED - NORMSW, 360SW
054041,000366:
Page 1272 |
054043,000368: # PROGRAM DESCRIPTION - TIME-RADIUS SUBROUTINE DATE - 11 OCTOBER 1967
054044,000369: # MOD NO. -1 LOG SECTION - CONIC SUBROUTINES
054045,000370: # MOD BY KRAUSE ASSEMBLY - COLOSSUS REVISION 88
054046,000371:
054047,000372: # FUNCTIONAL DESCRIPTION -
054048,000373: # THIS SUBROUTINE, GIVEN AN INITIAL STATE VECTOR AND A DESIRED RADIUS TO WHICH THE
054049,000374: # STATE IS TO BE UPDATED ALONG A CONIC TRAJECTORY, CALCULATES THE CORRESPONDING TIME-OF-FLIGHT AND, IN ADDITION,
054050,000375: # PROVIDES THE OPTION OF COMPUTING THE NEW UPDATED STATE VECTOR. THE RESULTING TRAJECTORY MAY BE A SECTION OF A
054051,000376: # CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON. THE USE OF THE SUBROUTINE CAN BE
054052,000377: # EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY CODING CHANGES,
054053,000378: # ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY.
054054,000379:
054055,000380: # IF THE DESIRED RADIUS IS BEYOND THE RADIUS OF APOCENTER OF THE CONIC OR BELOW THE RADIUS OF PERICENTER,
054056,000381: # APSESW WILL BE SET AND THE SUBROUTINE WILL RETURN THE APOCENTER OR PERICENTER SOLUTION, RESPECTIVELY.
054057,000382:
054058,000383: # THE RESTRICTIONS ARE -
054059,000384: # 1. THE ANGLE BETWEEN ANY POSITION VECTOR AND ITS VELOCITY VECTOR MUST BE GREATER THAN 1 DEGREE 47.5 MINUTES
054060,000385: # AND LESS THAN 178 DEGREES 12.5 MINUTES.
054061,000386: # 2. THE PARAMETERS IN THE PROBLEM MUST NOT EXCEED THEIR SCALING LIMITS SPECIFIED IN THE GSOP. IF THE LIMITS
054062,000387: # ARE EXCEEDED, THE RESULTING SOLUTION WILL BE MEANINGLESS.
054063,000388: # 3. AN ACCURACY DEGRADATION OCCURS AS THE SENSITIVITIES OF TIME AND UPDATED STATE VECTOR TO CHANGES IN
054064,000389: # RDESIRED INCREASE. THIS WILL OCCUR NEAR EITHER APSIS OF THE CONIC AND WHEN THE CONIC IS NEARLY CIRCULAR. IN
054065,000390: # PARTICULAR, IF THE CONIC IS AN EXACT CIRCLE, THE PROBLEM IS UNDEFINED AND THE SUBROUTINE WILL ABORT.
054066,000391:
054067,000392: # THE AGC COMPUTATION TIME IS APPROXIMATELY .363 SECONDS
054068,000393:
054069,000394: # REFERENCES -
054070,000395: # R-479, MISSION PROGRAMMING DEFINITION MEMO NO. 10, LUNAR LANDING MISSION GSOP-SECTION 5.5, SGA MEMO 67-8.
054071,000396:
054072,000397: # INPUT - ERASABLE INITIALIZATION REQUIRED
054073,000398: # * SCALE FACTOR *
054074,000399: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054075,000400: # --------*--------------* -----------------------
054076,000401: # RVEC * +29 FOR EARTH*DP INITIAL POSITION VECTOR IN METERS
054077,000402: # * +27 FOR MOON *
054078,000403: # VVEC * +7 FOR EARTH *DP INITIAL VELOCITY VECTOR IN METERS/CENTISECOND
054079,000404: # * +5 FOR MOON *
054080,000405: # RDESIRED* +29 FOR EARTH*DP TERMINAL RADIAL DISTANCE ON CONIC TRAJECTORY FOR WHICH TRANSFER TIME IS TO BE
054081,000406: # * +27 FOR MOON *COMPUTED.
054082,000407: # SGNRDOT * NONE *SP TAG SET TO +.5 OR -.5 ACCORDING TO WHETHER THE RADIAL VELOCITY AT RDESIRED IS TO BE
054083,000408: # * *POSITIVE OR NEGATIVE, RESPECTIVELY. THIS TAG REDUCES THE DOUBLE-VALUED PROBLEM TO A
Page 1273 |
054085,000410: # * *SINGLE-VALUED PROBLEM.
054086,000411: # X1 (38D)* NONE *INDEX REGISTER TO BE SET TO -2D OR -10D ACCORDING TO WHETHER THE EARTH OR MOON,
054087,000412: # * *RESPECTIVELY, IS THE CENTRAL BODY.
054088,000413: # RVSW * NONE *AN INTERPRETIVE SWITCH TO BE SET IF ONLY TIME IS TO BE AN OUTPUT, CLEAR IF THE NEW STATE
054089,000414: # * *IS TO BE COMPUTED ALSO.
054090,000415:
054091,000416: # SUBROUTINES CALLED -
054092,000417: # PARAM, GEOM, GETX, DELTIME, NEWSTATE
054093,000418:
054094,000419: # CALLING SEQUENCE AND NORMAL EXIT MODES -
054095,000420: # IF ONLY TIME IS DESIRED AS OUTPUT -
054096,000421: # L SET CALL MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
054097,000422: # L+1 RVSW
054098,000423: # L+2 TIMERAD RETURN WITH PL AT 0 AND T IN MPAC
054099,000424: # L+3 ... CONTINUE
054100,000425:
054101,000426: # IF THE UPDATE STATE VECTOR IS DESIRED AS WELL -
054102,000427: # L CLEAR CALL MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
054103,000428: # L+1 RVSW
054104,000429: # L+2 TIMERAD RETURNS WITH PL AT 6. THE INITIAL POSITION VECTOR IS IN 0D OF THE PUSHLIST AND
054105,000430: # THE INITIAL VELOCITY VECTOR IN MPAC.
054106,000431: # L+3 STOVL NEWVVEC
054107,000432: # L+4 STADR
054108,000433: # L+5 STORE NEWRVEC NEWVVEC AND NEWRVEC ARE SYMBOLIC REPRESENTATIONS OF THE USERS LOCATIONS.
054109,000434: # L+6 ... CONTINUE
054110,000435:
054111,000436: # ABORT EXIT MODES -
054112,000437: # IF SOLNSW AND/OR COGAFLAG AND/OR INFINFLG IS SET AT THE EXIT TO TIME-RADIUS, TIME-RADIUS WILL TRANSFER
054113,000438: # TO POODOO WITH AN ALARM CODE (ORIGINALLY 00607), AND NOT RETURN TO THE CALLING PROGRAM. (PCR 692 & 721)
054114,000439:
054115,000440: # OUTPUT -
054116,000441: # * SCALE FACTOR *
054117,000442: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054118,000443: # --------*--------------* -----------------------
054119,000444: # T (30D) * +28 *DP TRANSFER TIME IN CENTISECONDS
054120,000445: # INFINFLG* NONE *AN INTERPRETIVE SWITCH WHICH IS SET IF RDESIRED AND SGNRDOT REQUIRE CLOSURE THROUGH
054121,000446: # * *INFINITY (NO SOLUTION), CLEAR IF A PHYSICAL SOLUTION IS POSSIBLE.
054122,000447: # COGAFLAG* NONE *AN INTERPRETIVE SWITCH WHICH IS SET IF RESTRICTION 1 HAS BEEN VIOLATED (NO SOLUTION),
054123,000448: # * *CLEAR IF NOT.
054124,000449: # APSESW * NONE *AN INTERPRETIVE SWITCH WHICH IS SET IF RDESIRED WAS GREATER THAN RADIUS OF APOCENTER OR
Page 1274 |
054126,000451: # * *LESS THAN RADIUS OF PERICENTER. THE APOCENTER OR PERICENTER SOLUTION, RESPECTIVELY,
054127,000452: # * *WILL THEN BE RETURNED. THE SWITCH IS CLEAR IF RDESIRED WAS BETWEEN PERICENTER AND
054128,000453: # * *APOCENTER.
054129,000454: # SOLNSW * NONE *AN INTERPRETIVE SWITCH WHICH IS SET IF THE CONIC IS SO CLOSE TO A CIRCLE THAT THE TERMIN
054130,000455: # *POINT IS AMBIGUOUS, VIOLATING RESTRICTION 3. IF ECCENTRICITY IS GREATER THAN 2-TO-THE-
054131,000456: # *MINUS-18, THE SWITCH IS CLEAR.
054132,000457:
054133,000458: # IN ADDITION, IF RVSW IS CLEAR, THE FOLLOWING ARE OUTPUT -
054134,000459: # MPAC - * +7 FOR EARTH *DP TERMINAL VELOCITY VECTOR IN METERS/CENTISEC.
054135,000460: # MPAC +5* +5 FOR MOON *
054136,000461: # 0D - 5D * +29 FOR EARTH*DP TERMINAL POSITION VECTOR IN METERS (PL AT 6D)
054137,000462: # * +27 FOR MOON *
054138,000463:
054139,000464: # FOR OTHER OUTPUT WHICH MAY BE OF USE, SEE DEBRIS.
054140,000465:
054141,000466: # DEBRIS -
054142,000467: # PARAMETERS WHICH MAY BE OF USE -
054143,000468: # * SCALE FACTOR *
054144,000469: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054145,000470: # --------*--------------* -----------------------
054146,000471: # R1 (32D)* +29 FOR EARTH*DP MAGNITUDE OF INITIAL POSITION VECTOR, RVEC, IN METERS
054147,000472: # * +27 FOR MOON *
054148,000473: # R1A * +6 *DP RATIO OF R1 TO SEMIMAJOR AXIS (NEG. FOR HYPERBOLIC TRAJECTORIES)
054149,000474: # P * +4 *DP RATIO OF SEMILATUS RECTUM TO R1
054150,000475: # COGA * +5 *DP COTAN OF ANGLE BETWEEN RVEC AND VVEC
054151,000476: # UR1 * +1 *DP UNIT VECTOR OF RVEC
054152,000477: # U2 * +1 *DP UNIT VECTOR OF VVEC
054153,000478: # UN * +1 *DP UNIT VECTOR OF UR1*U2
054154,000479: # CSTH * +1 *DP COSINE OF TRUE ANOMALY DIFFERENCE BETWEEN RVEC AND RDESIRED.
054155,000480: # SNTH * +1 *DP SINE OF TRUE ANOMALY DIFFERENCE.
054156,000481:
054157,000482: # PARAMETERS OF NO USE -
054158,000483: # SP PARAMETERS - RTNTT, GEOMSGN, RTNPRM, MAGVEC2=R2 (DP), PLUS PUSHLIST LOCATIONS 0-11D, 14D-21D, 24D-39D, 41D
054159,000484: # ADDITIONAL INTERPRETIVE SWITCHES USED - NORMSW, 360SW
054160,000485:
054161,000486:
Page 1275 |
054163,000488: # PROGRAM DESCRIPTION - APSIDES SUBROUTINE DATE - 1 SEPTEMBER 1967
054164,000489: # MOD NO. - 0 LOG SECTION - CONIC SUBROUTINES
054165,000490: # MOD BY KRAUSE ASSEMBLY - COLOSSUS REVISION 88
054166,000491:
054167,000492: # FUNCTIONAL DESCRIPTION -
054168,000493: # THIS SUBROUTINE, GIVEN AN INITIAL STATE VECTOR CALCULATES THE RADIUS OF PERICENTER AND OF APOCENTER AND THE
054169,000494: # ECCENTRICITY OF THE RESULTING CONIC TRAJECTORY, WHICH MAY BE A STRAIGHT LINE,
054170,000495: # CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON. THE USE OF THE SUBROUTINE CAN BE
054171,000496: # EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY CODING CHANGES,
054172,000497: # ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY.
054173,000498:
054174,000499: # THE RESTRICTIONS ARE -
054175,000500: # 1. IF APOCENTER IS BEYOND THE SCALING OF POSITION, THE SCALE FACTOR LIMIT (536,870,910 METERS WITH RESPECT
054176,000501: # TO THE EARTH OR 134,217,727.5 METERS WITH RESPECT TO THE MOON) WILL BE RETURNED.
054177,000502: # 2. THE PARAMETERS IN THE PROBLEM MUST NOT EXCEED THEIR SCALING LIMITS SPECIFIED IN THE GSOP. IF THE LIMITS
054178,000503: # ARE EXCEEDED, THE RESULTING SOLUTION WILL BE MEANINGLESS.
054179,000504:
054180,000505: # THE AGC COMPUTATION TIME IS APPROXIMATELY .103 SECONDS.
054181,000506:
054182,000507: # REFERENCES -
054183,000508: # MISSION PROGRAMMING DEFINITION MEMO NO. 10, LUNAR LANDING MISSION GSOP-SECTION 5.5
054184,000509:
054185,000510: # INPUT - ERASABLE INITIALIZATION REQUIRED
054186,000511: # * SCALE FACTOR *
054187,000512: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054188,000513: # --------*--------------* -----------------------
054189,000514: # RVEC * +29 FOR EARTH*DP INITIAL POSITION VECTOR IN METERS
054190,000515: # * +27 FOR MOON *
054191,000516: # VVEC * +7 FOR EARTH *DP INITIAL VELOCITY VECTOR IN METERS/CENTISECOND
054192,000517: # * +5 FOR MOON *
054193,000518: # X1 (38D)* NONE *INDEX REGISTER TO BE SET TO -2D OR -10D ACCORDING TO WHETHER THE EARTH OR MOON,
054194,000519: # * *RESPECTIVELY, IS THE CENTRAL BODY.
054195,000520:
054196,000521: # SUBROUTINES CALLED -
054197,000522: # PARAM, GEOM
054198,000523:
054199,000524: # CALLING SEQUENCE AND NORMAL EXIT MODES -
Page 1276 |
054201,000526: # IF ONLY TIME IS DESIRED AS OUTPUT -
054202,000527: # L CALL MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
054203,000528: # L+1 APSIDES RETURNS WITH PL AT 0, RADIUS OF APOCENTER IN MPAC AND RADIUS OF PERICENTER IN 0D
054204,000529: # L+2 STODL APOAPSE
054205,000530: # L+3 0D
054206,000531: # L+4 STORE PERIAPSE APOAPSE AND PERIAPSE ARE SYMBOLIC REPRESENTATIONS OF THE USERS LOCATIONS
054207,000532: # L+5 ... CONTINUE
054208,000533:
054209,000534: # OUTPUT -
054210,000535: # * SCALE FACTOR *
054211,000536: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054212,000537: # --------*--------------* -----------------------
054213,000538: # MPAC * +29 FOR EARTH*DP RADIUS OF APOCENTER IN METERS
054214,000539: # * +27 FOR MOON *
054215,000540: # 0D-1D * +29 FOR EARTH*DP RADIUS OF PERICENTER IN METERS
054216,000541: # * +27 FOR MOON *
054217,000542: # ECC * +3 *DP ECCENTRICITY OF CONIC TRAJECTORY.
054218,000543:
054219,000544: # FOR OTHER OUTPUT WHICH MAY BE OF USE, SEE DEBRIS.
054220,000545:
054221,000546: # DEBRIS -
054222,000547: # PARAMETERS WHICH MAY BE OF USE -
054223,000548: # * SCALE FACTOR *
054224,000549: # VARIABLE*IN POWERS OF 2* DESCRIPTION AND REMARKS
054225,000550: # --------*--------------* -----------------------
054226,000551: # R1 (32D)* +29 FOR EARTH*DP MAGNITUDE OF INITIAL POSITION VECTOR, RVEC, IN METERS
054227,000552: # * +27 FOR MOON *
054228,000553: # R1A * +6 *DP RATIO OF R1 TO SEMIMAJOR AXIS (NEG. FOR HYPERBOLIC TRAJECTORIES)
054229,000554: # P * +4 *DP RATIO OF SEMILATUS RECTUM TO R1
054230,000555: # COGA * +5 *DP COTAN OF ANGLE BETWEEN RVEC AND VVEC
054231,000556: # UR1 * +1 *DP UNIT VECTOR OF RVEC
054232,000557: # U2 * +1 *DP UNIT VECTOR OF VVEC
054233,000558: # UN * +1 *DP UNIT VECTOR OF UR1*U2
054234,000559: # MAGVEC2 * +7 FOR EARTH *DP MAGNITUDE OF VVEC
054235,000560: # * +5 FOR MOON *
054236,000561:
054237,000562: # PARAMETERS OF NO USE -
054238,000563: # SP PARAMETERS - RTNAPSE, GEOMSGN, RTNPRM, PLUS PUSHLIST LOCATIONS 0-5, 10D-11D, 14D-21D, 31D-38D.
054239,000564: # ADDITIONAL INTERPRETIVE SWITCHES USED - NORMSW
054240,000565:
054241,000566: 12,2000 SETLOC CONICS
Page 1277 |
054243,000568: 12,2000 BANK
054244,000569:
054245,000570: 12,2042 COUNT 12/CONIC
054246,000571:
054247,000572: 12,2042 E5,1723 EBANK= UR1
054248,000573: 12,2042 40001 KEPLERN SETPD BOV
054249,000574: 12,2043 00001 0
054250,000575: 12,2044 24045 +1
054251,000576: 12,2045 77773 VLOAD*
054252,000577: 12,2046 11740 MUTABLE,1
054253,000578: 12,2047 24017 STOVL 14D
054254,000579: 12,2050 01503 RRECT
054255,000580: 12,2051 66256 UNIT SSP
054256,000581: 12,2052 00027 ITERCTR
054257,000582: 12,2053 00024 20D
054258,000583: 12,2054 16647 STODL URRECT
054259,000584: 12,2055 00045 36D
054260,000585: 12,2056 24041 STOVL R1
054261,000586: 12,2057 01503 RRECT
054262,000587: 12,2060 76441 DOT SL1R
054263,000588: 12,2061 01511 VRECT
054264,000589: 12,2062 76405 DMP SL1R
054265,000590: 12,2063 00023 1/ROOTMU # 1/ROOTMU (-17 OR -14)
054266,000591: 12,2064 24043 STOVL KEPC1 # C1=R.V/ROOTMU (+17 OR +16)
054267,000592:
054268,000593: 12,2065 01511 VRECT
054269,000594: 12,2066 57236 VSQ DMPR
054270,000595: 12,2067 00017 1/MU # 1/MU (-34 OR -28)
054271,000596: 12,2070 52405 DMP SL3
054272,000597: 12,2071 00041 R1
054273,000598: 12,2072 61425 DSU ROUND
054274,000599: 12,2073 11610 D1/64
054275,000600: 12,2074 00045 STORE KEPC2 # C2=RV.V/MU -1 (+6)
054276,000601:
054277,000602: 12,2075 74421 BDSU SR1R
054278,000603: 12,2076 11610 D1/64
054279,000604: 12,2077 77671 DDV
054280,000605: 12,2100 00041 R1
054281,000606: 12,2101 00011 STORE ALPHA # ALPHA=(1-C2)/R1 (-22 OR -20)
054282,000607:
054283,000608: 12,2102 71244 BPL DLOAD # MAXIMUM X DEPENDS ON TYPE OF CONIC
054284,000609: 12,2103 24112 1REV
054285,000610: 12,2104 11626 -50SC # -50SC (+12)
054286,000611: 12,2105 40071 DDV BOV
054287,000612: 12,2106 00011 ALPHA
054288,000613: 12,2107 24116 STOREMAX
054289,000614: 12,2110 52166 SQRT GOTO
054290,000615: 12,2111 24116 STOREMAX
Page 1278 |
054292,000617: 12,2112 55366 1REV SQRT BDDV
054293,000618: 12,2113 11630 2PISC # 2PISC (+6)
054294,000619: 12,2114 77600 BOV
054295,000620: 12,2115 24116 STOREMAX
054296,000621: 12,2116 00013 STOREMAX STORE XMAX
054297,000622: 12,2117 65205 DMP PDDL
054298,000623: 12,2120 00023 1/ROOTMU
054299,000624: 12,2121 00011 ALPHA
054300,000625: 12,2122 65301 NORM PDDL
054301,000626: 12,2123 00047 X1
054302,000627: 12,2124 56257 SL* DDV
054303,000628: 12,2125 20173 0 -6,1
054304,000629: 12,2126 50000 BOV BMN
054305,000630: 12,2127 24143 MODDONE
054306,000631: 12,2130 24143 MODDONE # MPAC=PERIOD
054307,000632: 12,2131 51525 PERIODCH PDDL ABS # 0D=PERIOD
054308,000633: 12,2132 02312 TAU.
054309,000634: 12,2133 50025 DSU BMN
054310,000635: 12,2134 00001 0D
054311,000636: 12,2135 24143 MODDONE
054312,000637: 12,2136 77765 SIGN
054313,000638: 12,2137 02312 TAU.
054314,000639: 12,2140 16312 STODL TAU.
054315,000640: 12,2141 77650 GOTO
054316,000641: 12,2142 24131 PERIODCH
054317,000642: 12,2143 71201 MODDONE SETPD DLOAD
054318,000643: 12,2144 00001 0
054319,000644: 12,2145 02306 XKEPNEW
054320,000645: 12,2146 00025 STORE X
054321,000646: 12,2147 53165 SIGN BZE
054322,000647: 12,2150 02312 TAU.
054323,000648: 12,2151 24320 BADX
054324,000649: 12,2152 51440 BMN ABS
054325,000650: 12,2153 24320 BADX
054326,000651: 12,2154 51025 DSU BPL
054327,000652: 12,2155 00013 XMAX
054328,000653: 12,2156 24320 BADX
054329,000654: 12,2157 51145 STORBNDS DLOAD BPL
054330,000655: 12,2160 02312 TAU.
054331,000656: 12,2161 24170 STOREMIN
054332,000657: 12,2162 57545 DLOAD DCOMP
054333,000658: 12,2163 00013 XMAX
054334,000659: 12,2164 14015 STODL XMIN
054335,000660: 12,2165 11566 KEPZERO
054336,000661: 12,2166 34013 STCALL XMAX
054337,000662: 12,2167 24173 DXCOMP
054338,000663: 12,2170 77745 STOREMIN DLOAD
054339,000664: 12,2171 11566 KEPZERO
054340,000665: 12,2172 00015 STORE XMIN
054341,000666: 12,2173 57345 DXCOMP DLOAD DMPR
Page 1279 |
054343,000668: 12,2174 02312 TAU.
054344,000669: 12,2175 11621 BEE22
054345,000670: 12,2176 77646 ABS
054346,000671: 12,2177 15350 STODL EPSILONT
054347,000672: 12,2200 01553 XPREV
054348,000673: 12,2201 77621 XDIFF BDSU
054349,000674: 12,2202 00025 X
054350,000675: 12,2203 02643 STORE DELX
054351,000676:
054352,000677: 12,2204 63545 KEPLOOP DLOAD DSQ
054353,000678: 12,2205 00025 X # X=XKEP
054354,000679: 12,2206 41501 NORM PUSH # 0D=XSQ (+34 OR +32 -N1) PL AT 2
054355,000680: 12,2207 00047 X1
054356,000681: 12,2210 53605 DMP SRR*
054357,000682: 12,2211 00011 ALPHA
054358,000683: 12,2212 21573 0 -6,1
054359,000684: 12,2213 34031 STCALL XI # XI=ALPHA XSQ (+6)
054360,000685: 12,2214 24433 DELTIME
054361,000686: 12,2215 44200 BOV BDSU
054362,000687: 12,2216 24326 TIMEOVFL # UNLIKELY
054363,000688: 12,2217 02312 TAU.
054364,000689: 12,2220 02645 STORE DELT # DELT=DELINDEP
054365,000690: 12,2221 44246 ABS BDSU
054366,000691: 12,2222 01350 EPSILONT
054367,000692: 12,2223 71244 BPL DLOAD
054368,000693: 12,2224 24346 KEPCONVG
054369,000694: 12,2225 00037 T
054370,000695: 12,2226 60225 DSU NORM
054371,000696: 12,2227 01551 TC
054372,000697: 12,2230 00047 X1
054373,000698: 12,2231 60325 PDDL NORM
054374,000699: 12,2232 02643 DELX
054375,000700: 12,2233 00050 X2
054376,000701: 12,2234 41260 XSU,1 DMP
054377,000702: 12,2235 00047 X2
054378,000703: 12,2236 02645 DELT
054379,000704: 12,2237 56257 SLR* DDV
054380,000705: 12,2240 21202 1,1
054381,000706: 12,2241 41542 SR1 PUSH # 0D=TRIAL DELX PL AT 2
054382,000707: 12,2242 71244 BPL DLOAD
054383,000708: 12,2243 24264 POSDELX
054384,000709: 12,2244 00025 X
054385,000710: 12,2245 00013 STORE XMAX # MOVE MAX BOUND IN
054386,000711: 12,2246 45221 BDSU DSU # PL AT 0
054387,000712: 12,2247 00015 XMIN
054388,000713: 12,2250 51000 BOV BPL
054389,000714: 12,2251 24256 NDXCHNGE
054390,000715: 12,2252 24256 NDXCHNGE
054391,000716: 12,2253 52145 DLOAD GOTO
Page 1280 |
054393,000718: 12,2254 00001 0D
054394,000719: 12,2255 24276 NEWDELX
054395,000720:
054396,000721: 12,2256 45345 NDXCHNGE DLOAD DSU
054397,000722: 12,2257 00015 XMIN
054398,000723: 12,2260 00025 X
054399,000724: 12,2261 52075 DMPR GOTO # TO FORCE MPAC +2 TO ZERO
054400,000725: 12,2262 11624 DP9/10
054401,000726: 12,2263 24276 NEWDELX
054402,000727:
054403,000728: 12,2264 77745 POSDELX DLOAD
054404,000729: 12,2265 00025 X
054405,000730: 12,2266 00015 STORE XMIN # MOVE MIN BOUND IN
054406,000731: 12,2267 45221 BDSU DSU # PL AT 0
054407,000732: 12,2270 00013 XMAX
054408,000733: 12,2271 50000 BOV BMN
054409,000734: 12,2272 24312 PDXCHNGE
054410,000735: 12,2273 24312 PDXCHNGE
054411,000736: 12,2274 77745 DLOAD
054412,000737: 12,2275 00001 0D
054413,000738: 12,2276 02643 NEWDELX STORE DELX
054414,000739: 12,2277 43254 BZE DAD
054415,000740: 12,2300 24346 KEPCONVG
054416,000741: 12,2301 00025 X
054417,000742: 12,2302 14025 STODL X
054418,000743: 12,2303 00037 T
054419,000744: 12,2304 01551 STORE TC
054420,000745: 12,2305 46034 BRNCHCTR RTB BHIZ
054421,000746: 12,2306 24656 CHECKCTR
054422,000747: 12,2307 24346 KEPCONVG
054423,000748: 12,2310 77650 GOTO
054424,000749: 12,2311 24204 KEPLOOP # ITERATE
054425,000750:
054426,000751: 12,2312 45345 PDXCHNGE DLOAD DSU
054427,000752: 12,2313 00013 XMAX
054428,000753: 12,2314 00025 X
054429,000754: 12,2315 52075 DMPR GOTO # TO FORCE MPAC +2 TO ZERO
054430,000755: 12,2316 11624 DP9/10
054431,000756: 12,2317 24276 NEWDELX
054432,000757:
054433,000758: 12,2320 70545 BADX DLOAD SR1
054434,000759: 12,2321 00013 XMAX
054435,000760: 12,2322 77765 SIGN
054436,000761: 12,2323 02312 TAU.
054437,000762: 12,2324 34025 STCALL X
054438,000763: 12,2325 24157 STORBNDS
Page 1281 |
054440,000765: 12,2326 50145 TIMEOVFL DLOAD BMN # X WAS TOO BIG
054441,000766: 12,2327 00025 X
054442,000767: 12,2330 24344 NEGTOVFL
054443,000768: 12,2331 00013 STORE XMAX
054444,000769: 12,2332 70545 CMNTOVFL DLOAD SR1
054445,000770: 12,2333 02643 DELX
054446,000771: 12,2334 02643 STORE DELX
054447,000772: 12,2335 44254 BZE BDSU
054448,000773: 12,2336 02270 KEPRTN
054449,000774: 12,2337 00025 X
054450,000775: 12,2340 14025 STODL X
054451,000776: 12,2341 01551 TC
054452,000777: 12,2342 34037 STCALL T
054453,000778: 12,2343 24305 BRNCHCTR
054454,000779: 12,2344 34015 NEGTOVFL STCALL XMIN
054455,000780: 12,2345 24332 CMNTOVFL
054456,000781: 12,2346 44545 KEPCONVG DLOAD SR4R
054457,000782: 12,2347 00041 R1
054458,000783: 12,2350 74225 DSU VXSC
054459,000784: 12,2351 00035 XSQC(XI)
054460,000785: 12,2352 02647 URRECT
054461,000786: 12,2353 65372 VSL1 PDDL # 0D=(R1-XSQC(XI))URRECT (+33 OR +31)
054462,000787: 12,2354 00025 X
054463,000788: 12,2355 60316 DSQ NORM
054464,000789: 12,2356 00047 X1
054465,000790: 12,2357 57275 DMPR DMPR
054466,000791: 12,2360 00023 1/ROOTMU
054467,000792: 12,2361 00025 X
054468,000793: 12,2362 53605 DMP SRR*
054469,000794: 12,2363 00033 S(XI)
054470,000795: 12,2364 21572 0 -7,1
054471,000796: 12,2365 77621 BDSU
054472,000797: 12,2366 00037 T
054473,000798: 12,2367 74352 SL1 VXSC
054474,000799: 12,2370 01511 VRECT
054475,000800: 12,2371 53372 VSL1 VAD # PL AT 0
054476,000801: 12,2372 77712 VSL4
054477,000802: 12,2373 01535 STORE RCV # RCV (+29 OR +27)
054478,000803:
054479,000804: 12,2374 60246 ABVAL NORM
054480,000805: 12,2375 00050 X2
054481,000806: 12,2376 16655 STODL RCNORM
054482,000807: 12,2377 00031 XI
054483,000808: 12,2400 45275 DMPR DSU
054484,000809: 12,2401 00033 S(XI)
054485,000810: 12,2402 11606 D1/128
054486,000811: 12,2403 76405 DMP SL1R
054487,000812: 12,2404 00021 ROOTMU
054488,000813: 12,2405 53605 DMP SLR*
Page 1282 |
054490,000815: 12,2406 00025 X
054491,000816: 12,2407 56601 0 -3,2
054492,000817: 12,2410 74271 DDV VXSC
054493,000818: 12,2411 02655 RCNORM
054494,000819: 12,2412 02647 URRECT
054495,000820: 12,2413 65372 VSL1 PDDL # 0D=URRECT(XI S(XI)-1)X ROOTMU/RCV (+15
054496,000821: 12,2414 00035 XSQC(XI) # OR +13) PL AT 6
054497,000822: 12,2415 56257 SLR* DDV
054498,000823: 12,2416 56602 0 -4,2
054499,000824: 12,2417 02655 RCNORM
054500,000825: 12,2420 74221 BDSU VXSC
054501,000826: 12,2421 11622 D1/256
054502,000827: 12,2422 01511 VRECT
054503,000828: 12,2423 42455 VAD VSL8
054504,000829: 12,2424 77626 STADR # PL AT 0
054505,000830: 12,2425 62234 STODL VCV # VCV (+7 OR +5)
054506,000831: 12,2426 00037 T
054507,000832: 12,2427 15551 STODL TC
054508,000833: 12,2430 00025 X
054509,000834: 12,2431 35553 STCALL XPREV
054510,000835: 12,2432 02270 KEPRTN
054511,000836:
Page 1283 |
054513,000838: 12,2433 77776 DELTIME EXIT # MPAC=XI (+6), 0D=XSQ (+34 OR +32 -N1)
054514,000839: 12,2434 07171 TC POLY
054515,000840: 12,2435 00010 DEC 8 B-14
054516,000841: 12,2436 02525 12526 2DEC .083333334
054517,000842:
054518,000843: 12,2440 67356 75666 2DEC -.266666684
054519,000844:
054520,000845: 12,2442 15001 23771 2DEC .406349155
054521,000846:
054522,000847: 12,2444 64342 43674 2DEC -.361198675
054523,000848:
054524,000849: 12,2446 06563 04645 2DEC .210153242
054525,000850:
054526,000851: 12,2450 75173 52672 2DEC -.086221951
054527,000852:
054528,000853: 12,2452 00656 14331 2DEC .026268812
054529,000854:
054530,000855: 12,2454 77633 40512 2DEC -.006163316
054531,000856:
054532,000857: 12,2456 00023 11210 2DEC .001177342
054533,000858:
054534,000859: 12,2460 77774 67506 2DEC -.000199055
054535,000860:
054536,000861: 12,2462 06006 TC INTPRET
054537,000862: 12,2463 14033 STODL S(XI)
054538,000863: 12,2464 00031 XI
054539,000864: 12,2465 77776 EXIT
054540,000865: 12,2466 07171 TC POLY
054541,000866: 12,2467 00010 DEC 8 B-14
054542,000867: 12,2470 01000 00000 2DEC .031250001
054543,000868:
054544,000869: 12,2472 72525 52506 2DEC -.166666719
054545,000870:
054546,000871: 12,2474 13301 15337 2DEC .355555413
054547,000872:
054548,000873: 12,2476 62776 54733 2DEC -.406347410
054549,000874:
054550,000875: 12,2500 11176 13267 2DEC .288962094
054551,000876:
054552,000877: 12,2502 73410 51674 2DEC -.140117894
054553,000878:
054554,000879: 12,2504 01446 33641 2DEC .049247387
054555,000880:
054556,000881: 12,2506 77451 65233 2DEC -.013081923
054557,000882:
054558,000883: 12,2510 00055 37266 2DEC .002806389
054559,000884:
054560,000885: 12,2512 77767 52336 2DEC -.000529414
054561,000886:
054562,000887: 12,2514 06006 TC INTPRET
Page 1284 |
054564,000889: 12,2515 53605 DMP SRR* # PL AT 0
054565,000890: 12,2516 00001 0D
054566,000891: 12,2517 21574 0 -5,1
054567,000892: 12,2520 00035 STORE XSQC(XI) # XSQC(XI) (+33 OR +31)
054568,000893: 12,2521 72405 DMP SL1
054569,000894: 12,2522 00043 KEPC1
054570,000895: 12,2523 65234 RTB PDDL # XCH WITH PL. 0D=C1 XSQ C(XI) (+49 OR +46
054571,000896: 12,2524 45565 TPMODE # PL AT 0,3
054572,000897: 12,2525 53605 DMP SRR*
054573,000898: 12,2526 00033 S(XI)
054574,000899: 12,2527 21574 0 -5,1
054575,000900: 12,2530 72405 DMP SL1
054576,000901: 12,2531 00045 KEPC2
054577,000902: 12,2532 65234 RTB PDDL # 3D=C2 XSQ S(XI) (+35 OR +33) PL AT 6
054578,000903: 12,2533 45565 TPMODE
054579,000904: 12,2534 00041 R1
054580,000905: 12,2535 76261 SR TAD # PL AT 3
054581,000906: 12,2536 20607 6
054582,000907: 12,2537 41301 NORM DMP # TO PRESERVE SIGNIF.
054583,000908: 12,2540 00047 X1
054584,000909: 12,2541 00025 X
054585,000910: 12,2542 76257 SR* TAD # X(C2 XSQ S(XI) +R1) (+49 OR +46) PL AT 0
054586,000911: 12,2543 20576 0 -3,1
054587,000912: 12,2544 57232 SL4R DMPR
054588,000913: 12,2545 00023 1/ROOTMU
054589,000914: 12,2546 00037 STORE T
054590,000915: 12,2547 77616 RVQ
054591,000916:
Page 1285 |
054593,000918: 12,2550 71214 ITERATOR BONCLR DLOAD
054594,000919: 12,2551 00614 SLOPESW
054595,000920: 12,2552 24620 FIRSTIME
054596,000921: 12,2553 00037 DEP
054597,000922: 12,2554 60225 DSU NORM
054598,000923: 12,2555 02764 DEPREV
054599,000924: 12,2556 00047 X1
054600,000925: 12,2557 60325 PDDL NORM
054601,000926: 12,2560 00015 DELINDEP
054602,000927: 12,2561 00050 X2
054603,000928: 12,2562 41260 XSU,1 DMP
054604,000929: 12,2563 00047 X2
054605,000930: 12,2564 02762 DELDEP
054606,000931: 12,2565 56257 SLR* DDV # PL UP 2
054607,000932: 12,2566 21202 1,1
054608,000933: 12,2567 43142 SR1 BOFF
054609,000934: 12,2570 04351 ORDERSW
054610,000935: 12,2571 24574 SGNCHECK
054611,000936: 12,2572 75246 ABS SIGN # IN CASE 2ND DERIV. CHANGED SIGN, MUST
054612,000937: 12,2573 02762 DELDEP # DISREGARD IT TO FIND MIN.
054613,000938:
054614,000939: 12,2574 51006 SGNCHECK PUSH BPL # TRIAL DELINDEP PL DOWN 2
054615,000940: 12,2575 24632 POSDEL
054616,000941: 12,2576 43145 DLOAD BON
054617,000942: 12,2577 03775 INDEP
054618,000943: 12,2600 04311 ORDERSW
054619,000944: 12,2601 24603 MINCHECK
054620,000945: 12,2602 00017 STORE MAX # IF NOT 2ND ORDER, CAN MOVE MAX BOUND IN.
054621,000946:
054622,000947: 12,2603 45221 MINCHECK BDSU DSU
054623,000948: 12,2604 00011 MIN
054624,000949: 12,2605 51000 BOV BPL
054625,000950: 12,2606 24612 MODNGDEL
054626,000951: 12,2607 24612 MODNGDEL
054627,000952: 12,2610 77650 GOTO
054628,000953: 12,2611 24644 DELOK
054629,000954:
054630,000955: 12,2612 45345 MODNGDEL DLOAD DSU # TRIAL DELINDEP WOULD EXCEED MIN BOUND
054631,000956: 12,2613 00011 MIN
054632,000957: 12,2614 03775 INDEP
054633,000958: 12,2615 52005 DMP GOTO
054634,000959: 12,2616 11624 DP9/10
054635,000960: 12,2617 24646 NEWDEL
054636,000961:
054637,000962: 12,2620 41345 FIRSTIME DLOAD DMP
054638,000963: 12,2621 00011 MIN
054639,000964: 12,2622 00051 TWEEKIT # DLOAD TWEEKIT(40D) SENSITIVE TO CHANGE.
054640,000965: 12,2623 41325 PDDL DMP # S2(41D) SHOULDNT CONTAIN HI ORDER ONES
Page 1286 |
054642,000967: 12,2624 00017 MAX
054643,000968: 12,2625 00051 TWEEKIT
054644,000969: 12,2626 77625 DSU
054645,000970: 12,2627 52165 SIGN GOTO
054646,000971: 12,2630 02762 DELDEP
054647,000972: 12,2631 24574 SGNCHECK
054648,000973:
054649,000974: 12,2632 43145 POSDEL DLOAD BON
054650,000975: 12,2633 03775 INDEP
054651,000976: 12,2634 04311 ORDERSW
054652,000977: 12,2635 24637 MAXCHECK
054653,000978: 12,2636 00011 STORE MIN # IF NOT 2ND ORDER, CAN MOVE MIN BOUND IN.
054654,000979:
054655,000980: 12,2637 45221 MAXCHECK BDSU DSU
054656,000981: 12,2640 00017 MAX
054657,000982: 12,2641 50000 BOV BMN
054658,000983: 12,2642 24650 MODPSDEL
054659,000984: 12,2643 24650 MODPSDEL
054660,000985: 12,2644 77745 DELOK DLOAD
054661,000986: 12,2645 00001 0D
054662,000987: 12,2646 00015 NEWDEL STORE DELINDEP
054663,000988: 12,2647 77616 RVQ
054664,000989:
054665,000990: 12,2650 45345 MODPSDEL DLOAD DSU
054666,000991: 12,2651 00017 MAX
054667,000992: 12,2652 03775 INDEP
054668,000993: 12,2653 52005 DMP GOTO
054669,000994: 12,2654 11624 DP9/10
054670,000995: 12,2655 24646 NEWDEL
054671,000996:
054672,000997: 12,2656 45017 CHECKCTR CS ONE
054673,000998: 12,2657 50120 INDEX FIXLOC
054674,000999: 12,2660 60026 AD ITERCTR
054675,001000: 12,2661 50120 INDEX FIXLOC
054676,001001: 12,2662 54026 TS ITERCTR
054677,001002: 12,2663 54154 TS MPAC
054678,001003: 12,2664 06030 TC DANZIG
054679,001004:
Page 1287 |
054681,001006: 12,2665 44545 NEWSTATE DLOAD SR4R
054682,001007: 12,2666 00041 R1
054683,001008: 12,2667 74225 DSU VXSC
054684,001009: 12,2670 00035 XSQC(XI)
054685,001010: 12,2671 02724 UR1
054686,001011: 12,2672 65372 VSL1 PDDL # 0D=(R1-XSQC(XI))UR1 (+33 OR 31) PL AT 6
054687,001012: 12,2673 00025 X
054688,001013: 12,2674 60316 DSQ NORM
054689,001014: 12,2675 00047 X1
054690,001015: 12,2676 57275 DMPR DMPR
054691,001016: 12,2677 00023 1/ROOTMU
054692,001017: 12,2700 00025 X
054693,001018: 12,2701 53605 DMP SRR*
054694,001019: 12,2702 00033 S(XI)
054695,001020: 12,2703 21572 0 -7,1
054696,001021: 12,2704 77621 BDSU
054697,001022: 12,2705 00037 T
054698,001023: 12,2706 74352 SL1 VXSC
054699,001024: 12,2707 02746 VVEC
054700,001025: 12,2710 53372 VSL1 VAD # PL AT 0
054701,001026: 12,2711 41512 VSL4 PUSH
054702,001027: 12,2712 77646 ABVAL
054703,001028: 12,2713 77701 LAMENTER NORM
054704,001029: 12,2714 00047 X1
054705,001030: 12,2715 16722 STODL R2
054706,001031: 12,2716 00031 XI
054707,001032: 12,2717 45205 DMP DSU
054708,001033: 12,2720 00033 S(XI)
054709,001034: 12,2721 11606 D1/128
054710,001035: 12,2722 76405 DMP SL1R
054711,001036: 12,2723 00021 ROOTMU
054712,001037: 12,2724 53605 DMP SLR*
054713,001038: 12,2725 00025 X
054714,001039: 12,2726 21176 0 -3,1
054715,001040: 12,2727 74271 DDV VXSC
054716,001041: 12,2730 02722 R2
054717,001042: 12,2731 02724 UR1
054718,001043: 12,2732 65372 VSL1 PDDL # 6D=V2VEC PART (+15 OR 13) PL AT 12
054719,001044: 12,2733 00035 XSQC(XI)
054720,001045: 12,2734 56257 SLR* DDV
054721,001046: 12,2735 21175 0 -4,1
054722,001047: 12,2736 02722 R2
054723,001048: 12,2737 77621 BDSU
054724,001049: 12,2740 11622 D1/256
054725,001050: 12,2741 53361 VXSC VAD
054726,001051: 12,2742 02746 VVEC # PL AT 6
054727,001052: 12,2743 43412 VSL8 RVQ
054728,001053:
Page 1288 |
054730,001055: 04,2000 SETLOC CONICS1
054731,001056: 04,2000 BANK
054732,001057:
054733,001058: 04,3602 COUNT 04/CONIC
054734,001059: # DO NOT DISTURB THE ORDER OF THESE CDS, OVERLAYS HAVE BEEN MADE.
054735,001060: 04,3602 00000 BEE17 DEC 0 B-14 # KEEP WITH D1/8 2DEC 1.0B-17 (0000004000)
054736,001061: 04,3603 04000 00000 D1/8 2DEC 1.0 B-3
054737,001062:
054738,001063: 04,3605 00200 00000 D1/128 2DEC 1.0 B-7
054739,001064:
054740,001065: 04,3607 00400 00000 D1/64 2DEC 1.0 B-6
054741,001066:
054742,001067: 04,3611 10000 00000 D1/4 2DEC 1.0 B-2
054743,001068:
054744,001069: 04,3613 02000 00000 D1/16 2DEC 1.0 B-4
054745,001070:
054746,001071: 04,3615 01000 00000 D1/32 2DEC 1.0 B-5
054747,001072:
054748,001073: 04,3617 00020 00000 D1/1024 2DEC 1.0 B-10
054749,001074:
054750,001075: 04,3621 00100 00000 D1/256 2DEC 1.0 B-8
054751,001076:
054752,001077: 04,3623 34631 23146 DP9/10 2DEC .9
054753,001078:
054754,001079: 04,3625 04,3565 KEPZERO EQUALS LO6ZEROS
054755,001080: 04,3625 77467 77777 -50SC 2DEC -50.0 B-12
054756,001081:
054757,001082: 04,3627 03110 17665 2PISC 2DEC 6.28318530 B-6
054758,001083:
054759,001084: 04,3631 04,3614 BEE19 EQUALS D1/32 -1 # 2DEC 1.0 B-19 (00000 01000)
054760,001085: 04,3631 04,3620 BEE22 EQUALS D1/256 -1 # 2DEC 1.0 B-22 (00000 00100)
054761,001086: 04,3631 00000 00001 ONEBIT 2DEC 1.0 B-28
054762,001087:
054763,001088: 04,3633 37767 37737 COGUPLIM 2DEC .999511597
054764,001089:
054765,001090: 04,3635 40010 40040 COGLOLIM 2DEC -.999511597
054766,001091:
Page 1289 |
054768,001093: 12,2000 SETLOC CONICS
054769,001094: 12,2000 BANK
054770,001095:
054771,001096: 12,2744 COUNT 12/CONIC
054772,001097:
054773,001098: 12,2744 40220 TIMETHET STQ SETPD # PL AT 0
054774,001099: 12,2745 02712 RTNTT
054775,001100: 12,2746 00001 0
054776,001101: 12,2747 77600 BOV
054777,001102: 12,2750 24751 +1
054778,001103: 12,2751 63375 VLOAD PDVL # SETUP FOR PARAM CALL PL AT 6
054779,001104: 12,2752 02657 RVEC
054780,001105: 12,2753 02746 VVEC
054781,001106: 12,2754 77624 CALL
054782,001107: 12,2755 11637 PARAM
054783,001108: 12,2756 45000 BOV CALL
054784,001109: 12,2757 24776 COGAOVFL # PL AT 0
054785,001110: 12,2760 25001 GETX
054786,001111: 12,2761 43145 COMMNOUT DLOAD BON
054787,001112: 12,2762 00031 XI
054788,001113: 12,2763 04310 INFINFLG
054789,001114: 12,2764 25751 ABTCONIC
054790,001115: 12,2765 45014 CLEAR CALL
054791,001116: 12,2766 04273 COGAFLAG
054792,001117: 12,2767 24433 DELTIME
054793,001118: 12,2770 45014 BON CALL
054794,001119: 12,2771 03706 RVSW
054795,001120: 12,2772 02712 RTNTT
054796,001121: 12,2773 24665 NEWSTATE
054797,001122: 12,2774 77650 GOTO
054798,001123: 12,2775 02712 RTNTT
054799,001124:
054800,001125: 12,2776 77614 COGAOVFL SETGO
054801,001126: 12,2777 04033 COGAFLAG
054802,001127: 12,3000 25751 ABTCONIC
054803,001128: 04,3637 BANK 4
054804,001129: 04,2000 SETLOC CONICS1
054805,001130: 04,2000 BANK
054806,001131: 04,3637 COUNT* $$/CONIC
054807,001132: 04,3637 43020 PARAM STQ CLEAR # MPAC=V1VEC, 0D=R1VEC PL AT 6
054808,001133: 04,3640 02755 RTNPRM
054809,001134: 04,3641 03665 NORMSW
054810,001135: 04,3642 77614 CLEAR
054811,001136: 04,3643 04273 COGAFLAG
054812,001137: 04,3644 45131 SSP CALL
054813,001138: 04,3645 02675 GEOMSGN
054814,001139: 04,3646 27777 37777 # GAMMA ALWAYS LESS THAN 180DEG
054815,001140: 04,3647 11702 GEOM # MPAC=SNGA (+1), 0D=CSGA (+1) PL AT 2
054816,001141: 04,3650 14045 STODL 36D # 36D=SIN GAMMA (+1) PL AT 0
Page 1290 |
054818,001143: 04,3651 56261 SR DDV
054819,001144: 04,3652 20606 5
054820,001145:
054821,001146: 04,3653 00045 36D
054822,001147: 04,3654 33775 STOVL* COGA
054823,001148: 04,3655 11740 MUTABLE,1
054824,001149: 04,3656 14017 STODL 1/MU
054825,001150: 04,3657 02722 MAGVEC2
054826,001151: 04,3660 60316 DSQ NORM
054827,001152: 04,3661 00047 X1
054828,001153: 04,3662 41275 DMPR DMP
054829,001154: 04,3663 00017 1/MU
054830,001155: 04,3664 00041 R1
054831,001156: 04,3665 77657 SRR*
054832,001157: 04,3666 21576 0 -3,1
054833,001158: 04,3667 44206 PUSH BDSU # 0D=R1 V1SQ/MU (+6) PL AT 2
054834,001159: 04,3670 11616 D1/32
054835,001160: 04,3671 16744 STODL R1A # R1A (+6) PL AT 0
054836,001161:
054837,001162: 04,3672 60205 DMP NORM
054838,001163: 04,3673 00045 36D
054839,001164: 04,3674 00047 X1
054840,001165: 04,3675 53605 DMP SR*
054841,001166: 04,3676 00045 36D
054842,001167: 04,3677 20575 0 -4,1
054843,001168: 04,3700 36742 STCALL P # P (+4)
054844,001169: 04,3701 02755 RTNPRM
054845,001170:
Page 1291 |
054847,001172: 04,3702 77656 GEOM UNIT # MPAC=V2VEC, 0D=R1VEC PL AT 6
054848,001173: 04,3703 16714 STODL U2 # U2 (+1)
054849,001174: 04,3704 00045 36D
054850,001175: 04,3705 26722 STOVL MAGVEC2 # PL AT 0
054851,001176: 04,3706 77656 UNIT
054852,001177: 04,3707 02724 STORE UR1 # UR1 (+1)
054853,001178: 04,3710 72441 DOT SL1
054854,001179: 04,3711 02714 U2
054855,001180: 04,3712 77725 PDDL # OD=CSTH (+1) PL AT 2
054856,001181: 04,3713 00045 36D
054857,001182: 04,3714 24041 STOVL R1 # R1 (+29 OR +27)
054858,001183: 04,3715 02724 UR1
054859,001184: 04,3716 76435 VXV VSL1
054860,001185: 04,3717 02714 U2
054861,001186: 04,3720 75214 BON SIGN
054862,001187: 04,3721 03705 NORMSW
054863,001188: 04,3722 11734 HAVENORM
054864,001189: 04,3723 02675 GEOMSGN
054865,001190: 04,3724 40056 UNIT BOV
054866,001191: 04,3725 11732 COLINEAR
054867,001192: 04,3726 16676 UNITNORM STODL UN # UN (+1)
054868,001193: 04,3727 00045 36D
054869,001194: 04,3730 43565 SIGN RVQ # MPAC=SNTH (+1), 34D=SNTH.SNTH (+2)
054870,001195: 04,3731 02675 GEOMSGN
054871,001196:
054872,001197: 04,3732 52162 COLINEAR VSR1 GOTO
054873,001198: 04,3733 11726 UNITNORM
054874,001199:
054875,001200: 04,3734 75246 HAVENORM ABVAL SIGN
054876,001201: 04,3735 02675 GEOMSGN
054877,001202: 04,3736 77616 RVQ # MPAC=SNTH (+1), 34D=SNTH.SNTH (+2)
054878,001203:
Page 1292 |
054880,001205: 12,3001 BANK 12
054881,001206: 12,2000 SETLOC CONICS
054882,001207: 12,2000 BANK
054883,001208:
054884,001209: 12,3001 COUNT 12/CONIC
054885,001210:
054886,001211: 12,3001 66374 GETX AXT,2 SSP # ASSUMES P (+4) IN MPAC
054887,001212: 12,3002 00003 3
054888,001213: 12,3003 00052 S2
054889,001214: 12,3004 00001 1
054890,001215: 12,3005 77614 CLEAR
054891,001216: 12,3006 04276 360SW
054892,001217: 12,3007 65366 SQRT PDDL # 0D=SQRT(P) PL AT 2
054893,001218: 12,3010 02734 CSTH
054894,001219: 12,3011 44342 SR1 BDSU
054895,001220: 12,3012 11612 D1/4
054896,001221: 12,3013 54325 PDDL SRR # PL AT 4D
054897,001222: 12,3014 02732 SNTH
054898,001223: 12,3015 21607 6
054899,001224: 12,3016 77671 DDV # PL AT 2
054900,001225: 12,3017 77600 BOV
054901,001226: 12,3020 25134 360CHECK
054902,001227: 12,3021 41225 DSU DMP
054903,001228: 12,3022 03775 COGA # PL AT 0
054904,001229: 12,3023 40132 SL2R BOV
054905,001230: 12,3024 25134 360CHECK
054906,001231: 12,3025 63406 WLOOP PUSH DSQ # 0D=W (+5) PL AT 2
054907,001232: 12,3026 65351 TLOAD PDDL # 2D=WSQ (+10) PL AT 5
054908,001233: 12,3027 00155 MPAC
054909,001234: 12,3030 02744 R1A
054910,001235: 12,3031 76202 SR4 TAD # PL AT 2
054911,001236: 12,3032 75440 BMN SQRT
054912,001237: 12,3033 25217 INFINITY
054913,001238: 12,3034 43306 ROUND DAD # PL AT 0D
054914,001239: 12,3035 61000 BOV TIX,2
054915,001240: 12,3036 25132 RESETX2
054916,001241: 12,3037 25025 WLOOP
054917,001242:
054918,001243: 12,3040 40065 BDDV BOV
054919,001244: 12,3041 11606 D1/128
054920,001245: 12,3042 25217 INFINITY
054921,001246: 12,3043 41440 POLYCOEF BMN PUSH # 0D=1/W (+2) OR 16/W (+6) PL AT 2
054922,001247: 12,3044 25217 INFINITY
054923,001248: 12,3045 77716 DSQ
054924,001249: 12,3046 41301 NORM DMP
054925,001250: 12,3047 00047 X1
054926,001251: 12,3050 02744 R1A
054927,001252: 12,3051 77457 SRR* EXIT
054928,001253: 12,3052 21567 0 -10D,1
Page 1293 |
054930,001255: 12,3053 07171 TC POLY
054931,001256: 12,3054 00005 DEC 5 B-14
054932,001257: 12,3055 20000 00000 2DEC .5
054933,001258:
054934,001259: 12,3057 72525 52471 2DEC -.166666770
054935,001260:
054936,001261: 12,3061 03146 15003 2DEC .100000392
054937,001262:
054938,001263: 12,3063 75556 45210 2DEC -.071401086
054939,001264:
054940,001265: 12,3065 01615 13553 2DEC .055503292
054941,001266:
054942,001267: 12,3067 76371 63777 2DEC -.047264098
054943,001268:
054944,001269: 12,3071 01232 27367 2DEC .040694204
054945,001270:
054946,001271: 12,3073 06006 TC INTPRET
054947,001272: 12,3074 76405 DMP SL1R # PL AT 0D
054948,001273: 12,3075 43006 PUSH BON
054949,001274: 12,3076 04316 360SW
054950,001275: 12,3077 25204 TRUE360X
054951,001276: 12,3100 60316 XCOMMON DSQ NORM
054952,001277: 12,3101 00047 X1
054953,001278: 12,3102 53605 DMP SRR*
054954,001279: 12,3103 02744 R1A
054955,001280: 12,3104 21565 0 -12D,1
054956,001281: 12,3105 14031 STODL XI # XI (+6)
054957,001282:
054958,001283: 12,3106 00041 R1
054959,001284: 12,3107 75542 SR1 SQRT
054960,001285: 12,3110 41306 ROUND DMP
054961,001286: 12,3111 77632 SL4R # PL AT 0
054962,001287: 12,3112 00025 STORE X # X (+17 OR +16)
054963,001288:
054964,001289: 12,3113 60316 DSQ NORM
054965,001290: 12,3114 00047 X1
054966,001291: 12,3115 41325 PDDL DMP # 0D=XSQ (+34 OR +32 -N1) PL AT 2
054967,001292: 12,3116 02742 P
054968,001293: 12,3117 00041 R1
054969,001294: 12,3120 75452 SL3 SQRT
054970,001295: 12,3121 56405 DMP SL3R
054971,001296: 12,3122 03775 COGA
054972,001297: 12,3123 14043 STODL KEPC1
054973,001298: 12,3124 02744 R1A
054974,001299: 12,3125 43021 BDSU CLEAR
054975,001300: 12,3126 11610 D1/64
054976,001301: 12,3127 04270 INFINFLG
054977,001302: 12,3130 00045 STORE KEPC2
Page 1294 |
054979,001304: 12,3131 77616 RVQ
054980,001305:
054981,001306: 12,3132 77774 RESETX2 AXT,2
054982,001307: 12,3133 00003 3
054983,001308:
054984,001309: 12,3134 51001 360CHECK SETPD BPL
054985,001310: 12,3135 00001 0D
054986,001311: 12,3136 25141 INVRSEQN
054987,001312: 12,3137 77614 SET
054988,001313: 12,3140 04076 360SW
054989,001314:
054990,001315: 12,3141 75545 INVRSEQN DLOAD SQRT
054991,001316: 12,3142 02742 P
054992,001317: 12,3143 41325 PDDL DMP # 0D=SQRT(P) (+2) PL AT 2
054993,001318: 12,3144 02732 SNTH
054994,001319: 12,3145 03775 COGA
054995,001320: 12,3146 65352 SL1 PDDL # 2D=SNTH COGA (+5) PL AT 4
054996,001321: 12,3147 02734 CSTH
054997,001322: 12,3150 43202 SR4 DAD
054998,001323: 12,3151 11616 D1/32
054999,001324: 12,3152 41225 DSU DMP # PL AT 2,0
055000,001325: 12,3153 55301 NORM BDDV
055001,001326: 12,3154 00047 X1
055002,001327: 12,3155 02732 SNTH
055003,001328: 12,3156 51457 SLR* ABS # NOTE: NEAR 360 CASE TREATED DIFFERENTLY
055004,001329: 12,3157 21174 0 -5,1
055005,001330: 12,3160 63406 PUSH DSQ # 0D=1/W (-1) PL AT 2
055006,001331: 12,3161 14043 STODL 34D
055007,001332: 12,3162 11614 D1/16
055008,001333: 12,3163 63406 1/WLOOP PUSH DSQ # 2D=G (+4) PL AT 4
055009,001334: 12,3164 65234 RTB PDDL # PL AT 7
055010,001335: 12,3165 45565 TPMODE
055011,001336: 12,3166 02744 R1A
055012,001337: 12,3167 40405 DMP SR4
055013,001338: 12,3170 00043 34D
055014,001339: 12,3171 77771 TAD
055015,001340: 12,3172 75440 BMN SQRT # PL AT 4
055016,001341: 12,3173 25217 INFINITY
055017,001342: 12,3174 77615 DAD # PL AT 2
055018,001343: 12,3175 60304 TIX,2 NORM
055019,001344: 12,3176 25163 1/WLOOP
055020,001345: 12,3177 00047 X1
055021,001346: 12,3200 77665 BDDV
055022,001347: 12,3201 52057 SLR* GOTO # PL AT 0
055023,001348: 12,3202 21172 0 -7,1
055024,001349: 12,3203 25043 POLYCOEF
055025,001350:
Page 1295 |
055027,001352: 12,3204 50145 TRUE360X DLOAD BMN
055028,001353: 12,3205 02744 R1A
055029,001354: 12,3206 25217 INFINITY
055030,001355: 12,3207 60366 SQRT NORM
055031,001356: 12,3210 00047 X1
055032,001357: 12,3211 53665 BDDV SL*
055033,001358: 12,3212 11630 2PISC
055034,001359: 12,3213 20176 0 -3,1
055035,001360: 12,3214 41425 DSU PUSH # 0D=2PI/SQRT(R1A) -X PL AT 0,2
055036,001361: 12,3215 77650 GOTO
055037,001362: 12,3216 25100 XCOMMON
055038,001363: 12,3217 40001 INFINITY SETPD BOV # NO SOLUTION EXISTS SINCE CLOSURE THROUGH
055039,001364: 12,3220 00001 0 # INFINITY IS REQUIRED
055040,001365: 12,3221 25222 OVFLCLR
055041,001366: 12,3222 43414 OVFLCLR SET RVQ
055042,001367: 12,3223 04070 INFINFLG
055043,001368:
Page 1296 |
055045,001370: 12,3224 40220 LAMBERT STQ SETPD
055046,001371: 12,3225 02712 RTNLAMB
055047,001372: 12,3226 00001 0D
055048,001373: 12,3227 77600 BOV
055049,001374: 12,3230 25231 +1
055050,001375: 12,3231 76731 SSP VLOAD*
055051,001376: 12,3232 00027 ITERCTR
055052,001377: 12,3233 00024 20D
055053,001378: 12,3234 11740 MUTABLE,1
055054,001379: 12,3235 14017 STODL 1/MU
055055,001380: 12,3236 02673 TDESIRED
055056,001381: 12,3237 77675 DMPR
055057,001382: 12,3240 11615 BEE19
055058,001383: 12,3241 03777 STORE EPSILONL
055059,001384: 12,3242 77214 SET VLOAD
055060,001385: 12,3243 00474 SLOPESW
055061,001386: 12,3244 02657 R1VEC
055062,001387: 12,3245 45115 PDVL CALL # 0D=R1VEC (+29 OR +27) PL AT 6
055063,001388: 12,3246 02665 R2VEC # MPAC=R2VEC (+29 OR +27)
055064,001389: 12,3247 11702 GEOM
055065,001390: 12,3250 16732 STODL SNTH # 0D=CSTH (+1) PL AT 2
055066,001391: 12,3251 02722 MAGVEC2
055067,001392: 12,3252 65301 NORM PDDL # PL AT 4
055068,001393: 12,3253 00047 X1
055069,001394: 12,3254 00041 R1
055070,001395: 12,3255 56342 SR1 DDV # PL AT 2
055071,001396: 12,3256 65257 SL* PDDL # DXCH WITH 0D, 0D=R1/R2 (+7) PL AT 0,2
055072,001397: 12,3257 20173 0 -6,1
055073,001398: 12,3260 77626 STADR
055074,001399: 12,3261 75043 STORE CSTH # CSTH (+1)
055075,001400: 12,3262 44342 SR1 BDSU
055076,001401: 12,3263 11612 D1/4
055077,001402: 12,3264 02736 STORE 1-CSTH # 1-CSTH (+2)
055078,001403:
055079,001404: 12,3265 53106 ROUND BZE
055080,001405: 12,3266 25473 360LAMB
055081,001406: 12,3267 65301 NORM PDDL # PL AT 4
055082,001407: 12,3270 00047 X1
055083,001408: 12,3271 00001 0D
055084,001409: 12,3272 56342 SR1 DDV # PL AT 2
055085,001410: 12,3273 75457 SL* SQRT
055086,001411: 12,3274 20176 0 -3,1
055087,001412: 12,3275 54325 PDDL SR # 2D=SQRT(2R1/R2(1-CSTH)) (+5) PL AT 4
055088,001413: 12,3276 02732 SNTH
055089,001414: 12,3277 20607 6
055090,001415: 12,3300 43271 DDV DAD # PL AT 2
055091,001416: 12,3301 02736 1-CSTH
055092,001417: 12,3302 77626 STADR
055093,001418: 12,3303 77760 STORE COGAMAX
055094,001419: 12,3304 50000 BOV BMN # IF OVFL, COGAMAX=COGUPLIM
Page 1297 |
055096,001421: 12,3305 25312 UPLIM # IF NEG, USE EVEN IF LT COGLOLIM, SINCE
055097,001422: 12,3306 25315 MAXCOGA # THIS WOULD BE RESET IN LAMBLOOP
055098,001423: 12,3307 50025 DSU BMN # IF COGAMAX GT COGUPLIM, COGAMAX=COGUPLIM
055099,001424: 12,3310 11634 COGUPLIM
055100,001425: 12,3311 25315 MAXCOGA # OTHERWISE OK, SO GO TO MAXCOGA
055101,001426: 12,3312 77745 UPLIM DLOAD
055102,001427: 12,3313 11634 COGUPLIM # COGUPLIM=.999511597 = MAX VALUE OF COGA
055103,001428: 12,3314 00017 STORE COGAMAX # NOT CAUSING OVFL IN R1A CALCULATION
055104,001429: 12,3315 77745 MAXCOGA DLOAD
055105,001430: 12,3316 02734 CSTH
055106,001431: 12,3317 45261 SR DSU # PL AT 0
055107,001432: 12,3320 20607 6
055108,001433: 12,3321 77626 STADR
055109,001434: 12,3322 61037 STODL CSTH-RHO
055110,001435: 12,3323 02675 GEOMSGN
055111,001436: 12,3324 71240 BMN DLOAD
055112,001437: 12,3325 25512 LOLIM
055113,001438: 12,3326 02740 CSTH-RHO
055114,001439: 12,3327 56352 SL1 DDV
055115,001440: 12,3330 02732 SNTH
055116,001441: 12,3331 77600 BOV
055117,001442: 12,3332 25512 LOLIM
055118,001443: 12,3333 00011 MINCOGA STORE COGAMIN # COGAMIN (+5)
055119,001444: 12,3334 66214 BON SSP
055120,001445: 12,3335 00715 GUESSW
055121,001446: 12,3336 25477 NOGUESS
055122,001447: 12,3337 00051 TWEEKIT
055123,001448: 12,3340 00001 00001
055124,001449: 12,3341 77745 DLOAD
055125,001450: 12,3342 03775 COGA
055126,001451:
055127,001452: 12,3343 77605 LAMBLOOP DMP
055128,001453: 12,3344 02732 SNTH
055129,001454: 12,3345 45342 SR1 DSU
055130,001455: 12,3346 02740 CSTH-RHO
055131,001456: 12,3347 65301 NORM PDDL # 0D=SNTH COGA-(CSTH-RHO) (+7+C(X1)) PL=2
055132,001457: 12,3350 00047 X1
055133,001458: 12,3351 02736 1-CSTH
055134,001459: 12,3352 56257 SL* DDV # 1-CSTH (+2) PL AT 0
055135,001460: 12,3353 20170 0 -9D,1
055136,001461: 12,3354 53040 BMN BZE
055137,001462: 12,3355 25431 NEGP
055138,001463: 12,3356 25431 NEGP
055139,001464: 12,3357 16742 STODL P # P=(1-CSTH)/(SNTH COGA-(CSTH-RHO)) (+4)
055140,001465: 12,3360 03775 COGA
055141,001466: 12,3361 43316 DSQ DAD
055142,001467: 12,3362 11620 D1/1024
055143,001468: 12,3363 41301 NORM DMP
055144,001469: 12,3364 00047 X1
Page 1298 |
055146,001471: 12,3365 02742 P
055147,001472: 12,3366 44257 SR* BDSU
055148,001473: 12,3367 20571 0 -8D,1
055149,001474: 12,3370 11616 D1/32
055150,001475: 12,3371 16744 STODL R1A # R1A=2-P(1+COGA COGA) (+6)
055151,001476:
055152,001477: 12,3372 02742 P
055153,001478: 12,3373 45000 BOV CALL
055154,001479: 12,3374 25434 HIENERGY
055155,001480: 12,3375 25001 GETX
055156,001481: 12,3376 77745 DLOAD
055157,001482: 12,3377 00037 T
055158,001483: 12,3400 16764 STODL TPREV
055159,001484: 12,3401 00031 XI
055160,001485: 12,3402 45014 BON CALL
055161,001486: 12,3403 04310 INFINFLG
055162,001487: 12,3404 25431 NEGP # HAVE EXCEEDED THEORETICAL BOUNDS
055163,001488: 12,3405 24433 DELTIME
055164,001489: 12,3406 44200 BOV BDSU
055165,001490: 12,3407 25450 BIGTIME
055166,001491: 12,3410 02673 TDESIRED
055167,001492: 12,3411 02762 STORE TERRLAMB
055168,001493: 12,3412 44246 ABS BDSU
055169,001494: 12,3413 03777 EPSILONL
055170,001495: 12,3414 47044 BPL RTB
055171,001496: 12,3415 25515 INITV
055172,001497: 12,3416 24656 CHECKCTR
055173,001498: 12,3417 45030 BHIZ CALL
055174,001499: 12,3420 25460 SUFFCHEK
055175,001500: 12,3421 24550 ITERATOR
055176,001501: 12,3422 53145 DLOAD BZE
055177,001502: 12,3423 00155 MPAC
055178,001503: 12,3424 25460 SUFFCHEK
055179,001504: 12,3425 77615 DAD
055180,001505: 12,3426 03775 COGA
055181,001506: 12,3427 37775 STCALL COGA
055182,001507: 12,3430 25343 LAMBLOOP
055183,001508:
055184,001509: 12,3431 51145 NEGP DLOAD BPL # IMPOSSIBLE TRAJECTORY DUE TO INACCURATE
055185,001510: 12,3432 00015 DCOGA # BOUND CALCULATION. TRY NEW COGA.
055186,001511: 12,3433 25453 LOENERGY
055187,001512:
055188,001513: 12,3434 71201 HIENERGY SETPD DLOAD # HIGH ENERGY TRAJECTORY RESULTED
055189,001514: 12,3435 00001 0
055190,001515: 12,3436 03775 COGA # IN OVFL OF P OR R1A, OR XI EXCEEDING 50.
055191,001516: 12,3437 00011 STORE COGAMIN # THIS IS THE NEW BOUND.
055192,001517: 12,3440 70545 COMMONLM DLOAD SR1
055193,001518: 12,3441 00015 DCOGA
Page 1299 |
055195,001520: 12,3442 00015 STORE DCOGA # USE DCOGA/2 AS DECREMENT
055196,001521: 12,3443 44254 BZE BDSU
055197,001522: 12,3444 25460 SUFFCHEK
055198,001523: 12,3445 03775 COGA
055199,001524: 12,3446 37775 STCALL COGA
055200,001525: 12,3447 25343 LAMBLOOP
055201,001526:
055202,001527: 12,3450 77745 BIGTIME DLOAD
055203,001528: 12,3451 02764 TPREV
055204,001529: 12,3452 00037 STORE T
055205,001530:
055206,001531: 12,3453 71201 LOENERGY SETPD DLOAD # LOW ENERGY TRAJECTORY RESULTED
055207,001532: 12,3454 00001 0
055208,001533: 12,3455 03775 COGA # IN OVERFLOW OF TIME.
055209,001534: 12,3456 34017 STCALL COGAMAX # THIS IS THE NEW BOUND.
055210,001535: 12,3457 25440 COMMONLM
055211,001536:
055212,001537: 12,3460 51545 SUFFCHEK DLOAD ABS
055213,001538: 12,3461 02762 TERRLAMB
055214,001539: 12,3462 41325 PDDL DMP
055215,001540: 12,3463 02673 TDESIRED # PL AT 2D
055216,001541: 12,3464 11612 D1/4
055217,001542: 12,3465 45215 DAD DSU # PL AT 0D
055218,001543: 12,3466 11632 ONEBIT
055219,001544: 12,3467 43044 BPL SETGO
055220,001545: 12,3470 25515 INITV
055221,001546: 12,3471 02434 SOLNSW
055222,001547: 12,3472 02712 RTNLAMB
055223,001548:
055224,001549: 12,3473 43001 360LAMB SETPD SETGO # LAMBERT CANNOT HANDLE CSTH=1
055225,001550: 12,3474 00001 0
055226,001551: 12,3475 02434 SOLNSW
055227,001552: 12,3476 02712 RTNLAMB
055228,001553:
055229,001554: 12,3477 71331 NOGUESS SSP DLOAD
055230,001555: 12,3500 00051 TWEEKIT
055231,001556: 12,3501 10000 20000
055232,001557: 12,3502 00011 COGAMIN
055233,001558: 12,3503 65342 SR1 PDDL # PL AT 2
055234,001559: 12,3504 00017 COGAMAX
055235,001560: 12,3505 43342 SR1 DAD
055236,001561: 12,3506 77626 STADR # PL AT 0
055237,001562: 12,3507 74002 STORE COGA
055238,001563: 12,3510 34015 STCALL DCOGA
055239,001564: 12,3511 25343 LAMBLOOP
Page 1300 |
055241,001566: 12,3512 52145 LOLIM DLOAD GOTO
055242,001567: 12,3513 11636 COGLOLIM # COGLOLIM=-.999511597
055243,001568: 12,3514 25333 MINCOGA
055244,001569:
055245,001570: 12,3515 60345 INITV DLOAD NORM
055246,001571: 12,3516 00041 R1
055247,001572: 12,3517 00047 X1
055248,001573: 12,3520 70525 PDDL SR1 # PL AT 2
055249,001574: 12,3521 02742 P
055250,001575: 12,3522 77671 DDV # PL AT 0
055251,001576: 12,3523 75457 SL* SQRT
055252,001577: 12,3524 20175 0 -4,1
055253,001578: 12,3525 72405 DMP SL1
055254,001579: 12,3526 00021 ROOTMU
055255,001580: 12,3527 41206 PUSH DMP # 0D=VTAN (+7) PL AT 2
055256,001581: 12,3530 03775 COGA
055257,001582: 12,3531 74261 SL VXSC
055258,001583: 12,3532 20206 5
055259,001584: 12,3533 02724 UR1
055260,001585: 12,3534 77725 PDDL # XCH WITH 0D PL AT 0,6
055261,001586: 12,3535 76561 VXSC VSL1
055262,001587: 12,3536 02676 UN
055263,001588: 12,3537 53235 VXV VAD
055264,001589: 12,3540 02724 UR1 # PL AT 0
055265,001590: 12,3541 43172 VSL1 CLEAR
055266,001591: 12,3542 02674 SOLNSW
055267,001592: 12,3543 02746 STORE VVEC
055268,001593: 12,3544 53135 SLOAD BZE
055269,001594: 12,3545 02704 VTARGTAG
055270,001595: 12,3546 25551 TARGETV
055271,001596: 12,3547 77650 GOTO
055272,001597: 12,3550 02712 RTNLAMB
055273,001598:
055274,001599: 12,3551 45145 TARGETV DLOAD CALL
055275,001600: 12,3552 02722 MAGVEC2
055276,001601: 12,3553 24713 LAMENTER
055277,001602: 12,3554 36705 STCALL VTARGET
055278,001603: 12,3555 02712 RTNLAMB
055279,001604:
Page 1301 |
055281,001606: 12,3556 40220 TIMERAD STQ SETPD # PL AT 0
055282,001607: 12,3557 02712 RTNTR
055283,001608: 12,3560 00001 0
055284,001609: 12,3561 77600 BOV
055285,001610: 12,3562 25563 +1
055286,001611: 12,3563 63375 VLOAD PDVL # PL AT 6
055287,001612: 12,3564 02657 RVEC
055288,001613: 12,3565 02746 VVEC
055289,001614: 12,3566 77624 CALL
055290,001615: 12,3567 11637 PARAM
055291,001616: 12,3570 71200 BOV DLOAD
055292,001617: 12,3571 24776 COGAOVFL # PL AT 0
055293,001618: 12,3572 11616 D1/32
055294,001619: 12,3573 41225 DSU DMP
055295,001620: 12,3574 02744 R1A
055296,001621: 12,3575 02742 P
055297,001622: 12,3576 41366 SQRT DMP
055298,001623: 12,3577 03775 COGA
055299,001624: 12,3600 74212 SL4 VXSC
055300,001625: 12,3601 02714 U2
055301,001626: 12,3602 45325 PDDL DSU # PL AT 6
055302,001627: 12,3603 11610 D1/64
055303,001628: 12,3604 02744 R1A
055304,001629: 12,3605 52361 VXSC VSU # PL AT 0
055305,001630: 12,3606 02724 UR1
055306,001631: 12,3607 53512 VSL4 UNIT
055307,001632: 12,3610 77600 BOV
055308,001633: 12,3611 25667 CIRCULAR
055309,001634: 12,3612 60325 PDDL NORM # 0D=UNIT(ECC) (+3) PL AT 6
055310,001635: 12,3613 02760 RDESIRED # 36D=ECC (+3)
055311,001636: 12,3614 00047 X1
055312,001637: 12,3615 41325 PDDL DMP # PL AT 8
055313,001638: 12,3616 00041 R1
055314,001639: 12,3617 02742 P
055315,001640: 12,3620 56257 SL* DDV # PL AT 6
055316,001641: 12,3621 20201 0,1
055317,001642: 12,3622 56225 DSU DDV
055318,001643: 12,3623 11614 D1/16
055319,001644: 12,3624 00045 36D # 36D=ECC (+3)
055320,001645: 12,3625 00031 STORE COSF
055321,001646: 12,3626 63400 BOV DSQ
055322,001647: 12,3627 25673 BADR2
055323,001648: 12,3630 50021 BDSU BMN
055324,001649: 12,3631 11612 D1/4
055325,001650: 12,3632 25673 BADR2
055326,001651: 12,3633 75366 SQRT SIGN
055327,001652: 12,3634 02757 SGNRDOT
055328,001653: 12,3635 77614 CLEAR
055329,001654: 12,3636 04272 APSESW
055330,001655:
Page 1302 |
055332,001657: 12,3637 76561 TERMNVEC VXSC VSL1
055333,001658: 12,3640 02676 UN
055334,001659: 12,3641 63235 VXV PDVL # VXCH WITH 0D PL AT 0,6
055335,001660: 12,3642 00001 0D
055336,001661: 12,3643 53361 VXSC VAD # PL AT 0
055337,001662: 12,3644 00031 COSF
055338,001663: 12,3645 41572 VSL1 PUSH # 0D=U2 PL AT 6
055339,001664:
055340,001665: 12,3646 56241 DOT DDV # LIMITS RESULT TO POSMAX OR NEGMAX
055341,001666: 12,3647 02724 UR1
055342,001667: 12,3650 23756 DP1/4
055343,001668: 12,3651 40142 SR1 BOV # SCALE BACK DOWN TO NORMAL
055344,001669: 12,3652 25653 +1 # CLEAR OVFIND IF SET
055345,001670: 12,3653 26734 STOVL CSTH # CSTH (+1)
055346,001671: 12,3654 02724 UR1
055347,001672: 12,3655 76435 VXV VSL1
055348,001673: 12,3656 72441 DOT SL1
055349,001674: 12,3657 02676 UN
055350,001675: 12,3660 16732 STODL SNTH # SNTH (+1)
055351,001676: 12,3661 02742 P
055352,001677: 12,3662 77624 CALL
055353,001678: 12,3663 25001 GETX
055354,001679: 12,3664 77614 CLRGO
055355,001680: 12,3665 02634 SOLNSW
055356,001681: 12,3666 24761 COMMNOUT
055357,001682:
055358,001683: 12,3667 43001 CIRCULAR SETPD SETGO
055359,001684: 12,3670 00001 0
055360,001685: 12,3671 02434 SOLNSW
055361,001686: 12,3672 25751 ABTCONIC
055362,001687:
055363,001688: 12,3673 75345 BADR2 DLOAD SIGN
055364,001689: 12,3674 11564 LODPHALF
055365,001690: 12,3675 00031 COSF
055366,001691: 12,3676 14031 STODL COSF
055367,001692: 12,3677 11566 KEPZERO
055368,001693: 12,3700 77614 SETGO
055369,001694: 12,3701 04032 APSESW
055370,001695: 12,3702 25637 TERMNVEC
055371,001696:
Page 1303 |
055373,001698: 12,3703 40220 APSIDES STQ SETPD # PL AT 0
055374,001699: 12,3704 02712 RTNAPSE
055375,001700: 12,3705 00001 0D
055376,001701: 12,3706 77600 BOV
055377,001702: 12,3707 25710 +1
055378,001703: 12,3710 63375 VLOAD PDVL # PL AT 6
055379,001704: 12,3711 02657 RVEC
055380,001705: 12,3712 02746 VVEC
055381,001706: 12,3713 77624 CALL
055382,001707: 12,3714 11637 PARAM
055383,001708: 12,3715 77600 BOV # PL AT 0
055384,001709: 12,3716 25717 GETECC
055385,001710: 12,3717 42405 GETECC DMP SL4
055386,001711: 12,3720 02744 R1A
055387,001712: 12,3721 75421 BDSU SQRT
055388,001713: 12,3722 11610 D1/64
055389,001714: 12,3723 02754 STORE ECC
055390,001715: 12,3724 65215 DAD PDDL # PL AT 2
055391,001716: 12,3725 11604 D1/8
055392,001717: 12,3726 00041 R1
055393,001718: 12,3727 72405 DMP SL1
055394,001719: 12,3730 02742 P
055395,001720: 12,3731 77671 DDV # PL AT 0
055396,001721: 12,3732 60325 PDDL NORM # 0D=RP (+29 OR +27) PL AT 2
055397,001722: 12,3733 02744 R1A
055398,001723: 12,3734 00047 X1
055399,001724: 12,3735 53725 PDDL SL* # PL AT 4
055400,001725: 12,3736 00041 R1
055401,001726: 12,3737 20174 0 -5,1
055402,001727: 12,3740 45271 DDV DSU # PL AT 2,0
055403,001728: 12,3741 50000 BOV BMN
055404,001729: 12,3742 25746 INFINAPO
055405,001730: 12,3743 25746 INFINAPO
055406,001731: 12,3744 77650 GOTO
055407,001732: 12,3745 02712 RTNAPSE
055408,001733: 12,3746 52145 INFINAPO DLOAD GOTO # RETURNS WITH APOAPSIS IN MPAC, PERIAPSIS
055409,001734: 12,3747 11577 LDPOSMAX
055410,001735: 12,3750 02712 RTNAPSE # THAT PL IS AT 0.
055411,001736:
Page 1304 |
055413,001738: 12,3751 77776 ABTCONIC EXIT
055414,001739: 12,3752 05721 TC POODOO
055415,001740: 12,3753 00607 OCT 00607
055416,001741:
Page 1305 |
055418,001743: 04,2000 SETLOC CONICS1
055419,001744: 04,2000 BANK
055420,001745:
055421,001746: 04,3737 COUNT 04/CONIC
055422,001747:
055423,001748: 04,3737 22437 16067 MUTABLE 2DEC* 3.986032 E10 B-36* # MUE
055424,001749:
055425,001750: 04,3741 15625 21042 2DEC* .25087606 E-10 B+34* # 1/MUE
055426,001751:
055427,001752: 04,3743 30276 04773 2DEC* 1.99650495 E5 B-18* # SQRT(MUE)
055428,001753:
055429,001754: 04,3745 25004 06702 2DEC* .50087529 E-5 B+17* # 1/SQRT(MUE)
055430,001755:
055431,001756: 04,3747 16471 01352 2DEC 4.902778 E8 B-30 # MUM
055432,001757:
055433,001758: 04,3751 21412 20500 2DEC .203966 E-8 B+28 # 1/MUM
055434,001759:
055435,001760: 04,3753 25477 03367 2DEC* 2.21422176 E4 B-15* # SQRT(MUM)
055436,001761:
055437,001762: 04,3755 27533 07571 2DEC* .45162595 E-4 B+14* # 1/SQRT(MUM)
055438,001763:
055439,001764: 04,3757 04,3576 LDPOSMAX EQUALS LODPMAX # DPPOSMAX IN LOW MEMORY.
055440,001765:
055441,001766: # ERASABLE ASSIGNMENTS
055442,001767:
055443,001768: # KEPLER SUBROUTINE
055444,001769:
055445,001770: # INPUT -
055446,001771: # RRECT ERASE +5
055447,001772: # VRECT ERASE +5
055448,001773: # TAU. ERASE +1
055449,001774: # XKEP ERASE +1
055450,001775: # TC ERASE +1
055451,001776: # XPREV ERASE +1
055452,001777: 04,3757 1/MU EQUALS 14D
055453,001778: 04,3757 ROOTMU EQUALS 16D
055454,001779: 04,3757 1/ROOTMU EQUALS 18D
055455,001780:
055456,001781: # OUTPUT -
055457,001782: # RCV ERASE +5
055458,001783: # VCV ERASE +5
055459,001784: # RC ERASE +1
055460,001785: # XPREV ERASE +1
055461,001786:
055462,001787: # DEBRIS -
055463,001788: 04,3757 ALPHA EQUALS 8D
055464,001789: 04,3757 XMAX EQUALS 10D
Page 1306 |
055466,001791: 04,3757 XMIN EQUALS 12D
055467,001792: 04,3757 X EQUALS 20D
055468,001793: 04,3757 XI EQUALS 24D
055469,001794: 04,3757 S(XI) EQUALS 26D
055470,001795: 04,3757 XSQC(XI) EQUALS 28D
055471,001796: 04,3757 T EQUALS 30D
055472,001797: 04,3757 R1 EQUALS 32D
055473,001798: 04,3757 KEPC1 EQUALS 34D
055474,001799: 04,3757 KEPC2 EQUALS 36D
055475,001800:
055476,001801: # DELX ERASE +1
055477,001802: # DELT ERASE +1
055478,001803: # URRECT ERASE +5
055479,001804: # RCNORM ERASE +1
055480,001805: # XPREV EQUALS XKEP
055481,001806:
055482,001807:
055483,001808: # LAMBERT SUBROUTINE
055484,001809:
055485,001810: # INPUT -
055486,001811: # R1VEC ERASE +5
055487,001812: # R2VEC ERASE +5
055488,001813: # TDESIRED ERASE +1
055489,001814: # GEOMSGN ERASE +0
055490,001815: # GUESSW 0 IF COGA GUESS AVAILABLE, 1 IF NOT
055491,001816: # COGA ERASE +1 INPUT ONLY IF GUESSW IS ZERO.
055492,001817: # NORMSW 0 IF UN TO BE COMPUTED, 1 IF UN INPUT
055493,001818: # UN ERASE +5 ONLY USED IF NORMSW IS 1
055494,001819: # VTARGTAG ERASE +0
055495,001820: # TWEEKIT EQUALS 40D ONLY USED IF GUESSW IS 0
055496,001821:
055497,001822: # OUTPUT -
055498,001823: # VTARGET ERASE +5 AVAILABLE ONLY IF VTARGTAG IS ZERO.
055499,001824: # V1VEC EQUALS MPAC
055500,001825:
055501,001826: # DEBRIS -
055502,001827: # RTNLAMB ERASE +0
055503,001828: # U2 ERASE +5
055504,001829: # MAGVEC2 ERASE +1
055505,001830: # UR1 ERASE +5
055506,001831: # R1 EQUALS 31D
055507,001832: # UN ERASE +5
055508,001833: # SNTH ERASE +1
055509,001834: # CSTH ERASE +1
055510,001835: # 1-CSTH ERASE +1
055511,001836: # CSTH-RHO ERASE +1
055512,001837:
055513,001838: 04,3757 COGAMAX EQUALS 14D # CLOBBERS 1/MU
055514,001839: 04,3757 COGAMIN EQUALS 8D
055515,001840: 04,3757 DCOGA EQUALS 12D
055516,001841:
055517,001842: # TWEEKIT EQUALS 40D
055518,001843: # P ERASE +1
Page 1307 |
055520,001845: # COGA ERASE +1
055521,001846: # R1A ERASE +1
055522,001847: # X EQUALS 20D
055523,001848: # XSQ EQUALS 22D
055524,001849: # XI EQUALS 24D
055525,001850: # S(XI) EQUALS 26D
055526,001851: # XSQC(XI) EQUALS 28D
055527,001852: # T EQUALS 30D
055528,001853: # KEPC1 EQUALS 34D
055529,001854: # KEPC2 EQUALS 36D
055530,001855: # SLOPESW
055531,001856: # SOLNSW
055532,001857:
055533,001858: # OTHERS -
055534,001859: # RVEC EQUALS R1VEC
055535,001860: # VVEC ERASE +5
055536,001861: # COGAFLAG
055537,001862: # RVSW
055538,001863: # INFINFLG
055539,001864: # APSESW
055540,001865: # 360SW
055541,001866: # RTNTT EQUALS RTNLAMB
055542,001867: # ECC ERASE +1
055543,001868: # RTNTR EQUALS RTNLAMB
055544,001869: # RTNAPSE EQUALS RTNLAMB
055545,001870: # R2 EQUALS MAGVEC2
055546,001871:
055547,001872: 04,3757 COSF EQUALS 24D
055548,001873:
055549,001874: # RTNPRM ERASE +0
055550,001875: # SGNRDOT ERASE +0
055551,001876: # RDESIRED ERASE +1
055552,001877:
055553,001878:
055554,001879: # ITERATOR SUBROUTINE
055555,001880:
055556,001881: # ORDERSW
055557,001882: 04,3757 MAX EQUALS 14D # CLOBBERS 1/MU
055558,001883: 04,3757 MIN EQUALS 8D
055559,001884:
055560,001885: # INDEP ERASE +1
055561,001886:
055562,001887: 04,3757 DELINDEP EQUALS 12D
055563,001888: 04,3757 ITERCTR EQUALS 22D
055564,001889: 04,3757 DEP EQUALS 30D
055565,001890:
055566,001891: # DELDEP ERASE +1
055567,001892: # DEPREV ERASE +1
055568,001893:
055569,001894: 04,3757 TWEEKIT EQUALS 40D
055570,001895:
055571,001896:
055572,001897: # MORE KEPLER
055573,001898:
055574,001899: # EPSILONT ERASE +1
055575,001900:
Page 1308 |
055577,001902: # MORE LAMBERT
055578,001903:
055579,001904: # TERRLAMB EQUALS DELDEP
055580,001905: # TPREV EQUALS DEPREV
055581,001906:
055582,001907: # EPSILONL EQUALS EPSILONT +2 DOUBLE PRECISION WORD
055583,001908:
055584,001909:
End of include-file CONIC_SUBROUTINES.agc. Parent file is MAIN.agc