Source Code
|
This is a reconstruction of the AGC program Luminary 99 Rev 0. It was the third release
of the Lunar Module flight software targeted for use in Apollo 11, after Luminary 96 and 97.
A bug (which had been around since at least Apollo 10, Luminary 69) was
discovered in Rev 0 shortly before the Apollo 11 flight, resulting in a last minute
revision into Rev 1,
which is what actually flew rather than
the Rev 0 presented here. A hardcopy of Rev 0 is known to
exist — it belonged to AGC developer Allan Klumpp for many years — but
unfortunately the Virtual AGC Project has not had access to that hardcopy. Thus
the code you see here had been reconstructed (we believe accurately) rather than
transcribed. The first step of the reconstruction of the Rev 0 source code was
the transcription of the Rev 1 source code from a hardcopy in the MIT Museum collection.
The process of reverting the active portion of the source code (i.e., other than
program comments) from Rev 1 to Rev 0 was very minor, consisting
only of moving the position of the STARTSB1 label in
FRESH START AND RESTART. Allan had previously given
us the checksums of the memory banks of Rev 0, and we have verified the program presented here has checksums
identical to all banks of Allan's listing of Rev 0. The notations on Allan's Rev 0 program listing read,
in part:GAP: ASSEMBLE REVISION 099 OF AGC PROGRAM LUMINARY BY NASA 2021112-051 A single program comment is known to differ between Rev 0 and Rev 1, but these are harder to reconstruct and verify than changes to the active portion of the code. Thus it is possible that there are additional differences between the program comments in Rev 0 and Rev 1 that are unknown to us, and therefore are not reflected in the code presented here. |
050482,000002: ## Copyright: Public domain.
050483,000003: ## Filename: CONIC_SUBROUTINES.agc
050484,000004: ## Purpose: Part of the reconstructed source code for LMY99 Rev 0,
050485,000005: ## otherwise known as Luminary Rev 99, the third release
050486,000006: ## of the Apollo Guidance Computer (AGC) software for Apollo 11.
050487,000007: ## It differs from LMY99 Rev 1 (the flown version) only in the
050488,000008: ## placement of a single label. The corrections shown here have
050489,000009: ## been verified to have the same bank checksums as AGC developer
050490,000010: ## Allan Klumpp's copy of Luminary Rev 99, and so are believed
050491,000011: ## to be accurate. This file is intended to be a faithful
050492,000012: ## recreation, except that the code format has been changed to
050493,000013: ## conform to the requirements of the yaYUL assembler rather than
050494,000014: ## the original YUL assembler.
050495,000015: ##
050496,000016: ## Assembler: yaYUL
050497,000017: ## Contact: Jim Lawton <jim DOT lawton AT gmail.com>
050498,000018: ## Website: www.ibiblio.org/apollo.
050499,000019: ## Pages: 1159-1204
050500,000020: ## Mod history: 2009-05-28 JL Started updating from page images.
050501,000021: ## 2009-06-02 JL Finished updating from page images.
050502,000022: ## 2010-12-31 JL Fixed page number comments.
050503,000023: ## 2016-12-17 RSB Proofed text comments with octopus/ProoferComments
050504,000024: ## and corrected the errors found.
050505,000025: ## 2017-01-28 RSB WTIH -> WITH and WHCIH -> WHICH.
050506,000026: ## 2017-03-14 RSB Comment-text fixes noted in proofing Luminary 116.
050507,000027: ## 2017-03-15 RSB Comment-text fixes identified in 5-way
050508,000028: ## side-by-side diff of Luminary 69/99/116/131/210.
050509,000029: ## 2017-03-17 RSB Comment-text fixes identified in diff'ing
050510,000030: ## Luminary 99 vs Comanche 55.
050511,000031: ## 2017-08-01 MAS Created from LMY99 Rev 1.
050512,000032:
050513,000033: ## This source code has been transcribed or otherwise adapted from
050514,000034: ## digitized images of a hardcopy from the MIT Museum. The digitization
050515,000035: ## was performed by Paul Fjeld, and arranged for by Deborah Douglas of
050516,000036: ## the Museum. Many thanks to both. The images (with suitable reduction
050517,000037: ## in storage size and consequent reduction in image quality as well) are
050518,000038: ## available online at www.ibiblio.org/apollo. If for some reason you
050519,000039: ## find that the images are illegible, contact me at info@sandroid.org
050520,000040: ## about getting access to the (much) higher-quality images which Paul
050521,000041: ## actually created.
050522,000042: ##
050523,000043: ## The code has been modified to match LMY99 Revision 0, otherwise
050524,000044: ## known as Luminary Revision 99, the Apollo 11 software release preceeding
050525,000045: ## the listing from which it was transcribed. It has been verified to
050526,000046: ## contain the same bank checksums as AGC developer Allan Klumpp's listing
050527,000047: ## of Luminary Revision 99 (for which we do not have scans).
050528,000048: ##
050529,000049: ## Notations on Allan Klumpp's listing read, in part:
050530,000050: ##
050531,000051: ## ASSEMBLE REVISION 099 OF AGC PROGRAM LUMINARY BY NASA 2021112-51
050532,000052:
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Page 1159 |
050534,000054: # PROGRAM DESCRIPTION - ENTIRE CONIC SUBROUTINE LOG SECTION DATE - 1 SEPTEMBER 1967
050535,000055: # MOD NO. - 0 LOG SECTION - CONIC SUBROUTINES
050536,000056: # MOD BY KRAUSE ASSEMBLY - COLOSSUS REVISION 88
050537,000057:
050538,000058: # FUNCTIONAL DESCRIPTION -
050539,000059: # THE FOLLOWING SET OF SUBROUTINES SOLVE VARIOUS PROBLEMS INVOLVING THE TRAJECTORY PRODUCED BY A CENTRAL
050540,000060: # INVERSE-SQUARE FORCE ACTING ON A POINT MASS, AS OUTLINED IN THE CMC AND LGC LUNAR LANDING MISSION GSOP, SECTION
050541,000061: # 5.5.1.2. A GENERAL USAGE POINT-OF-VIEW WAS TAKEN IN FORMULATING, MECHANIZING, AND SCALING THE SUBROUTINES,
050542,000062: # RATHER THAN OPTIMIZING EACH FOR A PARTICULAR USE. THEREFORE, MULTIPLE USAGE CAN BE MADE OF THE SUBROUTINES
050543,000063: # INVOLVING ANY REALISTIC SET OF CONSTRAINTS. IT SHOULD BE NOTED THAT ONLY ONE SET OF CODING IS USED, WHETHER THE
050544,000064: # EARTH, MOON, OR ANY OTHER CELESTIAL BODY IS SPECIFIED AS THE CENTRAL BODY OF THE PROBLEM, PROVIDED ONE OBSERVES
050545,000065: # THE INHERENT SCALE CHANGE REQUIRED IN POSITION, VELOCITY, MU, AND TIME, AS OUTLINED IN MISSION PROGRAMMING
050546,000066: # DEFINITION MEMO NO. 10. THIS CAN BE ACCOMPLISHED BY SIMPLY ADDING TO THE MUTABLE AND INITIALIZING THE SUBROU-
050547,000067: # TINES APPROPRIATELY.
050548,000068:
050549,000069: # DUE TO THE UNIFORMITY OF THE EQUATIONS INVOLVED, CODING WAS MINIMIZED BY TREATING INDIVIDUAL EQUATIONS AND
050550,000070: # BLOCKS OF EQUATIONS AS SUBROUTINES OF LOWER RANK WHENEVER POSSIBLE. AS A RESULT, THREE BY-PRODUCTS SUBROUTINES,
050551,000071: # DIRECTLY USABLE AS INDEPENDENT SUBROUTINES, WERE GENERATED.
050552,000072:
050553,000073: # RESTRICTIONS -
050554,000074: # THE ONLY LIMITATION IN THE SCOPE OF PROBLEM WHICH CAN BE SOLVED BY A PARTICULAR SUBROUTINE IS THE SCALING
050555,000075: # LIMIT OF EACH PARAMETER AS SPECIFIED IN THE GSOP. THESE SCALING LIMITS WERE CHOSEN SO THAT ALL FEASIBLE TRAJEC-
050556,000076: # TORIES COULD BE HANDLED.
050557,000077:
050558,000078: # SINCE THE SUBROUTINES (EXCEPT KEPLER) USE COMMON SUBROUTINES OF LOWER RANK WHICH USE ERASABLE OTHER THAN
050559,000079: # THE PUSHLIST (DUE TO ITS LIMITED SIZE) AND COMMON INTERPRETIVE SWITCHES, THE CONIC SUBROUTINES CANNOT BE ALLOWED
050560,000080: # TO INTERRUPT EACH OTHER. IT IS UP TO THE USER TO GUARANTEE THIS CONDITION.
050561,000081:
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Page 1160 |
050563,000083: # PROGRAM DESCRIPTION - KEPLER SUBROUTINE DATE - 11 OCTOBER 1967
050564,000084: # MOD NO. -1 LOG SECTION - CONIC SUBROUTINES
050565,000085: # MOD BY KRAUSE ASSEMBLY - COLOSSUS 103 AND SUNDANCE 222
050566,000086: # MOD NO. - 2 (AUGUST 1968) BY ROBERTSON: TO PERMIT BACKDATING BY MORE THAN ONE ORBITAL PERIOD.
050567,000087: # MOD NO. - 3 (DEC 1968) BY ROBERTSON: SUPPRESSION OF X-MODULO-ING
050568,000088: # MOD. NO. - 4 (JAN 1969) BY ROBERTSON: CLEAR OVFIND AT KEPLER ENTRY
050569,000089:
050570,000090: # FUNCTIONAL DESCRIPTION -
050571,000091: # THIS SUBROUTINE, GIVEN AN INITIAL STATE VECTOR AND THE DESIRED TRANSFER TIME THROUGH WHICH THE STATE IS TO
050572,000092: # BE UPDATED ALONG A CONIC TRAJECTORY, COMPUTES THE NEW, UPDATED STATE VECTOR. THE TRAJECTORY MAY BE ANY CONIC
050573,000093: # SECTION - CIRCULAR, ELLIPTIC, PARABOLIC, HYPERBOLIC, OR RECTILINEAR WITH RESPECT TO THE EARTH OR THE MOON. THE
050574,000094: # USE OF THE SUBROUTINE CAN BE EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT
050575,000095: # INTRODUCING ANY CODING CHANGES, ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY. AN ITERA-
050576,000096: # TION TECHNIQUE IS UTILIZED IN THE COMPUTATION.
050577,000097:
050578,000098: # IF A NEGATIVE TIME-OF-FLIGHT IS INPUT, THE PROGRAM WILL SOLVE FOR THE STATE WHICH WOULD BE PRODUCED BY
050579,000099: # EXTRAPOLATING THE POSITION BACKWARD IN TIME.
050580,000100:
050581,000101: # IF THE ABSOLUTE VALUE OF THE DESIRED TRANSFER TIME EXCEEDS THE ORBITAL PERIOD, THE SUBROUTINE, THROUGH A
050582,000102: # MODULAR TECHNIQUE, WILL COMPUTE THE STATE CORRESPONDING TO THE DESIRED TIME (WHETHER POSITIVE OR NEGATIVE).
050583,000103:
050584,000104: # THE RESTRICTIONS ARE -
050585,000105: # 1. (PREVIOUS RESTRICTION ON THE NEGATIVE DESIRED TRANSFER TIME IS NOW DELETED.)
050586,000106: # 2. THE PARAMETERS IN THE PROBLEM CANNOT EXCEED THEIR SCALING LIMITS AS SPECIFIED IN THE GSOP. IF
050587,000107: # ANY OF THESE LIMITS ARE EXCEEDED, THE RESULTING SOLUTION WILL BE MEANINGLESS.
050588,000108:
050589,000109: # THE NUMBER OF ITERATIONS AND, THEREFORE, THE COMPUTATION SPEED IS DEPENDENT ON THE ACCURACY OF THE
050590,000110: # GUESS, XKFPNEW. THE AGC COMPUTATION TIME IS APPROXIMATELY .061 SECONDS FOR INITIALIZATION, .065 SECONDS FOR THE
050591,000111: # FINAL COMPUTATIONS, PLUS .083 SECONDS FOR EACH ITERATION.
050592,000112:
050593,000113: # REFERENCES -
050594,000114: # R-479, MISSION PROGRAMMING DEFINITION MEMO NO. 10, LUNAR LANDING MISSION GSOP, SECTION 5.5, SGA
050595,000115: # MEMO 67-4.
050596,000116:
050597,000117: # INPUT - ERASABLE INITIALIZATION REQUIRED
050598,000118: # * SCALE FACTOR *
050599,000119: # VARIABLE *IN POWERS OF 2 * DESCRIPTION AND REMARKS
050600,000120: # -------- *-------------- * -----------------------
050601,000121: # RRECT * +29 FOR EARTH * DP INITIAL POSITION VECTOR IN METERS
050602,000122: # * +27 FOR MOON *
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Page 1161 |
050604,000124: # VRECT * +7 FOR EARTH * DP INITIAL VELOCITY VECTOR IN METERS/CENTISECOND
050605,000125: # * +5 FOR MOON *
050606,000126: # X1 (38D) * NONE * INDEX REGISTER SET TO -2D OR -10D ACCORDING TO WHETHER THE EARTH OR MOON,
050607,000127: # * * RESPECTIVELY, IS THE CENTRAL BODY
050608,000128: # TAU. * +28 * DESIRED TRANSFER TIME IN CENTISECONDS (DP)
050609,000129: # * * MAY BE POS OR NEG AND ABSOLUTE VALUE MAY BE GREATER OR LESS THAN ONE ORBITAL PERIOD.
050610,000130: # XKEPNEW * +17 FOR EARTH * DP GUESS OF ROOT X OF KEPLERS EQN IN SQRT(METERS). SIGN SHOULD AGREE WITH THAT OF TAU.
050611,000131: # * +16 FOR MOON * AND ABS VALUE SHOULD BE LESS THAN THAT CORRESPONDING TO A PERIOD, VIZ, 2PI SQRT(SEMI-
050612,000132: # * * MAJOR AXIS), FOR SPEED OF CONVERGENCE, BUT IF EITHER CONDITION FAILS, XKEPNEW IS RESET
050613,000133: # * * BY KEPLER TO A POOR BUT VALID GUESS.
050614,000134: # TC * +28 * DP PREV. VALUE OF TIME IN CENTISECS. MUST BE LESS THAN ONE ORBITAL PERIOD.
050615,000135: # XPREV * +17 FOR EARTH * DP PREV. VALUE OF X IN SQRT(METERS). MUST BE LESS THAN AN X CORRESPONDING TO ONE
050616,000136: # * +16 FOR MOON * ORBITAL PERIOD, VIZ, 2PI SQRT(SEMI-MAJOR AXIS)
050617,000137:
050618,000138: # SUBROUTINES CALLED -
050619,000139: # DELTIME
050620,000140:
050621,000141: # CALLING SEQUENCE AND NORMAL EXIT MODES -
050622,000142: # KEPRTN-2 GOTO MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
050623,000143: # KEPRTN-1 KEPLER RETURNS WITH XPREV IN MPAC. PL IS AT 0.
050624,000144: # KEPRTN ... CONTINUE
050625,000145:
050626,000146: # KEPLER MUST NOT BE CALLED DIRECTLY SINCE AN INTERRUPTION OF IT WOULD DESTROY THE ERASABLES IT NEEDS TO COMPLETE
050627,000147: # THE INTERRUPTED JOB. THEREFORE THE USER MUST CALL CSMCONIC OR LEMCONIC WHICH GUARANTEES NO INTERRUPTS AND WHICH
050628,000148: # ALSO CALLS KEPPREP TO COMPUTE A GUESS OF XKEPNEW.
050629,000149:
050630,000150: # ABORT EXIT MODES -
050631,000151: # NONE
050632,000152:
050633,000153: # OUTPUT -
050634,000154: # * SCALE FACTOR *
050635,000155: # VARIABLE *IN POWERS OF 2 * DESCRIPTION AND REMARKS
050636,000156: # -------- *-------------- * -----------------------
050637,000157: # RCV * +29 FOR EARTH * DP TERMINAL POSITION VECTOR IN METERS
050638,000158: # * +27 FOR MOON *
050639,000159: # VCV * +7 FOR EARTH * DP TERMINAL VELOCITY VECTOR IN METERS/CENTISEC
050640,000160: # * +5 FOR MOON *
050641,000161: # TC * +28 * DP TRANSFER TIME IN CENTISECS TO WHICH KEPLER CONVERGED. ALWAYS LESS THAN ONE PERIOD.
050642,000162: # XPREV * +17 FOR EARTH * DP VALUE OF X IN SQRT(METERS) TO WHCIH KEPLER CONVERGED. ALWAYS LESS THAN THE X
050643,000163: # * +16 FOR MOON * CORRESPONDING TO ONE PERIOD.
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Page 1162 |
050645,000165: # FOR OTHER OUTPUT WHICH MAY BE OF USE, SEE DEBRIS.
050646,000166:
050647,000167: # DEBRIS -
050648,000168: # PARAMETERS WHICH MAY BE OF USE -
050649,000169: # * SCALE FACTOR *
050650,000170: # VARIABLE *IN POWERS OF 2 * DESCRIPTION AND REMARKS
050651,000171: # -------- *-------------- * -----------------------
050652,000172: # URRECT * +1 * DP UNIT VECTOR OF INITIAL POSITION
050653,000173: # R1 * +29 FOR EARTH * DP MAGNITUDE OF INITIAL POSITION IN METERS
050654,000174: # * +27 FOR MOON *
050655,000175: # ALPHA * -22 FOR EARTH * DP INVERSE OF SEMIMAJOR AXIS IN 1/METERS
050656,000176: # * -20 FOR MOON *
050657,000177: # TMODULO * +28 * DP INTEGRAL NUMBER OF PERIODS IN CENTISECS. WHICH WAS SUBTRACTED FROM TAU. TO PRODUCE A
050658,000178: # * * TAU. OF LESS THAN ONE PERIOD.
050659,000179:
050660,000180: # PARAMETERS OF NO USE -
050661,000181: # DP PARAMETERS - EPSILONT, DELX, DELT, RCNORM, XMODULO, PLUS PUSHLIST REGISTERS 0 THROUGH 39D.
050662,000182:
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Page 1163 |
050664,000184:
050665,000185: # PROGRAM DESCRIPTION - LAMBERT SUBROUTINE DATE - 1 SEPTEMBER 1967
050666,000186: # MOD NO. - 0 LOG SECTION - CONIC SUBROUTINES
050667,000187: # MOD BY KRAUSE ASSEMBLY - COLOSSUS REVISION 88
050668,000188:
050669,000189: # FUNCTIONAL DESCRIPTION -
050670,000190: # THIS SUBROUTINE CALCULATES THE INITIAL VELOCITY REQUIRED TO TRANSFER A POINT-MASS ALONG A CONIC TRAJECTORY
050671,000191: # FROM AN INITIAL POSITION TO A TERMINAL POSITION IN A PRESCRIBED TIME INTERVAL. THE RESULTING TRAJECTORY MAY BE
050672,000192: # A SECTION OF A CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON. THE USE OF THE
050673,000193: # SUBROUTINE CAN BE EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY
050674,000194: # CODING CHANGES, ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY. AN ITERATION TECHNIQUE IS
050675,000195: # UTILIZED IN THE COMPUTATION.
050676,000196:
050677,000197: # THE RESTRICTIONS ARE -
050678,000198: # 1. RECTILINEAR TRAJECTORIES CANNOT BE COMPUTED.
050679,000199: # 2. AN ACCURACY DEGRADATION OCCURS AS THE COSINE OF THE TRUE ANOMALY DIFFERENCE APPROACHES +1.0.
050680,000200: # 3. THE ANGLE BETWEEN ANY POSITION VECTOR AND ITS VELOCITY VECTOR MUST BE GREATER THAN 1 DEGREE 47.5 MINUTES
050681,000201: # AND LESS THAN 178 DEGREES 12.5 MINUTES.
050682,000202: # 4. NEGATIVE TRANSFER TIME IS AMBIGUOUS AND WILL RESULT IN NO SOLUTION.
050683,000203: # 5. THE PARAMETERS IN THE PROBLEM MUST NOT EXCEED THEIR SCALING LIMITS SPECIFIED IN THE GSOP. IF THE
050684,000204: # LIMITS ARE EXCEEDED, THE RESULTING SOLUTION WILL BE MEANINGLESS.
050685,000205:
050686,000206: # THE NUMBER OF ITERATIONS AND, THEREFORE, THE COMPUTATIONS SPEED IS DEPENDENT ON THE ACCURACY OF THE FIRST
050687,000207: # GUESS OF THE INDEPENDENT VARIABLE, COGA. THE AGC COMPUTATION TIME IS APPROXIMATE-
050688,000208: # LY .105 SECONDS FOR INITIALIZATION, .069 SECONDS FOR FINAL COMPUTATIONS, PLUS .205 SECONDS FOR EACH ITERATION.
050689,000209:
050690,000210: # REFERENCES -
050691,000211: # R-479, MISSION PROGRAMMING DEFINITION MEMO NO. 10, LUNAR LANDING MISSION GSOP - SECTION 5.5, SGA MEMO 67-8,
050692,000212: # SGA MEMO 67-4.
050693,000213:
050694,000214: # INPUT - ERASABLE INITIALIZATION REQUIRED
050695,000215: #
050696,000216: # * SCALE FACTOR *
050697,000217: # VARIABLE *IN POWERS OF 2 * DESCRIPTION AND REMARKS
050698,000218: # -------- *-------------- * -----------------------
050699,000219: # R1VEC * +29 FOR EARTH * DP INITIAL POSITION VECTOR IN METERS
050700,000220: # * +27 FOR MOON *
050701,000221: # R2VEC * +29 FOR EARTH * DP TARGET OR TERMINAL POSITION VECTOR IN METERS
050702,000222: # * +27 FOR MOON *
050703,000223: # TDESIRED * +28 * DP DESIRED TRANSFER TIME IN CENTISECONDS
050704,000224: # X1 (38D) * NONE * INDEX REGISTER SET TO -2D OR -10D ACCORDING TO WHETHER THE EARTH OR MOON,
050705,000225: # * * RESPECTIVELY, IS THE CENTRAL BODY
050706,000226: # GEOMSGN * NONE * SP +.5 IF DESIRED TRANSFER ANGLE IS LESS THAN 180 DEGREES, -.5 IF GREATER THAN 180 DEG.
050707,000227: # 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 1164 |
050709,000229: # * * COGA IS TO BE USED BY LAMBERT
050710,000230: # COGA * +5 * DP GUESS OF COTANGNT OF FLIGHT PATH ANGLE (MEASURED FROM VERTICAL). THIS WILL BE
050711,000231: # * IGNORED IF GUESSW IS SET.
050712,000232: # NORMSW * NONE * AN INTERPRETER SWITCH TO BE SET IF UN IS TO BE AN INPUT TO THE SUBROUTINE, CLEAR IF
050713,000233: # * * LAMBERT IS TO COMPUTE ITS OWN NORMAL (UN).
050714,000234: # UN * +1 * DP UNIT NORMAL TO THE DESIRED ORBIT PLANE IN THE DIRECTION OF THE RESULTING ANGULAR
050715,000235: # * * MOMENTUM VECTOR. THIS WILL BE IGNORED IF NORMSW IS CLEAR.
050716,000236: # VTARGTAG * NONE * A S.P. TAG TO BE SET TO ZERO IF LAMBERT IS TO COMPUTE THE VELOCITY AT R2VEC AS WELL AS
050717,000237: # * * AT R1VEC.
050718,000238: # ITERCTR * NONE * A S.P. COUNTER WHICH SPECIFIES THE MAXIMUM NUMBER OF ITERATIONS ALLOWABLE.
050719,000239: # * * (AN ITERATION MEANS A PASS THRU KEPLER EQN (DELTIME). AT LEAST ONE OF THESE MUST
050720,000240: # * * ALWAYS OCCUR, EVEN IF COGA CORRESPONDING TO SOLUTION WERE INPUT AS A GUESS.)
050721,000241: # * * TWENTY ITERATIONS ARE SUFFICIENT TO SOLVE ALL PROBLEMS INCLUDING THOSE WITHOUT GUESS.
050722,000242:
050723,000243: # SUBROUTINES CALLED -
050724,000244: # GEOM, GETX, DELTIME, ITERATOR, LAMENTER (PART OF NEWSTATE)
050725,000245:
050726,000246: # CALLING SEQUENCE AND NORMAL EXIT MODES -
050727,000247: # L CALL MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
050728,000248: # L+1 LAMBERT RETURNS WITH PL AT 0 AND WITH VVEC IN MPAC IF VTARGTAG WAS NON-ZERO OR VTARGET
050729,000249: # IN MPAC IF VTARGTAG WAS ZERO
050730,000250: # L+2 BON CONTINUE IF SOLNSW CLEAR SINCE SOLUTION IS ACCEPTABLE
050731,000251: # L+3 SOLNSW
050732,000252: # L+4 LAMABORT
050733,000253:
050734,000254: # IF A LAMBERT RESULT IS TO BE A FIRST GUESS FOR THE NEXT LAMBERT CALCULATION, COGA MUST BE PRESERVED AND
050735,000255: # GUESSW MUST BE CLEAR FOR EACH SUCCEEDING LAMBERT CALL.
050736,000256:
050737,000257: # ABORT EXIT MODES -
050738,000258: # IF SOLNSW WAS SET UPON EXITING, EITHER LAMBERT WAS ASKED TO COMPUTE A TRANSFER TOO NEAR 0 OR 360 DEG, OR T
050739,000259: # WAS TOO SMALL TO PRODUCE A REALISTIC TRANSFER BETWEEN R1VEC AND R2VEC. IN EITHER CASE THE FIX MUST BE MADE
050740,000260: # ACCORDING TO THE NEEDS OF THE PARTICULAR USER. THE ABORT EXIT MODE MAY BE CODED AS ...
050741,000261: # LAMABORT DLOAD ABS A MEASURE OF PROXIMITY TO 0 OR
050742,000262: # 1-CSTH 360 DEGREES.
050743,000263: # DSU BMN
050744,000264: # ONEBIT
050745,000265: # CHANGER2 CHANGE R2VEC DIRECTION SLIGHTLY.
050746,000266: # DLOAD DAD
050747,000267: # TDESIRED
050748,000268: # SOMETIME
050749,000269: # STCALL TDESIRED INCREASE TDESIRED
050750,000270: # LAMBERT
050751,000271:
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Page 1165 |
050753,000273: # OUTPUT -
050754,000274: # * SCALE FACTOR *
050755,000275: # VARIABLE *IN POWERS OF 2 * DESCRIPTION AND REMARKS
050756,000276: # -------- *-------------- * -----------------------
050757,000277: # VVEC * +7 FOR EARTH * DP INITIAL VELOCITY VECTOR IN METERS/CENTISECOND REQUIRED TO SATISFY THE BOUNDARY VALUE
050758,000278: # * +5 FOR MOON * PROBLEM.
050759,000279: # VTARGET * +7 FOR EARTH * DP RESULTANT VELOCITY VECTOR AT R2VEC IN METERS/CENTISECOND.
050760,000280: # * +5 FOR MOON *
050761,000281: # SOLNSW * NONE * INTERPRETER SWITCH WHICH IS SET IF THE SUBROUTINE CANNOT SOLVE THE PROBLEM, CLEAR IF THE
050762,000282: # * * SOLUTION EXISTS.
050763,000283:
050764,000284: # FOR OTHER OUTPUT WHICH MAY BE OF USE, SEE DEBRIS.
050765,000285:
050766,000286: # DEBRIS -
050767,000287: # PARAMETERS WHICH MAY BE OF USE -
050768,000288:
050769,000289: # * SCALE FACTOR *
050770,000290: # VARIABLE *IN POWERS OF 2 * DESCRIPTION AND REMARKS
050771,000291: # -------- *-------------- * -----------------------
050772,000292: # SNTH * +1 * DP SIN OF ANGLE BETWEEN R1VEC AND R2VEC
050773,000293: # CSTH * +1 * DP COSINE OF ANGLE
050774,000294: # 1-CSTH * +2 * DP 1-CSTH
050775,000295: # COGA * +5 * DP COTAN OF INITIAL REQUIRED FLIGHT PATH ANGLE MEASURED FROM VERTICAL
050776,000296: # P * +4 * DP RATIO OF SEMILATUS RECTUM TO INITIAL RADIUS
050777,000297: # R1A * +6 * DP RATIO OF INITIAL RADIUS TO SEMIMAJOR AXIS
050778,000298: # R1 (32D) * +29 FOR EARTH * DP INITIAL RADIUS IN METERS
050779,000299: # * +27 FOR MOON *
050780,000300: # UR1 * +1 * DP UNIT VECTOR OF R1VEC
050781,000301: # U2 * +1 * DP UNIT VECTOR OF R2VEC
050782,000302:
050783,000303: # PARAMETERS OF NO USE
050784,000304: # DP PARAMETERS - EPSILONL, CSTH-RHO, TPREV, TERRLAMB, R2, RTNLAMB (SP), PLUS PUSHLIST REGISTER 0 THROUGH 41D
050785,000305: # ADDITIONAL INTERPRETIVE SWITCHES USED - INFINFLG, 360SW, SLOPESW, ORDERSW
050786,000306:
|
|
Page 1166 |
050788,000308: # PROGRAM DESCRIPTION - TIME-THETA SUBROUTINE DATE - 1 SEPTEMBER 1967
050789,000309: # MOD NO. - 0 LOG SECTION - CONIC SUBROUTINES
050790,000310: # MOD BY KRAUSE ASSEMBLY - COLOSSUS REVISION 88
050791,000311:
050792,000312: # FUNCTIONAL DESCRIPTION -
050793,000313: # THIS SUBROUTINE, GIVEN AN INITIAL STATE VECTOR AND A DESIRED TRUE-ANOMALY-DIFFERENCE THROUGH WHICH THE
050794,000314: # STATE IS TO BE UPDATED ALONG A CONIC TRAJECTORY, CALCULATES THE CORRESPONDING TIME-OF-FLIGHT AND, IN ADDITION,
050795,000315: # PROVIDES THE OPTION OF COMPUTING THE NEW UPDATED STATE VECTOR. THE RESULTING TRAJECTORY MAY BE A SECTION OF A
050796,000316: # CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON. THE USE OF THE SUBROUTINE CAN BE
050797,000317: # EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY CODING CHANGES,
050798,000318: # ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY.
050799,000319:
050800,000320: # THE RESTRICTIONS ARE -
050801,000321: # 1. THE ANGLE BETWEEN ANY POSITION VECTOR AND ITS VELOCITY VECTOR MUST BE GREATER THAN 1 DEGREE 47.5 MINUTES
050802,000322: # AND LESS THAN 178 DEGREES 12.5 MINUTES.
050803,000323: # 2. THE PARAMETERS IN THE PROBLEM MUST NOT EXCEED THEIR SCALING LIMITS SPECIFIED IN THE GSOP. IF THE LIMITS
050804,000324: # ARE EXCEEDED, THE RESULTING SOLUTION WILL BE MEANINGLESS.
050805,000325:
050806,000326: # THE AGC COMPUTATION TIME IS APPROXIMATELY .292 SECONDS.
050807,000327:
050808,000328: # REFERENCES -
050809,000329: # R-479, MISSION PROGRAMMING DEFINITION MEMO NO. 10, LUNAR LANDING MISSION GSOP-SECTION 5.5, SGA MEMO 67-8.
050810,000330:
050811,000331: # INPUT - ERASABLE INITIALIZATION REQUIRED
050812,000332: # * SCALE FACTOR *
050813,000333: # VARIABLE *IN POWERS OF 2 * DESCRIPTION AND REMARKS
050814,000334: # -------- *-------------- * -----------------------
050815,000335: # RVEC * +29 FOR EARTH * DP INITIAL POSITION VECTOR IN METERS
050816,000336: # * +27 FOR MOON *
050817,000337: # VVEC * +7 FOR EARTH * DP INITIAL VELOCITY VECTOR IN METERS/CENTISECOND
050818,000338: # * +5 FOR MOON *
050819,000339: # SNTH * +1 * DP SINE OF TRUE-ANOMALY-DIFFERENCE THROUGH WHICH THE STATE IS TO BE UPDATED
050820,000340: # CSTH * +1 * DP COSINE OF THE ANGLE
050821,000341: # RVSW * NONE * AN INTERPRETIVE SWITCH TO BE SET IF ONLY TIME IS TO BE AN OUTPUT, CLEAR IF THE NEW STATE
050822,000342: # * * IS TO BE COMPUTED ALSO.
050823,000343: # X1 (38D) * NONE * INDEX REGISTER TO BE SET TO -2D OR -10D ACCORDING TO WHETHER THE EARTH OR MOON,
050824,000344: # * * RESPECTIVELY, IS THE CENTRAL BODY.
050825,000345:
050826,000346: # SUBROUTINES CALLED -
|
|
Page 1167 |
050828,000348: # PARAM, GEOM, GETX, DELTIME, NEWSTATE
050829,000349:
050830,000350: # CALLING SEQUENCE AND NORMAL EXIT MODES -
050831,000351: # IF ONLY TIME IS DESIRED AS OUTPUT -
050832,000352: # L SET CALL MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
050833,000353: # L+1 RVSW
050834,000354: # L+2 TIMETHET RETURN WITH PL AT 0 AND T IN MPAC
050835,000355: # L+3 ... CONTINUE
050836,000356:
050837,000357: # IF THE UPDATE STATE VECTOR IS DESIRED AS WELL -
050838,000358: # L CLEAR CALL MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
050839,000359: # L+1 RVSW
050840,000360: # L+2 TIMETHET RETURNS WITH PL AT 6. THE INITIAL POSITION VECTOR IS IN 0D OF THE PUSHLIST AND
050841,000361: # THE INITIAL VELOCITY VECTOR IN MPAC.
050842,000362: # L+3 STOVL NEWVVEC
050843,000363: # L+4 STADR
050844,000364: # L+5 STORE NEWRVEC NEWVVEC AND NEWRVEC ARE SYMBOLIC REPRESENTATIONS OF THE USERS LOCATIONS.
050845,000365: # L+6 ... CONTINUE
050846,000366:
050847,000367: # ABORT EXIT MODES -
050848,000368: # IF COGAFLAG AND/OR INFINFLG IS SET AT THE EXIT TO TIME-THETA, TIME-THETA WILL TRANSFER TO POODOO WITH
050849,000369: # AN ALARM CODE (ORIGINALLY 00607), AND NOT RETURN TO THE CALLING PROGRAM. (PCR 692 AND 721).
050850,000370:
050851,000371: # OUTPUT -
050852,000372: # * SCALE FACTOR *
050853,000373: # VARIABLE *IN POWERS OF 2 * DESCRIPTION AND REMARKS
050854,000374: # -------- *-------------- * -----------------------
050855,000375: # T (30D) * +28 * DP TRANSFER TIME IN CENTISECONDS
050856,000376: # INFINFLG * NONE * AN INTERPRETIVE SWITCH WHICH IS SET IF THE TRANSFER ANGLE REQUIRES CLOSURE THROUGH
050857,000377: # * * INFINITY (NO SOLUTION), CLEAR IF A PHYSICAL SOLUTION IS POSSIBLE.
050858,000378: # COGAFLAG * NONE * AN INTERPRETIVE SWITCH WHICH IS SET IF RESTRICTION 1 HAS BEEN VIOLATED (NO SOLUTION),
050859,000379: # * * CLEAR IF NOT.
050860,000380:
050861,000381: # IN ADDITION, IF RVSW IS CLEAR, THE FOLLOWING ARE OUTPUT -
050862,000382: # MPAC - * +7 FOR EARTH * DP TERMINAL VELOCITY VECTOR IN METERS/CENTISEC.
050863,000383: # MPAC +5 * +5 FOR MOON *
050864,000384: # 0D - 5D * +29 FOR EARTH * DP TERMINAL POSITION VECTOR IN METERS (PL AT 6D)
050865,000385: # * +27 FOR MOON *
050866,000386:
050867,000387: # FOR OTHER OUTPUT WHICH MAY BE OF USE, SEE DEBRIS.
050868,000388:
|
|
Page 1168 |
050870,000390: # DEBRIS -
050871,000391: # PARAMETERS WHICH MAY BE OF USE -
050872,000392: #
050873,000393: # * SCALE FACTOR *
050874,000394: # VARIABLE *IN POWERS OF 2 * DESCRIPTION AND REMARKS
050875,000395: # -------- *-------------- * -----------------------
050876,000396: # R1 (32D) * +29 FOR EARTH * DP MAGNITUDE OF INITIAL POSITION VECTOR, RVEC, IN METERS
050877,000397: # * +27 FOR MOON *
050878,000398: # R1A * +6 * DP RATIO OF R1 TO SEMIMAJOR AXIS (NEG. FOR HYPERBOLIC TRAJECTORIES)
050879,000399: # P * +4 * DP RATIO OF SEMILATUS RECTUM TO R1
050880,000400: # COGA * +5 * DP COTAN OF ANGLE BETWEEN RVEC AND VVEC
050881,000401: # UR1 * +1 * DP UNIT VECTOR OF RVEC
050882,000402: # U2 * +1 * DP UNIT VECTOR OF VVEC
050883,000403: # UN * +1 * DP UNIT VECTOR OF UR1*U2
050884,000404:
050885,000405: # PARAMETERS OF NO USE -
050886,000406: # SP PARAMETERS - RTNTT, GEOMSGN, RTNPRM, MAGVEC2=R2 (DP), PLUS PUSHLIST LOCATIONS 0-11D, 14D-21D, 24D-39D, 41D
050887,000407: # ADDITIONAL INTERPRETIVE SWITCHES USED - NORMSW, 360SW
050888,000408:
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|
Page 1169 |
050890,000410: # PROGRAM DESCRIPTION - TIME-RADIUS SUBROUTINE DATE - 11 OCTOBER 1967
050891,000411: # MOD NO. -1 LOG SECTION - CONIC SUBROUTINES
050892,000412: # MOD BY KRAUSE ASSEMBLY - COLOSSUS REVISION 88
050893,000413:
050894,000414: # FUNCTIONAL DESCRIPTION -
050895,000415:
050896,000416: # THIS SUBROUTINE, GIVEN AN INITIAL STATE VECTOR AND A DESIRED RADIUS TO WHICH THE
050897,000417: # STATE IS TO BE UPDATED ALONG A CONIC TRAJECTORY, CALCULATES THE CORRESPONDING TIME-OF-FLIGHT AND, IN ADDITION,
050898,000418: # PROVIDES THE OPTION OF COMPUTING THE NEW UPDATED STATE VECTOR. THE RESULTING TRAJECTORY MAY BE A SECTION OF A
050899,000419: # CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON. THE USE OF THE SUBROUTINE CAN BE
050900,000420: # EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY CODING CHANGES,
050901,000421: # ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY.
050902,000422:
050903,000423: # IF THE DESIRED RADIUS IS BEYOND THE RADIUS OF APOCENTER OF THE CONIC OR BELOW THE RADIUS OF PERICENTER,
050904,000424: # APSESW WILL BE SET AND THE SUBROUTINE WILL RETURN THE APOCENTER OR PERICENTER SOLUTION, RESPECTIVELY.
050905,000425:
050906,000426: # THE RESTRICTIONS ARE -
050907,000427: # 1. THE ANGLE BETWEEN ANY POSITION VECTOR AND ITS VELOCITY VECTOR MUST BE GREATER THAN 1 DEGREE 47.5 MINUTES
050908,000428: # AND LESS THAN 178 DEGREES 12.5 MINUTES.
050909,000429: # 2. THE PARAMETERS IN THE PROBLEM MUST NOT EXCEED THEIR SCALING LIMITS SPECIFIED IN THE GSOP. IF THE LIMITS
050910,000430: # ARE EXCEEDED, THE RESULTING SOLUTION WILL BE MEANINGLESS.
050911,000431: # 3. AN ACCURACY DEGRADATION OCCURS AS THE SENSITIVITIES OF TIME AND UPDATED STATE VECTOR TO CHANGES IN
050912,000432: # RDESIRED INCREASE. THIS WILL OCCUR NEAR EITHER APSIS OF THE CONIC AND WHEN THE CONIC IS NEARLY CIRCULAR. IN
050913,000433: # PARTICULAR, IF THE CONIC IS AN EXACT CIRCLE, THE PROBLEM IS UNDEFINED AND THE SUBROUTINE WILL ABORT.
050914,000434:
050915,000435: # THE AGC COMPUTATION TIME IS APPROXIMATELY .363 SECONDS
050916,000436:
050917,000437: # REFERENCES -
050918,000438: # R-479, MISSION PROGRAMMING DEFINITION MEMO NO. 10, LUNAR LANDING MISSION GSOP-SECTION 5.5, SGA MEMO 67-8.
050919,000439:
050920,000440: # INPUT - ERASABLE INITIALIZATION REQUIRED
050921,000441: # * SCALE FACTOR *
050922,000442: # VARIABLE *IN POWERS OF 2 * DESCRIPTION AND REMARKS
050923,000443: # -------- *-------------- * -----------------------
050924,000444: # RVEC * +29 FOR EARTH * DP INITIAL POSITION VECTOR IN METERS
050925,000445: # * +27 FOR MOON *
050926,000446: # VVEC * +7 FOR EARTH * DP INITIAL VELOCITY VECTOR IN METERS/CENTISECOND
050927,000447: # * +5 FOR MOON *
050928,000448: # RDESIRED * +29 FOR EARTH * DP TERMINAL RADIAL DISTANCE ON CONIC TRAJECTORY FOR WHICH TRANSFER TIME IS TO BE
050929,000449: # * +27 FOR MOON * COMPUTED.
050930,000450: # SGNRDOT * NONE * SP TAG SET TO +.5 OR -.5 ACCORDING TO WHETHER THE RADIAL VELOCITY AT RDESIRED IS TO BE
050931,000451: # * * POSITIVE OR NEGATIVE, RESPECTIVELY. THIS TAG REDUCES THE DOUBLE-VALUED PROBLEM TO A
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|
Page 1170 |
050933,000453: # * * SINGLE-VALUED PROBLEM.
050934,000454: # X1 (38D) * NONE * INDEX REGISTER TO BE SET TO -2D OR -10D ACCORDING TO WHETHER THE EARTH OR MOON,
050935,000455: # * * RESPECTIVELY, IS THE CENTRAL BODY.
050936,000456: # RVSW * NONE * AN INTERPRETIVE SWITCH TO BE SET IF ONLY TIME IS TO BE AN OUTPUT, CLEAR IF THE NEW STATE
050937,000457: # * * IS TO BE COMPUTED ALSO.
050938,000458:
050939,000459: # SUBROUTINES CALLED -
050940,000460: # PARAM, GEOM, GETX, DELTIME, NEWSTATE
050941,000461:
050942,000462: # CALLING SEQUENCE AND NORMAL EXIT MODES -
050943,000463:
050944,000464: # IF ONLY TIME IS DESIRED AS OUTPUT -
050945,000465: # L SET CALL MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
050946,000466: # L+1 RVSW
050947,000467: # L+2 TIMERAD RETURN WITH PL AT 0 AND T IN MPAC
050948,000468: # L+3 ... CONTINUE
050949,000469:
050950,000470: # IF THE UPDATE STATE VECTOR IS DESIRED AS WELL -
050951,000471: # L CLEAR CALL MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
050952,000472: # L+1 RVSW
050953,000473: # L+2 TIMERAD RETURNS WITH PL AT 6. THE INITIAL POSITION VECTOR IS IN 0D OF THE PUSHLIST AND
050954,000474: # THE INITIAL VELOCITY VECTOR IN MPAC.
050955,000475: # L+3 STOVL NEWVVEC
050956,000476: # L+4 STADR
050957,000477: # L+5 STORE NEWRVEC NEWVVEC AND NEWRVEC ARE SYMBOLIC REPRESENTATIONS OF THE USERS LOCATIONS.
050958,000478: # L+6 ... CONTINUE
050959,000479:
050960,000480: # ABORT EXIT MODES -
050961,000481: # IF SOLNSW AND/OR COGAFLAG AND/OR INFINFLG IS SET AT THE EXIT TO TIME-RADIUS, TIME-RADIUS WILL TRANSFER
050962,000482: # TO POODOO WITH AN ALARM CODE (ORIGINALLY 00607), AND NOT RETURN TO THE CALLING PROGRAM. (PCR 692 & 721)
050963,000483:
050964,000484: # OUTPUT -
050965,000485: # * SCALE FACTOR *
050966,000486: # VARIABLE *IN POWERS OF 2 * DESCRIPTION AND REMARKS
050967,000487: # -------- *-------------- * -----------------------
050968,000488: # T (30D) * +28 * DP TRANSFER TIME IN CENTISECONDS
050969,000489: # INFINFLG * NONE * AN INTERPRETIVE SWITCH WHICH IS SET IF RDESIRED AND SGNRDOT REQUIRE CLOSURE THROUGH
050970,000490: # * * INFINITY (NO SOLUTION), CLEAR IF A PHYSICAL SOLUTION IS POSSIBLE.
050971,000491: # COGAFLAG * NONE * AN INTERPRETIVE SWITCH WHICH IS SET IF RESTRICTION 1 HAS BEEN VIOLATED (NO SOLUTION),
050972,000492: # * * CLEAR IF NOT.
050973,000493: # APSESW * NONE * AN INTERPRETIVE SWITCH WHICH IS SET IF RDESIRED WAS GREATER THAN RADIUS OF APOCENTER OR
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|
Page 1171 |
050975,000495: # * * LESS THAN RADIUS OF PERICENTER. THE APOCENTER OR PERICENTER SOLUTION, RESPECTIVELY,
050976,000496: # * * WILL THEN BE RETURNED. THE SWITCH IS CLEAR IF RDESIRED WAS BETWEEN PERICENTER AND
050977,000497: # * * APOCENTER.
050978,000498: # SOLNSW * NONE * AN INTERPRETIVE SWITCH WHICH IS SET IF THE CONIC IS SO CLOSE TO A CIRCLE THAT THE TERMIN
050979,000499: # * POINT IS AMBIGUOUS, VIOLATING RESTRICTION 3. IF ECCENTRICITY IS GREATER THAN 2-TO-THE-
050980,000500: # * MINUS-18, THE SWITCH IS CLEAR.
050981,000501:
050982,000502: # IN ADDITION, IF RVSW IS CLEAR, THE FOLLOWING ARE OUTPUT -
050983,000503:
050984,000504: # MPAC - * +7 FOR EARTH * DP TERMINAL VELOCITY VECTOR IN METERS/CENTISEC.
050985,000505: # MPAC +5 * +5 FOR MOON *
050986,000506: # 0D - 5D * +29 FOR EARTH * DP TERMINAL POSITION VECTOR IN METERS (PL AT 6D)
050987,000507: # * +27 FOR MOON *
050988,000508:
050989,000509: # FOR OTHER OUTPUT WHICH MAY BE OF USE, SEE DEBRIS.
050990,000510:
050991,000511: # DEBRIS -
050992,000512: # PARAMETERS WHICH MAY BE OF USE -
050993,000513:
050994,000514: # * SCALE FACTOR *
050995,000515: # VARIABLE *IN POWERS OF 2 * DESCRIPTION AND REMARKS
050996,000516: # -------- *-------------- * -----------------------
050997,000517: # R1 (32D) * +29 FOR EARTH * DP MAGNITUDE OF INITIAL POSITION VECTOR, RVEC, IN METERS
050998,000518: # * +27 FOR MOON *
050999,000519: # R1A * +6 * DP RATIO OF R1 TO SEMIMAJOR AXIS (NEG. FOR HYPERBOLIC TRAJECTORIES)
051000,000520: # P * +4 * DP RATIO OF SEMILATUS RECTUM TO R1
051001,000521: # COGA * +5 * DP COTAN OF ANGLE BETWEEN RVEC AND VVEC
051002,000522: # UR1 * +1 * DP UNIT VECTOR OF RVEC
051003,000523: # U2 * +1 * DP UNIT VECTOR OF VVEC
051004,000524: # UN * +1 * DP UNIT VECTOR OF UR1*U2
051005,000525: # CSTH * +1 * DP COSINE OF TRUE ANOMALY DIFFERENCE BETWEEN RVEC AND RDESIRED.
051006,000526: # SNTH * +1 * DP SINE OF TRUE ANOMALY DIFFERENCE.
051007,000527:
051008,000528: # PARAMETERS OF NO USE -
051009,000529: # SP PARAMETERS - RTNTT, GEOMSGN, RTNPRM, MAGVEC2=R2 (DP), PLUS PUSHLIST LOCATIONS 0-11D, 14D-21D, 24D-39D, 41D
051010,000530: # ADDITIONAL INTERPRETIVE SWITCHES USED - NORMSW, 360SW
051011,000531:
051012,000532:
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|
Page 1172 |
051014,000534: # PROGRAM DESCRIPTION - APSIDES SUBROUTINE DATE - 1 SEPTEMBER 1967
051015,000535: # MOD NO. - 0 LOG SECTION - CONIC SUBROUTINES
051016,000536: # MOD BY KRAUSE ASSEMBLY - COLOSSUS REVISION 88
051017,000537:
051018,000538: # FUNCTIONAL DESCRIPTION -
051019,000539:
051020,000540: # THIS SUBROUTINE, GIVEN AN INITIAL STATE VECTOR CALCULATES THE RADIUS OF PERICENTER AND OF APOCENTER AND THE
051021,000541: # ECCENTRICITY OF THE RESULTING CONIC TRAJECTORY, WHICH MAY BE A STRAIGHT LINE,
051022,000542: # CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON. THE USE OF THE SUBROUTINE CAN BE
051023,000543: # EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY CODING CHANGES,
051024,000544: # ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY.
051025,000545:
051026,000546: # THE RESTRICTIONS ARE -
051027,000547: # 1. IF APOCENTER IS BEYOND THE SCALING OF POSITION, THE SCALE FACTOR LIMIT (536,870,910 METERS WITH RESPECT
051028,000548: # TO THE EARTH OR 134,217,727.5 METERS WITH RESPECT TO THE MOON) WILL BE RETURNED.
051029,000549: # 2. THE PARAMETERS IN THE PROBLEM MUST NOT EXCEED THEIR SCALING LIMITS SPECIFIED IN THE GSOP. IF THE LIMITS
051030,000550: # ARE EXCEEDED, THE RESULTING SOLUTION WILL BE MEANINGLESS.
051031,000551:
051032,000552: # THE AGC COMPUTATION TIME IS APPROXIMATELY .103 SECONDS.
051033,000553:
051034,000554: # REFERENCES -
051035,000555: # MISSION PROGRAMMING DEFINITION MEMO NO. 10, LUNAR LANDING MISSION GSOP-SECTION 5.5
051036,000556:
051037,000557: # INPUT - ERASABLE INITIALIZATION REQUIRED
051038,000558: # * SCALE FACTOR *
051039,000559: # VARIABLE *IN POWERS OF 2 * DESCRIPTION AND REMARKS
051040,000560: # -------- *-------------- * -----------------------
051041,000561: # RVEC * +29 FOR EARTH * DP INITIAL POSITION VECTOR IN METERS
051042,000562: # * +27 FOR MOON *
051043,000563: # VVEC * +7 FOR EARTH * DP INITIAL VELOCITY VECTOR IN METERS/CENTISECOND
051044,000564: # * +5 FOR MOON *
051045,000565: # X1 (38D) * NONE * INDEX REGISTER TO BE SET TO -2D OR -10D ACCORDING TO WHETHER THE EARTH OR MOON,
051046,000566: # * * RESPECTIVELY, IS THE CENTRAL BODY.
051047,000567:
051048,000568: # SUBROUTINES CALLED -
051049,000569: # PARAM, GEOM
051050,000570:
051051,000571: # CALLING SEQUENCE AND NORMAL EXIT MODES -
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|
Page 1173 |
051053,000573: # IF ONLY TIME IS DESIRED AS OUTPUT -
051054,000574: # L CALL MUST BE IN INTERPRETIVE MODE BUT OVFIND ARBITRARY.
051055,000575: # L+1 APSIDES RETURNS WITH PL AT 0, RADIUS OF APOCENTER IN MPAC AND RADIUS OF PERICENTER IN 0D
051056,000576: # L+2 STODL APOAPSE
051057,000577: # L+3 0D
051058,000578: # L+4 STORE PERIAPSE APOAPSE AND PERIAPSE ARE SYMBOLIC REPRESENTATIONS OF THE USERS LOCATIONS
051059,000579: # L+5 ... CONTINUE
051060,000580:
051061,000581: # OUTPUT -
051062,000582: # * SCALE FACTOR *
051063,000583: # VARIABLE *IN POWERS OF 2 * DESCRIPTION AND REMARKS
051064,000584: # -------- *-------------- * -----------------------
051065,000585: # MPAC * +29 FOR EARTH * DP RADIUS OF APOCENTER IN METERS
051066,000586: # * +27 FOR MOON *
051067,000587: # 0D-1D * +29 FOR EARTH * DP RADIUS OF PERICENTER IN METERS
051068,000588: # * +27 FOR MOON *
051069,000589: # ECC * +3 * DP ECCENTRICITY OF CONIC TRAJECTORY.
051070,000590:
051071,000591: # FOR OTHER OUTPUT WHICH MAY BE OF USE, SEE DEBRIS.
051072,000592:
051073,000593: # DEBRIS -
051074,000594:
051075,000595: # PARAMETERS WHICH MAY BE OF USE -
051076,000596:
051077,000597: # * SCALE FACTOR *
051078,000598: # VARIABLE *IN POWERS OF 2 * DESCRIPTION AND REMARKS
051079,000599: # -------- *-------------- * -----------------------
051080,000600: # R1 (32D) * +29 FOR EARTH * DP MAGNITUDE OF INITIAL POSITION VECTOR, RVEC, IN METERS
051081,000601: # * +27 FOR MOON *
051082,000602: # R1A * +6 * DP RATIO OF R1 TO SEMIMAJOR AXIS (NEG. FOR HYPERBOLIC TRAJECTORIES)
051083,000603: # P * +4 * DP RATIO OF SEMILATUS RECTUM TO R1
051084,000604: # COGA * +5 * DP COTAN OF ANGLE BETWEEN RVEC AND VVEC
051085,000605: # UR1 * +1 * DP UNIT VECTOR OF RVEC
051086,000606: # U2 * +1 * DP UNIT VECTOR OF VVEC
051087,000607: # UN * +1 * DP UNIT VECTOR OF UR1*U2
051088,000608: # MAGVEC2 * +7 FOR EARTH * DP MAGNITUDE OF VVEC
051089,000609: # * +5 FOR MOON *
051090,000610:
051091,000611: # PARAMETERS OF NO USE -
051092,000612: # SP PARAMETERS - RTNAPSE, GEOMSGN, RTNPRM, PLUS PUSHLIST LOCATIONS 0-5, 10D-11D, 14D-21D, 31D-38D.
051093,000613: # ADDITIONAL INTERPRETIVE SWITCHES USED - NORMSW
051094,000614:
051095,000615: 12,2000 SETLOC CONICS
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|
Page 1174 |
051097,000617: 12,2000 BANK
051098,000618:
051099,000619: 12,2023 COUNT* $$/CONIC
051100,000620: 12,2023 E5,1721 EBANK= UR1
051101,000621: 12,2023 40001 KEPLERN SETPD BOV
051102,000622: 12,2024 00001 0
051103,000623: 12,2025 24026 +1
051104,000624: 12,2026 77773 VLOAD*
051105,000625: 12,2027 10005 MUTABLE,1
051106,000626: 12,2030 24017 STOVL 14D
051107,000627: 12,2031 01503 RRECT
051108,000628: 12,2032 66256 UNIT SSP
051109,000629: 12,2033 00027 ITERCTR
051110,000630: 12,2034 00024 20D
051111,000631: 12,2035 16647 STODL URRECT
051112,000632: 12,2036 00045 36D
051113,000633: 12,2037 24041 STOVL R1
051114,000634: 12,2040 01503 RRECT
051115,000635: 12,2041 76441 DOT SL1R
051116,000636: 12,2042 01511 VRECT
051117,000637: 12,2043 76405 DMP SL1R
051118,000638: 12,2044 00023 1/ROOTMU # 1/ROOTMU (-17 OR -14)
051119,000639: 12,2045 24043 STOVL KEPC1 # C1=R.V/ROOTMU (+17 OR +16)
051120,000640: 12,2046 01511 VRECT
051121,000641: 12,2047 57236 VSQ DMPR
051122,000642: 12,2050 00017 1/MU # 1/MU (-34 OR -28)
051123,000643: 12,2051 52405 DMP SL3
051124,000644: 12,2052 00041 R1
051125,000645: 12,2053 61425 DSU ROUND
051126,000646: 12,2054 11035 D1/64
051127,000647: 12,2055 00045 STORE KEPC2 # C2=RV.V/MU -1 (+6)
051128,000648:
051129,000649: 12,2056 74421 BDSU SR1R
051130,000650: 12,2057 11035 D1/64
051131,000651: 12,2060 77671 DDV
051132,000652: 12,2061 00041 R1
051133,000653: 12,2062 00011 STORE ALPHA # ALPHA=(1-C2)/R1 (-22 OR -20)
051134,000654:
051135,000655: 12,2063 71244 BPL DLOAD # MAXIMUM X DEPENDS ON TYPE OF CONIC
051136,000656: 12,2064 24073 1REV
051137,000657: 12,2065 11053 -50SC # -50SC (+12)
051138,000658: 12,2066 40071 DDV BOV
051139,000659: 12,2067 00011 ALPHA
051140,000660: 12,2070 24077 STOREMAX
051141,000661: 12,2071 52166 SQRT GOTO
051142,000662: 12,2072 24077 STOREMAX
051143,000663:
051144,000664: 12,2073 55366 1REV SQRT BDDV
|
|
Page 1175 |
051146,000666: 12,2074 11055 2PISC # 2PISC (+6)
051147,000667: 12,2075 77600 BOV
051148,000668: 12,2076 24077 STOREMAX
051149,000669: 12,2077 00013 STOREMAX STORE XMAX
051150,000670: 12,2100 65205 DMP PDDL
051151,000671: 12,2101 00023 1/ROOTMU
051152,000672: 12,2102 00011 ALPHA
051153,000673: 12,2103 65301 NORM PDDL
051154,000674: 12,2104 00047 X1
051155,000675: 12,2105 56257 SL* DDV
051156,000676: 12,2106 20173 0 -6,1
051157,000677: 12,2107 50000 BOV BMN
051158,000678: 12,2110 24124 MODDONE
051159,000679: 12,2111 24124 MODDONE # MPAC=PERIOD
051160,000680: 12,2112 51525 PERIODCH PDDL ABS # 0D=PERIOD
051161,000681: 12,2113 02074 TAU.
051162,000682: 12,2114 50025 DSU BMN
051163,000683: 12,2115 00001 0D
051164,000684: 12,2116 24124 MODDONE
051165,000685: 12,2117 77765 SIGN
051166,000686: 12,2120 02074 TAU.
051167,000687: 12,2121 16074 STODL TAU.
051168,000688: 12,2122 77650 GOTO
051169,000689: 12,2123 24112 PERIODCH
051170,000690: 12,2124 71201 MODDONE SETPD DLOAD
051171,000691: 12,2125 00001 0
051172,000692: 12,2126 02130 XKEPNEW
051173,000693: 12,2127 00025 STORE X
051174,000694: 12,2130 53165 SIGN BZE
051175,000695: 12,2131 02074 TAU.
051176,000696: 12,2132 24302 BADX
051177,000697: 12,2133 51440 BMN ABS
051178,000698: 12,2134 24302 BADX
051179,000699: 12,2135 51025 DSU BPL
051180,000700: 12,2136 00013 XMAX
051181,000701: 12,2137 24302 BADX
051182,000702: 12,2140 51145 STORBNDS DLOAD BPL
051183,000703: 12,2141 02074 TAU.
051184,000704: 12,2142 24152 STOREMIN
051185,000705: 12,2143 57545 DLOAD DCOMP
051186,000706: 12,2144 00013 XMAX
051187,000707: 12,2145 14015 STODL XMIN
051188,000708: 12,2146 24007 KEPZERO
051189,000709: 12,2147 00013 STORE XMAX
051190,000710: 12,2150 77650 GOTO
051191,000711: 12,2151 24155 DXCOMP
051192,000712: 12,2152 77745 STOREMIN DLOAD
051193,000713: 12,2153 24007 KEPZERO
051194,000714: 12,2154 00015 STORE XMIN
051195,000715: 12,2155 57345 DXCOMP DLOAD DMPR
|
|
Page 1176 |
051197,000717: 12,2156 02074 TAU.
051198,000718: 12,2157 11046 BEE22
051199,000719: 12,2160 77646 ABS
051200,000720: 12,2161 16177 STODL EPSILONT
051201,000721: 12,2162 01553 XPREV
051202,000722: 12,2163 77621 XDIFF BDSU
051203,000723: 12,2164 00025 X
051204,000724: 12,2165 02643 STORE DELX
051205,000725:
051206,000726: 12,2166 63545 KEPLOOP DLOAD DSQ
051207,000727: 12,2167 00025 X # X=XKEP
051208,000728: 12,2170 41501 NORM PUSH # 0D=XSQ (+34 OR +32 -N1) PL AT 2
051209,000729: 12,2171 00047 X1
051210,000730: 12,2172 53605 DMP SRR*
051211,000731: 12,2173 00011 ALPHA
051212,000732: 12,2174 21573 0 -6,1
051213,000733: 12,2175 34031 STCALL XI # XI=ALPHA XSQ (+6)
051214,000734: 12,2176 24421 DELTIME
051215,000735: 12,2177 44200 BOV BDSU
051216,000736: 12,2200 24311 TIMEOVFL # UNLIKELY
051217,000737: 12,2201 02074 TAU.
051218,000738: 12,2202 02645 STORE DELT # DELT=DELINDEP
051219,000739: 12,2203 44246 ABS BDSU
051220,000740: 12,2204 02177 EPSILONT
051221,000741: 12,2205 71244 BPL DLOAD
051222,000742: 12,2206 24333 KEPCONVG
051223,000743: 12,2207 00037 T
051224,000744: 12,2210 60225 DSU NORM
051225,000745: 12,2211 01551 TC
051226,000746: 12,2212 00047 X1
051227,000747: 12,2213 60325 PDDL NORM
051228,000748: 12,2214 02643 DELX
051229,000749: 12,2215 00050 X2
051230,000750: 12,2216 41260 XSU,1 DMP
051231,000751: 12,2217 00047 X2
051232,000752: 12,2220 02645 DELT
051233,000753: 12,2221 56257 SLR* DDV
051234,000754: 12,2222 21202 1,1
051235,000755: 12,2223 41542 SR1 PUSH # 0D=TRIAL DELX PL AT 2
051236,000756: 12,2224 71244 BPL DLOAD
051237,000757: 12,2225 24246 POSDELX
051238,000758: 12,2226 00025 X
051239,000759: 12,2227 00013 STORE XMAX # MOVE MAX BOUND IN
051240,000760: 12,2230 45221 BDSU DSU # PL AT 0
051241,000761: 12,2231 00015 XMIN
051242,000762: 12,2232 51000 BOV BPL
051243,000763: 12,2233 24240 NDXCHNGE
051244,000764: 12,2234 24240 NDXCHNGE
051245,000765: 12,2235 52145 DLOAD GOTO
|
|
Page 1177 |
051247,000767: 12,2236 00001 0D
051248,000768: 12,2237 24260 NEWDELX
051249,000769:
051250,000770: 12,2240 45345 NDXCHNGE DLOAD DSU
051251,000771: 12,2241 00015 XMIN
051252,000772: 12,2242 00025 X
051253,000773: 12,2243 52075 DMPR GOTO # TO FORCE MPAC +2 TO ZERO
051254,000774: 12,2244 11051 DP9/10
051255,000775: 12,2245 24260 NEWDELX
051256,000776:
051257,000777: 12,2246 77745 POSDELX DLOAD
051258,000778: 12,2247 00025 X
051259,000779: 12,2250 00015 STORE XMIN # MOVE MIN BOUND IN
051260,000780: 12,2251 45221 BDSU DSU # PL AT 0
051261,000781: 12,2252 00013 XMAX
051262,000782: 12,2253 50000 BOV BMN
051263,000783: 12,2254 24274 PDXCHNGE
051264,000784: 12,2255 24274 PDXCHNGE
051265,000785: 12,2256 77745 DLOAD
051266,000786: 12,2257 00001 0D
051267,000787: 12,2260 02643 NEWDELX STORE DELX
051268,000788: 12,2261 43254 BZE DAD
051269,000789: 12,2262 24333 KEPCONVG
051270,000790: 12,2263 00025 X
051271,000791: 12,2264 14025 STODL X
051272,000792: 12,2265 00037 T
051273,000793: 12,2266 01551 STORE TC
051274,000794: 12,2267 46034 BRNCHCTR RTB BHIZ
051275,000795: 12,2270 24644 CHECKCTR
051276,000796: 12,2271 24333 KEPCONVG
051277,000797: 12,2272 77650 GOTO
051278,000798: 12,2273 24166 KEPLOOP # ITERATE
051279,000799:
051280,000800: 12,2274 45345 PDXCHNGE DLOAD DSU
051281,000801: 12,2275 00013 XMAX
051282,000802: 12,2276 00025 X
051283,000803: 12,2277 52075 DMPR GOTO # TO FORCE MPAC +2 TO ZERO
051284,000804: 12,2300 11051 DP9/10
051285,000805: 12,2301 24260 NEWDELX
051286,000806:
051287,000807: 12,2302 70545 BADX DLOAD SR1
051288,000808: 12,2303 00013 XMAX
051289,000809: 12,2304 77765 SIGN
051290,000810: 12,2305 02074 TAU.
051291,000811: 12,2306 00025 STORE X
051292,000812: 12,2307 77650 GOTO
|
|
Page 1178 |
051294,000814: 12,2310 24140 STORBNDS
051295,000815: 12,2311 50145 TIMEOVFL DLOAD BMN # X WAS TOO BIG
051296,000816: 12,2312 00025 X
051297,000817: 12,2313 24330 NEGTOVFL
051298,000818: 12,2314 00013 STORE XMAX
051299,000819: 12,2315 70545 CMNTOVFL DLOAD SR1
051300,000820: 12,2316 02643 DELX
051301,000821: 12,2317 02643 STORE DELX
051302,000822: 12,2320 44254 BZE BDSU
051303,000823: 12,2321 02112 KEPRTN
051304,000824: 12,2322 00025 X
051305,000825: 12,2323 14025 STODL X
051306,000826: 12,2324 01551 TC
051307,000827: 12,2325 00037 STORE T
051308,000828: 12,2326 77650 GOTO
051309,000829: 12,2327 24267 BRNCHCTR
051310,000830: 12,2330 00015 NEGTOVFL STORE XMIN
051311,000831: 12,2331 77650 GOTO
051312,000832: 12,2332 24315 CMNTOVFL
051313,000833: 12,2333 44545 KEPCONVG DLOAD SR4R
051314,000834: 12,2334 00041 R1
051315,000835: 12,2335 74225 DSU VXSC
051316,000836: 12,2336 00035 XSQC(XI)
051317,000837: 12,2337 02647 URRECT
051318,000838: 12,2340 65372 VSL1 PDDL # 0D=(R1-XSQC(XI))URRECT (+33 OR +31)
051319,000839: 12,2341 00025 X
051320,000840: 12,2342 60316 DSQ NORM
051321,000841: 12,2343 00047 X1
051322,000842: 12,2344 57275 DMPR DMPR
051323,000843: 12,2345 00023 1/ROOTMU
051324,000844: 12,2346 00025 X
051325,000845: 12,2347 53605 DMP SRR*
051326,000846: 12,2350 00033 S(XI)
051327,000847: 12,2351 21572 0 -7,1
051328,000848: 12,2352 77621 BDSU
051329,000849: 12,2353 00037 T
051330,000850: 12,2354 74352 SL1 VXSC
051331,000851: 12,2355 01511 VRECT
051332,000852: 12,2356 53372 VSL1 VAD # PL AT 0
051333,000853: 12,2357 77712 VSL4
051334,000854: 12,2360 01535 STORE RCV # RCV (+29 OR +27)
051335,000855:
051336,000856: 12,2361 60246 ABVAL NORM
051337,000857: 12,2362 00050 X2
051338,000858: 12,2363 14043 STODL RCNORM
051339,000859: 12,2364 00031 XI
051340,000860: 12,2365 45275 DMPR DSU
051341,000861: 12,2366 00033 S(XI)
051342,000862: 12,2367 11033 D1/128
|
|
Page 1179 |
051344,000864: 12,2370 76405 DMP SL1R
051345,000865: 12,2371 00021 ROOTMU
051346,000866: 12,2372 53605 DMP SLR*
051347,000867: 12,2373 00025 X
051348,000868: 12,2374 56601 0 -3,2
051349,000869: 12,2375 74271 DDV VXSC
051350,000870: 12,2376 00043 RCNORM
051351,000871: 12,2377 02647 URRECT
051352,000872: 12,2400 65372 VSL1 PDDL # 0D=URRECT(XI S(XI)-1)X ROOTMU/RCV (+15
051353,000873: 12,2401 00035 XSQC(XI) # OR +13) PL AT 6
051354,000874: 12,2402 56257 SLR* DDV
051355,000875: 12,2403 56602 0 -4,2
051356,000876: 12,2404 00043 RCNORM
051357,000877: 12,2405 74221 BDSU VXSC
051358,000878: 12,2406 11047 D1/256
051359,000879: 12,2407 01511 VRECT
051360,000880: 12,2410 42455 VAD VSL8
051361,000881: 12,2411 77626 STADR # PL AT 0
051362,000882: 12,2412 62234 STODL VCV # VCV (+7 OR +5)
051363,000883: 12,2413 00037 T
051364,000884: 12,2414 15551 STODL TC
051365,000885: 12,2415 00025 X
051366,000886: 12,2416 01553 STORE XPREV
051367,000887: 12,2417 77650 GOTO
051368,000888: 12,2420 02112 KEPRTN
051369,000889:
|
|
Page 1180 |
051371,000891: 12,2421 77776 DELTIME EXIT # MPAC=XI (+6), 0D=XSQ (+34 OR +32 -N1)
051372,000892: 12,2422 07222 TC POLY
051373,000893: 12,2423 00010 DEC 8 B-14
051374,000894: 12,2424 02525 12526 2DEC .083333334
051375,000895: 12,2426 67356 75666 2DEC -.266666684
051376,000896: 12,2430 15001 23771 2DEC .406349155
051377,000897: 12,2432 64342 43674 2DEC -.361198675
051378,000898: 12,2434 06563 04645 2DEC .210153242
051379,000899: 12,2436 75173 52672 2DEC -.086221951
051380,000900: 12,2440 00656 14331 2DEC .026268812
051381,000901: 12,2442 77633 40512 2DEC -.006163316
051382,000902: 12,2444 00023 11210 2DEC .001177342
051383,000903: 12,2446 77774 67506 2DEC -.000199055
051384,000904:
051385,000905: 12,2450 06037 TC INTPRET
051386,000906: 12,2451 14033 STODL S(XI)
051387,000907: 12,2452 00031 XI
051388,000908: 12,2453 77776 EXIT
051389,000909: 12,2454 07222 TC POLY
051390,000910: 12,2455 00010 DEC 8 B-14
051391,000911: 12,2456 01000 00000 2DEC .031250001
051392,000912: 12,2460 72525 52506 2DEC -.166666719
051393,000913: 12,2462 13301 15337 2DEC .355555413
051394,000914: 12,2464 62776 54733 2DEC -.406347410
051395,000915: 12,2466 11176 13267 2DEC .288962094
051396,000916: 12,2470 73410 51674 2DEC -.140117894
051397,000917: 12,2472 01446 33641 2DEC .049247387
051398,000918: 12,2474 77451 65233 2DEC -.013081923
051399,000919: 12,2476 00055 37266 2DEC .002806389
051400,000920: 12,2500 77767 52336 2DEC -.000529414
051401,000921: 12,2502 06037 TC INTPRET
|
|
Page 1181 |
051403,000923: 12,2503 53605 DMP SRR* # PL AT 0
051404,000924: 12,2504 00001 0D
051405,000925: 12,2505 21574 0 -5,1
051406,000926: 12,2506 00035 STORE XSQC(XI) # XSQC(XI) (+33 OR +31)
051407,000927: 12,2507 72405 DMP SL1
051408,000928: 12,2510 00043 KEPC1
051409,000929: 12,2511 65234 RTB PDDL # XCH WITH PL. 0D=C1 XSQ C(XI) (+49 OR +46
051410,000930: 12,2512 21633 TPMODE # PL AT 0,3
051411,000931: 12,2513 53605 DMP SRR*
051412,000932: 12,2514 00033 S(XI)
051413,000933: 12,2515 21574 0 -5,1
051414,000934: 12,2516 72405 DMP SL1
051415,000935: 12,2517 00045 KEPC2
051416,000936: 12,2520 65234 RTB PDDL # 3D=C2 XSQ S(XI) (+35 OR +33) PL AT 6
051417,000937: 12,2521 21633 TPMODE
051418,000938: 12,2522 00041 R1
051419,000939: 12,2523 76261 SR TAD # PL AT 3
051420,000940: 12,2524 20607 6
051421,000941: 12,2525 41301 NORM DMP # TO PRESERVE SIGNIF.
051422,000942: 12,2526 00047 X1
051423,000943: 12,2527 00025 X
051424,000944: 12,2530 76257 SR* TAD # X(C2 XSQ S(XI) +R1) (+49 OR +46) PL AT 0
051425,000945: 12,2531 20576 0 -3,1
051426,000946: 12,2532 57232 SL4R DMPR
051427,000947: 12,2533 00023 1/ROOTMU
051428,000948: 12,2534 00037 STORE T
051429,000949: 12,2535 77616 RVQ
051430,000950:
|
|
Page 1182 |
051432,000952: 12,2536 71214 ITERATOR BONCLR DLOAD
051433,000953: 12,2537 00614 SLOPESW
051434,000954: 12,2540 24606 FIRSTIME
051435,000955: 12,2541 00037 DEP
051436,000956: 12,2542 60225 DSU NORM
051437,000957: 12,2543 02762 DEPREV
051438,000958: 12,2544 00047 X1
051439,000959: 12,2545 60325 PDDL NORM
051440,000960: 12,2546 00015 DELINDEP
051441,000961: 12,2547 00050 X2
051442,000962: 12,2550 41260 XSU,1 DMP
051443,000963: 12,2551 00047 X2
051444,000964: 12,2552 02760 DELDEP
051445,000965: 12,2553 56257 SLR* DDV # PL UP 2
051446,000966: 12,2554 21202 1,1
051447,000967: 12,2555 43142 SR1 BOFF
051448,000968: 12,2556 04351 ORDERSW
051449,000969: 12,2557 24562 SGNCHECK
051450,000970: 12,2560 75246 ABS SIGN # IN CASE 2ND DERIV. CHANGED SIGN, MUST
051451,000971: 12,2561 02760 DELDEP # DISREGARD IT TO FIND MIN.
051452,000972:
051453,000973: 12,2562 51006 SGNCHECK PUSH BPL # TRIAL DELINDEP PL DOWN 2
051454,000974: 12,2563 24620 POSDEL
051455,000975: 12,2564 43145 DLOAD BON
051456,000976: 12,2565 02766 INDEP
051457,000977: 12,2566 04311 ORDERSW
051458,000978: 12,2567 24571 MINCHECK
051459,000979: 12,2570 00017 STORE MAX # IF NOT 2ND ORDER, CAN MOVE MAX BOUND IN.
051460,000980:
051461,000981: 12,2571 45221 MINCHECK BDSU DSU
051462,000982: 12,2572 00011 MIN
051463,000983: 12,2573 51000 BOV BPL
051464,000984: 12,2574 24600 MODNGDEL
051465,000985: 12,2575 24600 MODNGDEL
051466,000986: 12,2576 77650 GOTO
051467,000987: 12,2577 24632 DELOK
051468,000988:
051469,000989: 12,2600 45345 MODNGDEL DLOAD DSU # TRIAL DELINDEP WOULD EXCEED MIN BOUND
051470,000990: 12,2601 00011 MIN
051471,000991: 12,2602 02766 INDEP
051472,000992: 12,2603 52005 DMP GOTO
051473,000993: 12,2604 11051 DP9/10
051474,000994: 12,2605 24634 NEWDEL
051475,000995:
051476,000996: 12,2606 41345 FIRSTIME DLOAD DMP
051477,000997: 12,2607 00011 MIN
051478,000998: 12,2610 00051 TWEEKIT # DLOAD TWEEKIT(40D) SENSITIVE TO CHANGE.
051479,000999: 12,2611 41325 PDDL DMP # S2(41D) SHOULDNT CONTAIN HI ORDER ONES
|
|
Page 1183 |
051481,001001: 12,2612 00017 MAX
051482,001002: 12,2613 00051 TWEEKIT
051483,001003: 12,2614 77625 DSU
051484,001004: 12,2615 52165 SIGN GOTO
051485,001005: 12,2616 02760 DELDEP
051486,001006: 12,2617 24562 SGNCHECK
051487,001007:
051488,001008: 12,2620 43145 POSDEL DLOAD BON
051489,001009: 12,2621 02766 INDEP
051490,001010: 12,2622 04311 ORDERSW
051491,001011: 12,2623 24625 MAXCHECK
051492,001012: 12,2624 00011 STORE MIN # IF NOT 2ND ORDER, CAN MOVE MIN BOUND IN.
051493,001013:
051494,001014: 12,2625 45221 MAXCHECK BDSU DSU
051495,001015: 12,2626 00017 MAX
051496,001016: 12,2627 50000 BOV BMN
051497,001017: 12,2630 24636 MODPSDEL
051498,001018: 12,2631 24636 MODPSDEL
051499,001019: 12,2632 77745 DELOK DLOAD
051500,001020: 12,2633 00001 0D
051501,001021: 12,2634 00015 NEWDEL STORE DELINDEP
051502,001022: 12,2635 77616 RVQ
051503,001023:
051504,001024: 12,2636 45345 MODPSDEL DLOAD DSU
051505,001025: 12,2637 00017 MAX
051506,001026: 12,2640 02766 INDEP
051507,001027: 12,2641 52005 DMP GOTO
051508,001028: 12,2642 11051 DP9/10
051509,001029: 12,2643 24634 NEWDEL
051510,001030:
051511,001031: 12,2644 44753 CHECKCTR CS ONE
051512,001032: 12,2645 50120 INDEX FIXLOC
051513,001033: 12,2646 60026 AD ITERCTR
051514,001034: 12,2647 50120 INDEX FIXLOC
051515,001035: 12,2650 54026 TS ITERCTR
051516,001036: 12,2651 54154 TS MPAC
051517,001037: 12,2652 06061 TC DANZIG
051518,001038:
|
|
Page 1184 |
051520,001040: 12,2653 44545 NEWSTATE DLOAD SR4R
051521,001041: 12,2654 00041 R1
051522,001042: 12,2655 74225 DSU VXSC
051523,001043: 12,2656 00035 XSQC(XI)
051524,001044: 12,2657 02722 UR1
051525,001045: 12,2660 65372 VSL1 PDDL # 0D=(R1-XSQC(XI))UR1 (+33 OR 31) PL AT 6
051526,001046: 12,2661 00025 X
051527,001047: 12,2662 60316 DSQ NORM
051528,001048: 12,2663 00047 X1
051529,001049: 12,2664 57275 DMPR DMPR
051530,001050: 12,2665 00023 1/ROOTMU
051531,001051: 12,2666 00025 X
051532,001052: 12,2667 53605 DMP SRR*
051533,001053: 12,2670 00033 S(XI)
051534,001054: 12,2671 21572 0 -7,1
051535,001055: 12,2672 77621 BDSU
051536,001056: 12,2673 00037 T
051537,001057: 12,2674 74352 SL1 VXSC
051538,001058: 12,2675 02744 VVEC
051539,001059: 12,2676 53372 VSL1 VAD # PL AT 0
051540,001060: 12,2677 41512 VSL4 PUSH
051541,001061: 12,2700 77646 ABVAL
051542,001062: 12,2701 77701 LAMENTER NORM
051543,001063: 12,2702 00047 X1
051544,001064: 12,2703 16720 STODL R2
051545,001065: 12,2704 00031 XI
051546,001066: 12,2705 45205 DMP DSU
051547,001067: 12,2706 00033 S(XI)
051548,001068: 12,2707 11033 D1/128
051549,001069: 12,2710 76405 DMP SL1R
051550,001070: 12,2711 00021 ROOTMU
051551,001071: 12,2712 53605 DMP SLR*
051552,001072: 12,2713 00025 X
051553,001073: 12,2714 21176 0 -3,1
051554,001074: 12,2715 74271 DDV VXSC
051555,001075: 12,2716 02720 R2
051556,001076: 12,2717 02722 UR1
051557,001077: 12,2720 65372 VSL1 PDDL # 6D=V2VEC PART (+15 OR 13) PL AT 12
051558,001078: 12,2721 00035 XSQC(XI)
051559,001079: 12,2722 56257 SLR* DDV
051560,001080: 12,2723 21175 0 -4,1
051561,001081: 12,2724 02720 R2
051562,001082: 12,2725 77621 BDSU
051563,001083: 12,2726 11047 D1/256
051564,001084: 12,2727 53361 VXSC VAD # PL AT 6
051565,001085: 12,2730 02744 VVEC
051566,001086: 12,2731 43412 VSL8 RVQ
051567,001087:
|
|
Page 1185 |
051569,001089: 04,2000 SETLOC CONICS1
051570,001090: 04,2000 BANK
051571,001091:
051572,001092: 04,3027 COUNT* $$/CONIC
051573,001093: # DO NOT DISTURB THE ORDER OF THESE CDS, OVERLAYS HAVE BEEN MADE.
051574,001094: 04,3027 00000 BEE17 DEC 0 B-14 # KEEP WITH D1/8 2DEC 1.0B-17 (0000004000)
051575,001095: 04,3030 04000 00000 D1/8 2DEC 1.0 B-3
051576,001096: 04,3032 00200 00000 D1/128 2DEC 1.0 B-7
051577,001097: 04,3034 00400 00000 D1/64 2DEC 1.0 B-6
051578,001098: 04,3036 10000 00000 D1/4 2DEC 1.0 B-2
051579,001099: 04,3040 02000 00000 D1/16 2DEC 1.0 B-4
051580,001100: 04,3042 01000 00000 D1/32 2DEC 1.0 B-5
051581,001101: 04,3044 00020 00000 D1/1024 2DEC 1.0 B-10
051582,001102: 04,3046 00100 00000 D1/256 2DEC 1.0 B-8
051583,001103: 04,3050 34631 23146 DP9/10 2DEC .9
051584,001104: 04,3052 12,2006 KEPZERO EQUALS LO6ZEROS
051585,001105: 04,3052 77467 77777 -50SC 2DEC -50.0 B-12
051586,001106: 04,3054 03110 17665 2PISC 2DEC 6.28318530 B-6
051587,001107: 04,3056 04,3041 BEE19 EQUALS D1/32 -1 # 2DEC 1.0 B-19 (00000 01000)
051588,001108: 04,3056 04,3045 BEE22 EQUALS D1/256 -1 # 2DEC 1.0 B-22 (00000 00100)
051589,001109: 04,3056 00000 00001 ONEBIT 2DEC 1.0 B-28
051590,001110: 04,3060 37767 37737 COGUPLIM 2DEC .999511597
051591,001111: 04,3062 40010 40040 COGLOLIM 2DEC -.999511597
051592,001112:
|
|
Page 1186 |
051594,001114: 12,2000 SETLOC CONICS
051595,001115: 12,2000 BANK
051596,001116:
051597,001117: 12,2732 COUNT* $$/CONIC
051598,001118: 12,2732 40220 TIMETHET STQ SETPD # PL AT 0
051599,001119: 12,2733 02710 RTNTT
051600,001120: 12,2734 00001 0
051601,001121: 12,2735 77600 BOV
051602,001122: 12,2736 24737 +1
051603,001123: 12,2737 63375 VLOAD PDVL # SETUP FOR PARAM CALL PL AT 6
051604,001124: 12,2740 02655 RVEC
051605,001125: 12,2741 02744 VVEC
051606,001126: 12,2742 77624 CALL
051607,001127: 12,2743 11064 PARAM
051608,001128: 12,2744 45000 BOV CALL # PL AT 0
051609,001129: 12,2745 24764 COGAOVFL
051610,001130: 12,2746 24767 GETX
051611,001131: 12,2747 43145 COMMNOUT DLOAD BON
051612,001132: 12,2750 00031 XI
051613,001133: 12,2751 04310 INFINFLG
051614,001134: 12,2752 25742 ABTCONIC
051615,001135: 12,2753 45014 CLEAR CALL
051616,001136: 12,2754 04273 COGAFLAG
051617,001137: 12,2755 24421 DELTIME
051618,001138: 12,2756 45014 BON CALL
051619,001139: 12,2757 03706 RVSW
051620,001140: 12,2760 02710 RTNTT
051621,001141: 12,2761 24653 NEWSTATE
051622,001142: 12,2762 77650 GOTO
051623,001143: 12,2763 02710 RTNTT
051624,001144:
051625,001145: 12,2764 77614 COGAOVFL SETGO
051626,001146: 12,2765 04033 COGAFLAG
051627,001147: 12,2766 25742 ABTCONIC
051628,001148:
051629,001149: 04,3064 BANK 4
051630,001150: 04,2000 SETLOC CONICS1
051631,001151: 04,2000 BANK
051632,001152: 04,3064 COUNT* $$/CONIC
051633,001153: 04,3064 43020 PARAM STQ CLEAR # MPAC=V1VEC, 0D=R1VEC PL AT 6
051634,001154: 04,3065 02753 RTNPRM
051635,001155: 04,3066 03665 NORMSW
051636,001156: 04,3067 77614 CLEAR
051637,001157: 04,3070 04273 COGAFLAG
051638,001158: 04,3071 45131 SSP CALL
051639,001159: 04,3072 02673 GEOMSGN
051640,001160: 04,3073 27777 37777 # GAMMA ALWAYS LESS THAN 180DEG
051641,001161: 04,3074 11130 GEOM # MPAC=SNGA (+1), 0D=CSGA (+1) PL AT 2
051642,001162: 04,3075 14045 STODL 36D # 36D=SIN GAMMA (+1) PL AT 0
051643,001163: 04,3076 56261 SR DDV
|
|
Page 1187 |
051645,001165: 04,3077 20606 5
051646,001166: 04,3100 00045 36D
051647,001167: 04,3101 32766 STOVL* COGA
051648,001168: 04,3102 10005 MUTABLE,1
051649,001169: 04,3103 14017 STODL 1/MU
051650,001170: 04,3104 02720 MAGVEC2
051651,001171: 04,3105 60316 DSQ NORM
051652,001172: 04,3106 00047 X1
051653,001173: 04,3107 41275 DMPR DMP
051654,001174: 04,3110 00017 1/MU
051655,001175: 04,3111 00041 R1
051656,001176: 04,3112 77657 SRR*
051657,001177: 04,3113 21576 0 -3,1
051658,001178: 04,3114 44206 PUSH BDSU # 0D=R1 V1SQ/MU (+6) PL AT 2
051659,001179: 04,3115 11043 D1/32
051660,001180: 04,3116 16742 STODL R1A # R1A (+6) PL AT 0
051661,001181:
051662,001182: 04,3117 60205 DMP NORM
051663,001183: 04,3120 00045 36D
051664,001184: 04,3121 00047 X1
051665,001185: 04,3122 53605 DMP SR*
051666,001186: 04,3123 00045 36D
051667,001187: 04,3124 20575 0 -4,1
051668,001188: 04,3125 02740 STORE P # P (+4)
051669,001189: 04,3126 77650 GOTO
051670,001190: 04,3127 02753 RTNPRM
051671,001191:
|
|
Page 1188 |
051673,001193: 04,3130 77656 GEOM UNIT # MPAC=V2VEC, 0D=R1VEC PL AT 6
051674,001194: 04,3131 16712 STODL U2 # U2 (+1)
051675,001195: 04,3132 00045 36D
051676,001196: 04,3133 26720 STOVL MAGVEC2 # PL AT 0
051677,001197: 04,3134 77656 UNIT
051678,001198: 04,3135 02722 STORE UR1 # UR1 (+1)
051679,001199: 04,3136 72441 DOT SL1
051680,001200: 04,3137 02712 U2
051681,001201: 04,3140 77725 PDDL # OD=CSTH (+1) PL AT 2
051682,001202: 04,3141 00045 36D
051683,001203: 04,3142 24041 STOVL R1 # R1 (+29 OR +27)
051684,001204: 04,3143 02722 UR1
051685,001205: 04,3144 76435 VXV VSL1
051686,001206: 04,3145 02712 U2
051687,001207: 04,3146 75214 BON SIGN
051688,001208: 04,3147 03705 NORMSW
051689,001209: 04,3150 11162 HAVENORM
051690,001210: 04,3151 02673 GEOMSGN
051691,001211: 04,3152 40056 UNIT BOV
051692,001212: 04,3153 11160 COLINEAR
051693,001213: 04,3154 16674 UNITNORM STODL UN # UN (+1)
051694,001214: 04,3155 00045 36D
051695,001215: 04,3156 43565 SIGN RVQ # MPAC=SNTH (+1), 34D=SNTH.SNTH (+2)
051696,001216: 04,3157 02673 GEOMSGN
051697,001217:
051698,001218: 04,3160 52162 COLINEAR VSR1 GOTO
051699,001219: 04,3161 11154 UNITNORM
051700,001220:
051701,001221: 04,3162 75246 HAVENORM ABVAL SIGN
051702,001222: 04,3163 02673 GEOMSGN
051703,001223: 04,3164 77616 RVQ # MPAC=SNTH (+1), 34D=SNTH.SNTH (+2)
051704,001224:
|
|
Page 1189 |
051706,001226: 12,2767 BANK 12
051707,001227: 12,2000 SETLOC CONICS
051708,001228: 12,2000 BANK
051709,001229:
051710,001230: 12,2767 COUNT* $$/CONIC
051711,001231: 12,2767 66374 GETX AXT,2 SSP # ASSUMES P (+4) IN MPAC
051712,001232: 12,2770 00003 3
051713,001233: 12,2771 00052 S2
051714,001234: 12,2772 00001 1
051715,001235: 12,2773 77614 CLEAR
051716,001236: 12,2774 04276 360SW
051717,001237: 12,2775 65366 SQRT PDDL # 0D=SQRT(P) PL AT 2
051718,001238: 12,2776 02732 CSTH
051719,001239: 12,2777 44342 SR1 BDSU
051720,001240: 12,3000 11037 D1/4
051721,001241: 12,3001 54325 PDDL SRR # PL AT 4D
051722,001242: 12,3002 02730 SNTH
051723,001243: 12,3003 21607 6
051724,001244: 12,3004 77671 DDV # PL AT 2
051725,001245: 12,3005 77600 BOV
051726,001246: 12,3006 25122 360CHECK
051727,001247: 12,3007 41225 DSU DMP
051728,001248: 12,3010 02766 COGA # PL AT 0
051729,001249: 12,3011 40132 SL2R BOV
051730,001250: 12,3012 25122 360CHECK
051731,001251: 12,3013 63406 WLOOP PUSH DSQ # 0D=W (+5) PL AT 2
051732,001252: 12,3014 65351 TLOAD PDDL # 2D=WSQ (+10) PL AT 5
051733,001253: 12,3015 00155 MPAC
051734,001254: 12,3016 02742 R1A
051735,001255: 12,3017 76202 SR4 TAD # PL AT 2
051736,001256: 12,3020 75440 BMN SQRT
051737,001257: 12,3021 25205 INFINITY
051738,001258: 12,3022 43306 ROUND DAD # PL AT 0D
051739,001259: 12,3023 61000 BOV TIX,2
051740,001260: 12,3024 25120 RESETX2
051741,001261: 12,3025 25013 WLOOP
051742,001262:
051743,001263: 12,3026 40065 BDDV BOV
051744,001264: 12,3027 11033 D1/128
051745,001265: 12,3030 25205 INFINITY
051746,001266: 12,3031 41440 POLYCOEF BMN PUSH # 0D=1/W (+2) OR 16/W (+6) PL AT 2
051747,001267: 12,3032 25205 INFINITY
051748,001268: 12,3033 77716 DSQ
051749,001269: 12,3034 41301 NORM DMP
051750,001270: 12,3035 00047 X1
051751,001271: 12,3036 02742 R1A
051752,001272: 12,3037 77457 SRR* EXIT
051753,001273: 12,3040 21567 0 -10D,1
051754,001274: 12,3041 07222 TC POLY
|
|
Page 1190 |
051756,001276: 12,3042 00005 DEC 5 B-14
051757,001277: 12,3043 20000 00000 2DEC .5
051758,001278: 12,3045 72525 52471 2DEC -.166666770
051759,001279: 12,3047 03146 15003 2DEC .100000392
051760,001280: 12,3051 75556 45210 2DEC -.071401086
051761,001281: 12,3053 01615 13553 2DEC .055503292
051762,001282: 12,3055 76371 63777 2DEC -.047264098
051763,001283: 12,3057 01232 27367 2DEC .040694204
051764,001284:
051765,001285: 12,3061 06037 TC INTPRET
051766,001286: 12,3062 76405 DMP SL1R # PL AT 0D
051767,001287: 12,3063 43006 PUSH BON
051768,001288: 12,3064 04316 360SW
051769,001289: 12,3065 25172 TRUE360X
051770,001290: 12,3066 60316 XCOMMON DSQ NORM
051771,001291: 12,3067 00047 X1
051772,001292: 12,3070 53605 DMP SRR*
051773,001293: 12,3071 02742 R1A
051774,001294: 12,3072 21565 0 -12D,1
051775,001295: 12,3073 14031 STODL XI # XI (+6)
051776,001296: 12,3074 00041 R1
051777,001297: 12,3075 75542 SR1 SQRT
051778,001298: 12,3076 41306 ROUND DMP
051779,001299: 12,3077 77632 SL4R # PL AT 0
051780,001300: 12,3100 00025 STORE X # X (+17 OR +16)
051781,001301:
051782,001302: 12,3101 60316 DSQ NORM
051783,001303: 12,3102 00047 X1
051784,001304: 12,3103 41325 PDDL DMP # 0D=XSQ (+34 OR +32 -N1) PL AT 2
051785,001305: 12,3104 02740 P
051786,001306: 12,3105 00041 R1
051787,001307: 12,3106 75452 SL3 SQRT
051788,001308: 12,3107 56405 DMP SL3R
051789,001309: 12,3110 02766 COGA
051790,001310: 12,3111 14043 STODL KEPC1
051791,001311: 12,3112 02742 R1A
051792,001312: 12,3113 43021 BDSU CLEAR
051793,001313: 12,3114 11035 D1/64
051794,001314: 12,3115 04270 INFINFLG
051795,001315: 12,3116 00045 STORE KEPC2
051796,001316: 12,3117 77616 RVQ
051797,001317:
|
|
Page 1191 |
051799,001319: 12,3120 77774 RESETX2 AXT,2
051800,001320: 12,3121 00003 3
051801,001321:
051802,001322: 12,3122 51001 360CHECK SETPD BPL
051803,001323: 12,3123 00001 0D
051804,001324: 12,3124 25127 INVRSEQN
051805,001325: 12,3125 77614 SET
051806,001326: 12,3126 04076 360SW
051807,001327:
051808,001328: 12,3127 75545 INVRSEQN DLOAD SQRT
051809,001329: 12,3130 02740 P
051810,001330: 12,3131 41325 PDDL DMP # 0D=SQRT(P) (+2) PL AT 2
051811,001331: 12,3132 02730 SNTH
051812,001332: 12,3133 02766 COGA
051813,001333: 12,3134 65352 SL1 PDDL # 2D=SNTH COGA (+5) PL AT 4
051814,001334: 12,3135 02732 CSTH
051815,001335: 12,3136 43202 SR4 DAD
051816,001336: 12,3137 11043 D1/32
051817,001337: 12,3140 41225 DSU DMP # PL AT 2,0
051818,001338: 12,3141 55301 NORM BDDV
051819,001339: 12,3142 00047 X1
051820,001340: 12,3143 02730 SNTH
051821,001341: 12,3144 51457 SLR* ABS # NOTE: NEAR 360 CASE TREATED DIFFERENTLY
051822,001342: 12,3145 21174 0 -5,1
051823,001343: 12,3146 63406 PUSH DSQ # 0D=1/W (-1) PL AT 2
051824,001344: 12,3147 14043 STODL 34D
051825,001345: 12,3150 11041 D1/16
051826,001346: 12,3151 63406 1/WLOOP PUSH DSQ # 2D=G (+4) PL AT 4
051827,001347: 12,3152 65234 RTB PDDL # PL AT 7
051828,001348: 12,3153 21633 TPMODE
051829,001349: 12,3154 02742 R1A
051830,001350: 12,3155 40405 DMP SR4
051831,001351: 12,3156 00043 34D
051832,001352: 12,3157 77771 TAD # PL AT 4
051833,001353: 12,3160 75440 BMN SQRT
051834,001354: 12,3161 25205 INFINITY
051835,001355: 12,3162 77615 DAD # PL AT 2
051836,001356: 12,3163 60304 TIX,2 NORM
051837,001357: 12,3164 25151 1/WLOOP
051838,001358: 12,3165 00047 X1
051839,001359: 12,3166 77665 BDDV
051840,001360: 12,3167 52057 SLR* GOTO # PL AT 0
051841,001361: 12,3170 21172 0 -7,1
051842,001362: 12,3171 25031 POLYCOEF
051843,001363:
051844,001364: 12,3172 50145 TRUE360X DLOAD BMN
051845,001365: 12,3173 02742 R1A
|
|
Page 1192 |
051847,001367: 12,3174 25205 INFINITY
051848,001368: 12,3175 60366 SQRT NORM
051849,001369: 12,3176 00047 X1
051850,001370: 12,3177 53665 BDDV SL*
051851,001371: 12,3200 11055 2PISC
051852,001372: 12,3201 20176 0 -3,1
051853,001373: 12,3202 41425 DSU PUSH # 0D=2PI/SQRT(R1A) -X PL AT 0,2
051854,001374: 12,3203 77650 GOTO
051855,001375: 12,3204 25066 XCOMMON
051856,001376: 12,3205 40001 INFINITY SETPD BOV # NO SOLUTION EXISTS SINCE CLOSURE THROUGH
051857,001377: 12,3206 00001 0 # INFINITY IS REQUIRED
051858,001378: 12,3207 25210 OVFLCLR
051859,001379: 12,3210 43414 OVFLCLR SET RVQ
051860,001380: 12,3211 04070 INFINFLG
051861,001381:
|
|
Page 1193 |
051863,001383: 12,3212 40220 LAMBERT STQ SETPD
051864,001384: 12,3213 02710 RTNLAMB
051865,001385: 12,3214 00001 0D
051866,001386: 12,3215 77600 BOV
051867,001387: 12,3216 25217 +1
051868,001388: 12,3217 76614 CLEAR VLOAD*
051869,001389: 12,3220 02674 SOLNSW
051870,001390: 12,3221 10005 MUTABLE,1
051871,001391: 12,3222 14017 STODL 1/MU
051872,001392: 12,3223 02671 TDESIRED
051873,001393: 12,3224 77675 DMPR
051874,001394: 12,3225 11042 BEE19
051875,001395: 12,3226 02764 STORE EPSILONL
051876,001396: 12,3227 77214 SET VLOAD
051877,001397: 12,3230 00474 SLOPESW
051878,001398: 12,3231 02655 R1VEC
051879,001399: 12,3232 45115 PDVL CALL # 0D=R1VEC (+29 OR +27) PL AT 6
051880,001400: 12,3233 02663 R2VEC # MPAC=R2VEC (+29 OR +27)
051881,001401: 12,3234 11130 GEOM
051882,001402: 12,3235 16730 STODL SNTH # 0D=CSTH (+1) PL AT 2
051883,001403: 12,3236 02720 MAGVEC2
051884,001404: 12,3237 65301 NORM PDDL # PL AT 4
051885,001405: 12,3240 00047 X1
051886,001406: 12,3241 00041 R1
051887,001407: 12,3242 56342 SR1 DDV # PL AT 2
051888,001408: 12,3243 65257 SL* PDDL # DXCH WITH 0D, 0D=R1/R2 (+7) PL AT 0,2
051889,001409: 12,3244 20173 0 -6,1
051890,001410: 12,3245 77626 STADR
051891,001411: 12,3246 75045 STORE CSTH # CSTH (+1)
051892,001412: 12,3247 44342 SR1 BDSU
051893,001413: 12,3250 11037 D1/4
051894,001414: 12,3251 02734 STORE 1-CSTH # 1-CSTH (+2)
051895,001415:
051896,001416: 12,3252 53106 ROUND BZE
051897,001417: 12,3253 25463 360LAMB
051898,001418: 12,3254 65301 NORM PDDL # PL AT 4
051899,001419: 12,3255 00047 X1
051900,001420: 12,3256 00001 0D
051901,001421: 12,3257 56342 SR1 DDV # PL AT 2
051902,001422: 12,3260 75457 SL* SQRT
051903,001423: 12,3261 20176 0 -3,1
051904,001424: 12,3262 54325 PDDL SR # 2D=SQRT(2R1/R2(1-CSTH)) (+5) PL AT 4
051905,001425: 12,3263 02730 SNTH
051906,001426: 12,3264 20607 6
051907,001427: 12,3265 43271 DDV DAD # PL AT 2
051908,001428: 12,3266 02734 1-CSTH
051909,001429: 12,3267 77626 STADR
051910,001430: 12,3270 77760 STORE COGAMAX
051911,001431: 12,3271 50000 BOV BMN # IF OVFL, COGAMAX=COGUPLIM
051912,001432: 12,3272 25277 UPLIM # IF NEG, USE EVEN IF LT COGLOLIM, SINCE
|
|
Page 1194 |
051914,001434: 12,3273 25302 MAXCOGA # THIS WOULD BE RESET IN LAMBLOOP
051915,001435: 12,3274 50025 DSU BMN # IF COGAMAX GT COGUPLIM, COGAMAX=COGUPLIM
051916,001436: 12,3275 11061 COGUPLIM
051917,001437: 12,3276 25302 MAXCOGA # OTHERWISE OK, SO GO TO MAXCOGA
051918,001438: 12,3277 77745 UPLIM DLOAD
051919,001439: 12,3300 11061 COGUPLIM # COGUPLIM=.999511597 = MAX VALUE OF COGA
051920,001440: 12,3301 00017 STORE COGAMAX # NOT CAUSING OVFL IN R1A CALCULATION
051921,001441: 12,3302 77745 MAXCOGA DLOAD
051922,001442: 12,3303 02732 CSTH
051923,001443: 12,3304 45261 SR DSU # PL AT 0
051924,001444: 12,3305 20607 6
051925,001445: 12,3306 77626 STADR
051926,001446: 12,3307 61041 STODL CSTH-RHO
051927,001447: 12,3310 02673 GEOMSGN
051928,001448: 12,3311 71240 BMN DLOAD
051929,001449: 12,3312 25503 LOLIM
051930,001450: 12,3313 02736 CSTH-RHO
051931,001451: 12,3314 56352 SL1 DDV
051932,001452: 12,3315 02730 SNTH
051933,001453: 12,3316 77600 BOV
051934,001454: 12,3317 25503 LOLIM
051935,001455: 12,3320 00011 MINCOGA STORE COGAMIN # COGAMIN (+5)
051936,001456: 12,3321 66214 BON SSP
051937,001457: 12,3322 00715 GUESSW
051938,001458: 12,3323 25467 NOGUESS
051939,001459: 12,3324 00051 TWEEKIT
051940,001460: 12,3325 00001 00001
051941,001461: 12,3326 77745 DLOAD
051942,001462: 12,3327 02766 COGA
051943,001463:
051944,001464: 12,3330 77605 LAMBLOOP DMP
051945,001465: 12,3331 02730 SNTH
051946,001466: 12,3332 45342 SR1 DSU
051947,001467: 12,3333 02736 CSTH-RHO
051948,001468: 12,3334 65301 NORM PDDL # 0D=SNTH COGA-(CSTH-RHO) (+7+C(X1)) PL=2
051949,001469: 12,3335 00047 X1
051950,001470: 12,3336 02734 1-CSTH
051951,001471: 12,3337 56257 SL* DDV # 1-CSTH (+2) PL AT 0
051952,001472: 12,3340 20170 0 -9D,1
051953,001473: 12,3341 53040 BMN BZE
051954,001474: 12,3342 25417 NEGP
051955,001475: 12,3343 25417 NEGP
051956,001476: 12,3344 16740 STODL P # P=(1-CSTH)/(SNTH COGA-(CSTH-RHO)) (+4)
051957,001477: 12,3345 02766 COGA
051958,001478: 12,3346 43316 DSQ DAD
051959,001479: 12,3347 11045 D1/1024
051960,001480: 12,3350 41301 NORM DMP
051961,001481: 12,3351 00047 X1
051962,001482: 12,3352 02740 P
|
|
Page 1195 |
051964,001484: 12,3353 44257 SR* BDSU
051965,001485: 12,3354 20571 0 -8D,1
051966,001486: 12,3355 11043 D1/32
051967,001487: 12,3356 16742 STODL R1A # R1A=2-P(1+COGA COGA) (+6)
051968,001488: 12,3357 02740 P
051969,001489: 12,3360 45000 BOV CALL
051970,001490: 12,3361 25422 HIENERGY
051971,001491: 12,3362 24767 GETX
051972,001492: 12,3363 77745 DLOAD
051973,001493: 12,3364 00037 T
051974,001494: 12,3365 16762 STODL TPREV
051975,001495: 12,3366 00031 XI
051976,001496: 12,3367 45014 BON CALL
051977,001497: 12,3370 04310 INFINFLG
051978,001498: 12,3371 25417 NEGP # HAVE EXCEEDED THEORETICAL BOUNDS
051979,001499: 12,3372 24421 DELTIME
051980,001500: 12,3373 44200 BOV BDSU
051981,001501: 12,3374 25437 BIGTIME
051982,001502: 12,3375 02671 TDESIRED
051983,001503: 12,3376 02760 STORE TERRLAMB
051984,001504: 12,3377 44246 ABS BDSU
051985,001505: 12,3400 02764 EPSILONL
051986,001506: 12,3401 47044 BPL RTB
051987,001507: 12,3402 25506 INITV
051988,001508: 12,3403 24644 CHECKCTR
051989,001509: 12,3404 45030 BHIZ CALL
051990,001510: 12,3405 25450 SUFFCHEK
051991,001511: 12,3406 24536 ITERATOR
051992,001512: 12,3407 53145 DLOAD BZE
051993,001513: 12,3410 00155 MPAC
051994,001514: 12,3411 25450 SUFFCHEK
051995,001515: 12,3412 77615 DAD
051996,001516: 12,3413 02766 COGA
051997,001517: 12,3414 02766 STORE COGA
051998,001518: 12,3415 77650 GOTO
051999,001519: 12,3416 25330 LAMBLOOP
052000,001520:
052001,001521: 12,3417 51145 NEGP DLOAD BPL # IMPOSSIBLE TRAJECTORY DUE TO INACCURATE
052002,001522: 12,3420 00015 DCOGA # BOUND CALCULATION. TRY NEW COGA.
052003,001523: 12,3421 25442 LOENERGY
052004,001524:
052005,001525: 12,3422 71201 HIENERGY SETPD DLOAD # HIGH ENERGY TRAJECTORY RESULTED
052006,001526: 12,3423 00001 0
052007,001527: 12,3424 02766 COGA # IN OVFL OF P OR R1A, OR XI EXCEEDING 50.
052008,001528: 12,3425 00011 STORE COGAMIN # THIS IS THE NEW BOUND.
052009,001529: 12,3426 70545 COMMONLM DLOAD SR1
052010,001530: 12,3427 00015 DCOGA
|
|
Page 1196 |
052012,001532: 12,3430 00015 STORE DCOGA # USE DCOGA/2 AS DECREMENT
052013,001533: 12,3431 44254 BZE BDSU
052014,001534: 12,3432 25450 SUFFCHEK
052015,001535: 12,3433 02766 COGA
052016,001536: 12,3434 02766 STORE COGA
052017,001537: 12,3435 77650 GOTO # RESTART THIS LOOP
052018,001538: 12,3436 25330 LAMBLOOP
052019,001539:
052020,001540: 12,3437 77745 BIGTIME DLOAD
052021,001541: 12,3440 02762 TPREV
052022,001542: 12,3441 00037 STORE T
052023,001543:
052024,001544: 12,3442 71201 LOENERGY SETPD DLOAD # LOW ENERGY TRAJECTORY RESULTED
052025,001545: 12,3443 00001 0
052026,001546: 12,3444 02766 COGA # IN OVERFLOW OF TIME.
052027,001547: 12,3445 00017 STORE COGAMAX # THIS IS THE NEW BOUND.
052028,001548: 12,3446 77650 GOTO
052029,001549: 12,3447 25426 COMMONLM
052030,001550:
052031,001551: 12,3450 51545 SUFFCHEK DLOAD ABS
052032,001552: 12,3451 02760 TERRLAMB
052033,001553: 12,3452 41325 PDDL DMP # PL AT 2D
052034,001554: 12,3453 02671 TDESIRED
052035,001555: 12,3454 11030 BEE17
052036,001556: 12,3455 45215 DAD DSU # PL AT 0D
052037,001557: 12,3456 11057 ONEBIT
052038,001558: 12,3457 43044 BPL SETGO
052039,001559: 12,3460 25506 INITV
052040,001560: 12,3461 02434 SOLNSW
052041,001561: 12,3462 25506 INITV
052042,001562: 12,3463 43001 360LAMB SETPD SETGO # LAMBERT CANNOT HANDLE CSTH=1
052043,001563: 12,3464 00001 0
052044,001564: 12,3465 02434 SOLNSW
052045,001565: 12,3466 02710 RTNLAMB
052046,001566:
052047,001567: 12,3467 71331 NOGUESS SSP DLOAD
052048,001568: 12,3470 00051 TWEEKIT
052049,001569: 12,3471 10000 20000
052050,001570: 12,3472 00011 COGAMIN
052051,001571: 12,3473 65342 SR1 PDDL # PL AT 2
052052,001572: 12,3474 00017 COGAMAX
052053,001573: 12,3475 43342 SR1 DAD
052054,001574: 12,3476 77626 STADR # PL AT 0
052055,001575: 12,3477 75011 STORE COGA
052056,001576: 12,3500 00015 STORE DCOGA
052057,001577: 12,3501 77650 GOTO
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|
Page 1197 |
052059,001579: 12,3502 25330 LAMBLOOP
052060,001580:
052061,001581: 12,3503 52145 LOLIM DLOAD GOTO
052062,001582: 12,3504 11063 COGLOLIM # COGLOLIM=-.999511597
052063,001583: 12,3505 25320 MINCOGA
052064,001584:
052065,001585: 12,3506 60345 INITV DLOAD NORM
052066,001586: 12,3507 00041 R1
052067,001587: 12,3510 00047 X1
052068,001588: 12,3511 70525 PDDL SR1 # PL AT 2
052069,001589: 12,3512 02740 P
052070,001590: 12,3513 77671 DDV # PL AT 0
052071,001591: 12,3514 75457 SL* SQRT
052072,001592: 12,3515 20175 0 -4,1
052073,001593: 12,3516 72405 DMP SL1
052074,001594: 12,3517 00021 ROOTMU
052075,001595: 12,3520 41206 PUSH DMP # 0D=VTAN (+7) PL AT 2
052076,001596: 12,3521 02766 COGA
052077,001597: 12,3522 74261 SL VXSC
052078,001598: 12,3523 20206 5
052079,001599: 12,3524 02722 UR1
052080,001600: 12,3525 77725 PDDL # XCH WITH 0D PL AT 0,6
052081,001601: 12,3526 76561 VXSC VSL1
052082,001602: 12,3527 02674 UN
052083,001603: 12,3530 53235 VXV VAD # PL AT 0
052084,001604: 12,3531 02722 UR1
052085,001605: 12,3532 77772 VSL1
052086,001606: 12,3533 02744 STORE VVEC
052087,001607: 12,3534 53135 SLOAD BZE
052088,001608: 12,3535 02702 VTARGTAG
052089,001609: 12,3536 25541 TARGETV
052090,001610: 12,3537 77650 GOTO
052091,001611: 12,3540 02710 RTNLAMB
052092,001612:
052093,001613: 12,3541 45145 TARGETV DLOAD CALL
052094,001614: 12,3542 02720 MAGVEC2
052095,001615: 12,3543 24701 LAMENTER
052096,001616: 12,3544 02703 STORE VTARGET
052097,001617: 12,3545 77650 GOTO
052098,001618: 12,3546 02710 RTNLAMB
052099,001619:
|
|
Page 1198 |
052101,001621: 12,3547 40220 TIMERAD STQ SETPD # PL AT 0
052102,001622: 12,3550 02710 RTNTR
052103,001623: 12,3551 00001 0
052104,001624: 12,3552 77600 BOV
052105,001625: 12,3553 25554 +1
052106,001626: 12,3554 63375 VLOAD PDVL # PL AT 6
052107,001627: 12,3555 02655 RVEC
052108,001628: 12,3556 02744 VVEC
052109,001629: 12,3557 77624 CALL
052110,001630: 12,3560 11064 PARAM
052111,001631: 12,3561 71200 BOV DLOAD # PL AT 0
052112,001632: 12,3562 24764 COGAOVFL
052113,001633: 12,3563 11043 D1/32
052114,001634: 12,3564 41225 DSU DMP
052115,001635: 12,3565 02742 R1A
052116,001636: 12,3566 02740 P
052117,001637: 12,3567 41366 SQRT DMP
052118,001638: 12,3570 02766 COGA
052119,001639: 12,3571 74212 SL4 VXSC
052120,001640: 12,3572 02712 U2
052121,001641: 12,3573 45325 PDDL DSU # PL AT 6
052122,001642: 12,3574 11035 D1/64
052123,001643: 12,3575 02742 R1A
052124,001644: 12,3576 52361 VXSC VSU # PL AT 0
052125,001645: 12,3577 02722 UR1
052126,001646: 12,3600 53512 VSL4 UNIT
052127,001647: 12,3601 77600 BOV
052128,001648: 12,3602 25660 CIRCULAR
052129,001649: 12,3603 60325 PDDL NORM # 0D=UNIT(ECC) (+3) PL AT 6
052130,001650: 12,3604 02756 RDESIRED # 36D=ECC (+3)
052131,001651: 12,3605 00047 X1
052132,001652: 12,3606 41325 PDDL DMP # PL AT 8
052133,001653: 12,3607 00041 R1
052134,001654: 12,3610 02740 P
052135,001655: 12,3611 56257 SL* DDV # PL AT 6
052136,001656: 12,3612 20201 0,1
052137,001657: 12,3613 56225 DSU DDV
052138,001658: 12,3614 11041 D1/16
052139,001659: 12,3615 00045 36D # 36D=ECC (+3)
052140,001660: 12,3616 00031 STORE COSF
052141,001661: 12,3617 63400 BOV DSQ
052142,001662: 12,3620 25664 BADR2
052143,001663: 12,3621 50021 BDSU BMN
052144,001664: 12,3622 11037 D1/4
052145,001665: 12,3623 25664 BADR2
052146,001666: 12,3624 75366 SQRT SIGN
052147,001667: 12,3625 02755 SGNRDOT
052148,001668: 12,3626 77614 CLEAR
052149,001669: 12,3627 04272 APSESW
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|
Page 1199 |
052151,001671: 12,3630 76561 TERMNVEC VXSC VSL1
052152,001672: 12,3631 02674 UN
052153,001673: 12,3632 63235 VXV PDVL # VXCH WITH 0D PL AT 0,6
052154,001674: 12,3633 00001 0D
052155,001675: 12,3634 53361 VXSC VAD # PL AT 0
052156,001676: 12,3635 00031 COSF
052157,001677: 12,3636 41572 VSL1 PUSH # 0D=U2 PL AT 6
052158,001678:
052159,001679: 12,3637 56241 DOT DDV # LIMITS RESULT TO POSMAX OR NEGMAX
052160,001680: 12,3640 02722 UR1
052161,001681: 12,3641 25756 DP1/4
052162,001682: 12,3642 40142 SR1 BOV # SCALE BACK DOWN TO NORMAL
052163,001683: 12,3643 25644 +1 # CLEAR OVFIND IF SET
052164,001684: 12,3644 26732 STOVL CSTH # CSTH (+1)
052165,001685: 12,3645 02722 UR1
052166,001686: 12,3646 76435 VXV VSL1
052167,001687: 12,3647 72441 DOT SL1
052168,001688: 12,3650 02674 UN
052169,001689: 12,3651 16730 STODL SNTH # SNTH (+1)
052170,001690: 12,3652 02740 P
052171,001691: 12,3653 77624 CALL
052172,001692: 12,3654 24767 GETX
052173,001693: 12,3655 77614 CLRGO
052174,001694: 12,3656 02634 SOLNSW
052175,001695: 12,3657 24747 COMMNOUT
052176,001696:
052177,001697: 12,3660 43001 CIRCULAR SETPD SETGO
052178,001698: 12,3661 00001 0
052179,001699: 12,3662 02434 SOLNSW
052180,001700: 12,3663 25742 ABTCONIC
052181,001701:
052182,001702: 12,3664 75345 BADR2 DLOAD SIGN
052183,001703: 12,3665 24005 LODPHALF
052184,001704: 12,3666 00031 COSF
052185,001705: 12,3667 14031 STODL COSF
052186,001706: 12,3670 24007 KEPZERO
052187,001707: 12,3671 77614 SETGO
052188,001708: 12,3672 04032 APSESW
052189,001709: 12,3673 25630 TERMNVEC
052190,001710:
|
|
Page 1200 |
052192,001712: 12,3674 40220 APSIDES STQ SETPD # PL AT 0
052193,001713: 12,3675 02710 RTNAPSE
052194,001714: 12,3676 00001 0D
052195,001715: 12,3677 77600 BOV
052196,001716: 12,3700 25701 +1
052197,001717: 12,3701 63375 VLOAD PDVL # PL AT 6
052198,001718: 12,3702 02655 RVEC
052199,001719: 12,3703 02744 VVEC
052200,001720: 12,3704 77624 CALL
052201,001721: 12,3705 11064 PARAM
052202,001722: 12,3706 77600 BOV # PL AT 0
052203,001723: 12,3707 25710 GETECC
052204,001724: 12,3710 42405 GETECC DMP SL4
052205,001725: 12,3711 02742 R1A
052206,001726: 12,3712 75421 BDSU SQRT
052207,001727: 12,3713 11035 D1/64
052208,001728: 12,3714 02752 STORE ECC
052209,001729: 12,3715 65215 DAD PDDL # PL AT 2
052210,001730: 12,3716 11031 D1/8
052211,001731: 12,3717 00041 R1
052212,001732: 12,3720 72405 DMP SL1
052213,001733: 12,3721 02740 P
052214,001734: 12,3722 77671 DDV # PL AT 0
052215,001735: 12,3723 60325 PDDL NORM # 0D=RP (+29 OR +27) PL AT 2
052216,001736: 12,3724 02742 R1A
052217,001737: 12,3725 00047 X1
052218,001738: 12,3726 53725 PDDL SL* # PL AT 4
052219,001739: 12,3727 00041 R1
052220,001740: 12,3730 20174 0 -5,1
052221,001741: 12,3731 45271 DDV DSU # PL AT 2,0
052222,001742: 12,3732 50000 BOV BMN
052223,001743: 12,3733 25737 INFINAPO
052224,001744: 12,3734 25737 INFINAPO
052225,001745: 12,3735 77650 GOTO
052226,001746: 12,3736 02710 RTNAPSE
052227,001747: 12,3737 52145 INFINAPO DLOAD GOTO # RETURNS WITH APOAPSIS IN MPAC, PERIAPSIS
052228,001748: 12,3740 24020 LDPOSMAX
052229,001749: 12,3741 02710 RTNAPSE # THAT PL IS AT 0.
052230,001750:
|
|
Page 1201 |
052232,001752: 12,3742 77776 ABTCONIC EXIT
052233,001753: 12,3743 05652 TC POODOO
052234,001754: 12,3744 00607 OCT 00607
052235,001755:
|
|
Page 1202 |
052237,001757: 12,3745 12,2017 LDPOSMAX EQUALS LODPMAX # DPPOSMAX IN LOW MEMORY.
052238,001758:
052239,001759: # ERASABLE ASSIGNMENTS
052240,001760:
052241,001761: # KEPLER SUBROUTINE
052242,001762:
052243,001763: # INPUT -
052244,001764: # RRECT ERASE +5
052245,001765: # VRECT ERASE +5
052246,001766: # TAU. ERASE +1
|
|
Handwritten "NEW" next to XKEP. |
052248,001768: # XKEP ERASE +1
052249,001769: # TC ERASE +1
052250,001770: # XPREV ERASE +1
052251,001771: 12,3745 1/MU EQUALS 14D
052252,001772: 12,3745 ROOTMU EQUALS 16D
052253,001773: 12,3745 1/ROOTMU EQUALS 18D
052254,001774:
052255,001775: # OUTPUT -
052256,001776: # RCV ERASE +5
052257,001777: # VCV ERASE +5
|
|
The beginning of the next line is garbled, but I believe that it is RC with a hand-written correction to TC — RSB, 2016. |
052259,001779: # RC ERASE +1
052260,001780: # XPREV ERASE +1
052261,001781:
052262,001782: # DEBRIS -
052263,001783: 12,3745 ALPHA EQUALS 8D
052264,001784: 12,3745 XMAX EQUALS 10D
052265,001785: 12,3745 XMIN EQUALS 12D
052266,001786: 12,3745 X EQUALS 20D
052267,001787: 12,3745 XI EQUALS 24D
052268,001788: 12,3745 S(XI) EQUALS 26D
052269,001789: 12,3745 XSQC(XI) EQUALS 28D
052270,001790: 12,3745 T EQUALS 30D
052271,001791: 12,3745 R1 EQUALS 32D
052272,001792: 12,3745 KEPC1 EQUALS 34D
052273,001793: 12,3745 KEPC2 EQUALS 36D
052274,001794: # DELX ERASE +1
052275,001795: # DELT ERASE +1
052276,001796: # URRECT ERASE +5
052277,001797: # RCNORM ERASE +1
052278,001798: # XPREV EQUALS XKEP
052279,001799:
052280,001800:
052281,001801: # LAMBERT SUBROUTINE
052282,001802:
052283,001803: # INPUT -
052284,001804: # R1VEC ERASE +5
052285,001805: # R2VEC ERASE +5
052286,001806: # TDESIRED ERASE +1
052287,001807: # GEOMSGN ERASE +0
052288,001808: # GUESSW 0 IF COGA GUESS AVAILABLE, 1 IF NOT
|
|
Page 1203 |
052290,001810: # COGA ERASE +1 INPUT ONLY IF GUESSW IS ZERO.
052291,001811: # NORMSW 0 IF UN TO BE COMPUTED, 1 IF UN INPUT
052292,001812: # UN ERASE +5 ONLY USED IF NORMSW IS 1
052293,001813: # VTARGTAG ERASE +0
052294,001814: # TWEEKIT EQUALS 40D ONLY USED IF GUESSW IS 0
052295,001815:
052296,001816: # OUTPUT -
052297,001817: # VTARGET ERASE +5 AVAILABLE ONLY IF VTARGTAG IS ZERO.
052298,001818: # V1VEC EQUALS MPAC
052299,001819:
052300,001820: # DEBRIS -
052301,001821: # RTNLAMB ERASE +0
052302,001822: # U2 ERASE +5
052303,001823: # MAGVEC2 ERASE +1
052304,001824: # UR1 ERASE +5
|
|
There is a hand-written 32D to the right of the next line. |
052306,001826: # R1 EQUALS 31D
052307,001827: # UN ERASE +5
052308,001828: # SNTH ERASE +1
052309,001829: # CSTH ERASE +1
052310,001830: # 1-CSTH ERASE +1
052311,001831: # CSTH-RHO ERASE +1
052312,001832: 12,3745 COGAMAX EQUALS 14D # CLOBBERS 1/MU
052313,001833: 12,3745 COGAMIN EQUALS 8D
052314,001834: 12,3745 DCOGA EQUALS 12D
052315,001835: # TWEEKIT EQUALS 40D
052316,001836: # P ERASE +1
052317,001837: # COGA ERASE +1
052318,001838: # R1A ERASE +1
052319,001839: # X EQUALS 20D
052320,001840: # XSQ EQUALS 22D
052321,001841: # XI EQUALS 24D
052322,001842: # S(XI) EQUALS 26D
052323,001843: # XSQC(XI) EQUALS 28D
052324,001844: # T EQUALS 30D
052325,001845: # KEPC1 EQUALS 34D
052326,001846: # KEPC2 EQUALS 36D
052327,001847: # SLOPESW
052328,001848: # SOLNSW
052329,001849:
052330,001850: # OTHERS -
052331,001851: # RVEC EQUALS R1VEC
052332,001852: # VVEC ERASE +5
052333,001853: # COGAFLAG
052334,001854: # RVSW
052335,001855: # INFINFLG
052336,001856: # APSESW
052337,001857: # 360SW
052338,001858: # RTNTT EQUALS RTNLAMB
052339,001859: # ECC ERASE +1
052340,001860: # RTNTR EQUALS RTNLAMB
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Page 1204 |
052342,001862: # RTNAPSE EQUALS RTNLAMB
052343,001863: # R2 EQUALS MAGVEC2
052344,001864: 12,3745 COSF EQUALS 24D
052345,001865: # RTNPRM ERASE +0
052346,001866: # SGNRDOT ERASE +0
052347,001867: # RDESIRED ERASE +1
052348,001868:
052349,001869:
052350,001870: # ITERATOR SUBROUTINE
052351,001871: # ORDERSW
052352,001872: 12,3745 MAX EQUALS 14D # CLOBBERS 1/MU
052353,001873: 12,3745 MIN EQUALS 8D
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|
"E5,1765" is hand-written next to the following. |
052355,001875: # INDEP ERASE +1
052356,001876: 12,3745 DELINDEP EQUALS 12D
052357,001877: 12,3745 ITERCTR EQUALS 22D
052358,001878: 12,3745 DEP EQUALS 30D
|
|
"E5,1757" is hand-written next to the following. |
052360,001880: # DELDEP ERASE +1
|
|
"E5,1761" is hand-written next to the following. |
052362,001882: # DEPREV ERASE +1
052363,001883: 12,3745 TWEEKIT EQUALS 40D
052364,001884:
052365,001885:
052366,001886: # MORE KEPLER
052367,001887: # EPSILONT ERASE +1
052368,001888:
052369,001889:
052370,001890: # MORE LAMBERT
052371,001891: # TERRLAMB EQUALS DELDEP
052372,001892: # TPREV EQUALS DEPREV
052373,001893:
052374,001894: # EPSILONL EQUALS EPSILONT +2 DOUBLE PRECISION WORD
End of include-file CONIC_SUBROUTINES.agc. Parent file is MAIN.agc