proof(luminary099): page 1171
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# * * CLEAR IF NOT.
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# APSESW * NONE * AN INTERPRETIVE SWITCH WHICH IS SET IF RDESIRED WAS GREATER THAN RADIUS OF APOCENTER OR
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# Page 1171
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# * * LESS THAN RADIUS OF PERICENTER. THE APOCENTER OR PERICENTER SOLUTION, RESPECTIVELY,
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# * * WILL THEN BE RETURNED. THE SWITCH IS CLEAR IF RDESIRED WAS BETWEEN PERICENTER AND
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# * * APOCENTER.
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# SOLNSW * NONE * AN INTERPRETIVE SWITCH WHICH IS SET IF THE CONIC IS SO CLOSE TO A CIRCLE THAT THE TERMIN
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# * * POINT IS AMBIGUOUS, VIOLATING RESTRICTION 3. IF ECCENTRICITY IS GREATER THAN 2-TO-THE-
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# * * MINUS-18, THE SWITCH IS CLEAR.
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# * * LESS THAN RADIUS OF PERICENTER. THE APOCENTER OR PERICENTER SOLUTION, RESPECTIVELY,
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# * * WILL THEN BE RETURNED. THE SWITCH IS CLEAR IF RDESIRED WAS BETWEEN PERICENTER AND
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# * * APOCENTER.
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# SOLNSW * NONE * AN INTERPRETIVE SWITCH WHICH IS SET IF THE CONIC IS SO CLOSE TO A CIRCLE THAT THE TERMIN
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# * * POINT IS AMBIGUOUS, VIOLATING RESTRICTION 3. IF ECCENTRICITY IS GREATER THAN 2-TO-THE-
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# * * MINUS-18, THE SWITCH IS CLEAR.
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#
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# IN ADDITION, IF RVSW IS CLEAR, THE FOLLOWING ARE OUTPUT -
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#
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# MPAC - * +7 FOR EARTH * DP TERMINAL VELOCITY VECTOR IN METERS/CENTISEC.
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# MPAC +5 * +5 FOR MOON *
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# 0D - 5D * +29 FOR EARTH * DP TERMINAL POSITION VECTOR IN METERS (PL AT 6D)
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# * +27 FOR MOON *
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# IN ADDITION, IF RVSW IS CLEAR, THE FOLLOWING ARE OUTPUT-
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#
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# MPAC - * +7 FOR EARTH * DP TERMINAL VELOCITY VECTOR IN METERS/CENTISEC.
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# MPAC +5 * +5 FOR MOON *
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# 0D - 5D * +29 FOR EARTH* DP TERMINAL POSITION VECTOR IN METERS (PL AT 6D)
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# * +27 FOR MOON *
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#
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# FOR OTHER OUTPUT WHICH MAY BE OF USE, SEE DEBRIS.
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#
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# FOR OTHER OUTPUT WHICH MAY BE OF USE, SEE DEBRIS.
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#
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# DEBRIS -
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#
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# PARAMETERS WHICH MAY BE OF USE -
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#
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# * SCALE FACTOR *
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# VARIABLE *IN POWERS OF 2 * DESCRIPTION AND REMARKS
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# -------- *-------------- * -----------------------
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# R1 (32D) * +29 FOR EARTH * DP MAGNITUDE OF INITIAL POSITION VECTOR, RVEC, IN METERS
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# * +27 FOR MOON *
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# R1A * +6 * DP RATIO OF R1 TO SEMIMAJOR AXIS (NEG. FOR HYPERBOLIC TRAJECTORIES)
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# P * +4 * DP RATIO OF SEMILATUS RECTUM TO R1
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# COGA * +5 * DP COTAN OF ANGLE BETWEEN RVEC AND VVEC
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# UR1 * +1 * DP UNIT VECTOR OF RVEC
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# U2 * +1 * DP UNIT VECTOR OF VVEC
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# UN * +1 * DP UNIT VECTOR OF UR1*U2
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# CSTH * +1 * DP COSINE OF TRUE ANOMALY DIFFERENCE BETWEEN RVEC AND RDESIRED.
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# SNTH * +1 * DP SINE OF TRUE ANOMALY DIFFERENCE.
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# * SCALE FACTOR *
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# VARIABLE *IN POWERS OF 2* DESCRIPTION AND REMARKS
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# -------- *--------------* -----------------------
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# R1 (32D) * +29 FOR EARTH* DP MAGNITUDE OF INITIAL POSITION VECTOR, RVEC, IN METERS
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# * +27 FOR MOON *
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# R1A * +6 * DP RATIO OF R1 TO SEMIMAJOR AXIS (NEG. FOR HYPERBOLIC TRAJECTORIES)
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# P * +4 * DP RATIO OF SEMILATUS RECTUM TO R1
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# COGA * +5 * DP COTAN OF ANGLE BETWEEN RVEC AND VVEC
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# UR1 * +1 * DP UNIT VECTOR OF RVEC
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# U2 * +1 * DP UNIT VECTOR OF VVEC
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# UN * +1 * DP UNIT VECTOR OF UR1*U2
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# CSTH * +1 * DP COSINE OF TRUE ANOMALY DIFFERENCE BETWEEN RVEC AND RDESIRED.
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# SNTH * +1 * DP SINE OF TRUE ANOMALY DIFFERENCE.
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#
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#
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# PARAMETERS OF NO USE -
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# SP PARAMETERS -- RTNTT, GEOMSGN, RTNPRM, MAGVEC2=R2 (DP), PLUS PUSHLIST LOCATIONS 0-11D, 14D-21D, 24D-39D, 41D
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# ADDITIONAL INTERPRETIVE SWITCHES USED -- NORMSW, 360SW
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# SP PARAMETERS - RTNTT, GEOMSGN, RTNPRM, MAGVEC2=R2 (DP), PLUS PUSHLIST LOCATIONS 0-11D, 14D-21D, 24D-39D, 41D
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# ADDITIONAL INTERPRETIVE SWITCHES USED - NORMSW, 360SW
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#
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# Page 1172
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