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Luminary099/CONIC_SUBROUTINES.agc
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@ -266,38 +266,39 @@
#
# Page 1165
# OUTPUT -
# * SCALE FACTOR *
# VARIABLE *IN POWERS OF 2 * DESCRIPTION AND REMARKS
# -------- *-------------- * -----------------------
# VVEC * +7 FOR EARTH * DP INITIAL VELOCITY VECTOR IN METERS/CENTISECOND REQUIRED TO SATISFY THE BOUNDARY VALUE
# * +5 FOR MOON * PROBLEM.
# VTARGET * +7 FOR EARTH * DP RESULTANT VELOCITY VECTOR AT R2VEC IN METERS/CENTISECOND.
# * +5 FOR MOON *
# SOLNSW * NONE * INTERPRETER SWITCH WHICH IS SET IF THE SUBROUTINE CANNOT SOLVE THE PROBLEM, CLEAR IF THE
# * * SOLUTION EXISTS.
#
# * SCALE FACTOR *
# VARIABLE *IN POWERS OF 2* DESCRIPTION AND REMARKS
# -------- *--------------* -----------------------
# VVEC * +7 FOR EARTH * DP INITIAL VELOCITY VECTOR IN METERS/CENTISECOND REQUIRED TO SATISFY THE BOUNDARY VALUE
# * +5 FOR MOON * PROBLEM.
# VTARGET * +7 FOR EARTH * DP RESULTANT VELOCITY VECTOR AT R2VEC IN METERS/CENTISECOND.
# * +5 FOR MOON *
# SOLNSW * NONE * INTERPRETER SWITCH WHICH IS SET IF THE SUBROUTINE CANNOT SOLVE THE PROBLEM, CLEAR IF THE
# * * SOLUTION EXISTS.
# FOR OTHER OUTPUT WHICH MAY BE OF USE, SEE DEBRIS.
#
#
# DEBRIS -
# PARAMETERS WHICH MAY BE OF USE -
#
# * SCALE FACTOR *
# VARIABLE *IN POWERS OF 2 * DESCRIPTION AND REMARKS
# -------- *-------------- * -----------------------
# SNTH * +1 * DP SIN OF ANGLE BETWEEN R1VEC AND R2VEC
# CSTH * +1 * DP COSINE OF ANGLE
# 1-CSTH * +2 * DP 1-CSTH
# COGA * +5 * DP COTAN OF INITIAL REQUIRED FLIGHT PATH ANGLE MEASURED FROM VERTICAL
# P * +4 * DP RATIO OF SEMILATUS RECTUM TO INITIAL RADIUS
# R1A * +6 * DP RATIO OF INITIAL RADIUS TO SEMI-MAJOR AXIS
# R1 (32D) * +29 FOR EARTH * DP INITIAL RADIUS IN METERS
# * +27 FOR MOON *
# UR1 * +1 * DP UNIT VECTOR OF R1VEC
# U2 * +1 * DP UNIT VECTOR OF R2VEC
# * SCALE FACTOR *
# VARIABLE *IN POWERS OF 2* DESCRIPTION AND REMARKS
# -------- *--------------* -----------------------
# SNTH * +1 * DP SIN OF ANGLE BETWEEN R1VEC AND R2VEC
# CSTH * +1 * DP COSINE OF ANGLE
# 1-CSTH * +2 * DP 1-CSTH
# COGA * +5 * DP COTAN OF INITIAL REQUIRED FLIGHT PATH ANGLE MEASURED FROM VERTICAL
# P * +4 * DP RATIO OF SEMILATUS RECTUM TO INITIAL RADIUS
# R1A * +6 * DP RATIO OF INITIAL RADIUS TO SEMIMAJOR AXIS
# R1 (32D) * +29 FOR EARTH* DP INITIAL RADIUS IN METERS
# * +27 FOR MOON *
# UR1 * +1 * DP UNIT VECTOR OF R1VEC
# U2 * +1 * DP UNIT VECTOR OF R2VEC
#
# PARAMETERS OF NO USE -
# DP PARAMETERS - EPSILONL, CSTH-RHO, TPREV, TERRLAMB, R2, RTNLAMB (SP), PLUS PUSHLIST REGISTER 0 THROUGH 41D
# ADDITIONAL INTERPRETIVE SWITCHES USED - INFINFLG, 360SW, SLOPESW, ORDERSW
# DP PARAMETERS - EPSILONL, CSTH-RHO, TPREV, TERRLAMB, R2, RTNLAMB (SP), PLUS PUSHLIST REGISTER 0 THROUGH 41D
# ADDITIONAL INTERPRETIVE SWITCHES USED - INFINFLG, 360SW, SLOPESW, ORDERSW
#
# Page 1166
# PROGRAM DESCRIPTION - TIME-THETA SUBROUTINE DATE - 1 SEPTEMBER 1967