proof(luminary099): page 1160

Luminary099/CONIC_SUBROUTINES.agc

@@ -58,45 +58,47 @@
 
 # Page 1160
 # PROGRAM DESCRIPTION - KEPLER SUBROUTINE			DATE - 11 OCTOBER 1967
-# MOD NO. -1							LOG SECTION - CONIC SUBROUTINES
+# MOD NO. -1								LOG SECTION - CONIC SUBROUTINES
 # MOD BY KRAUSE							ASSEMBLY - COLOSSUS 103 AND SUNDANCE 222
 # MOD NO. - 2 (AUGUST 1968) BY ROBERTSON: TO PERMIT BACKDATING BY MORE THAN ONE ORBITAL PERIOD.
-# MOD NO. - 3 (DEC 1968) BY ROBERTSON:  SUPPRESSION OF X-MODULO-ING
+#
-# MOD NO. - 4 (JAN 1969) BY ROBERTSON:  CLEAR OVFIND AT KEPLER ENTRY
+# MOD NO. - 3 (DEC 1968) BY ROBERTSON: SUPPRESSION OF X-MODULO-ING
+#
+# MOD NO. - 4 (JAN 1969) BY ROBERTSON: CLEAR OVFIND AT KEPLER ENTRY
 #
 # FUNCTIONAL DESCRIPTION -
 #	THIS SUBROUTINE, GIVEN AN INITIAL STATE VECTOR AND THE DESIRED TRANSFER TIME THROUGH WHICH THE STATE IS TO
 # BE UPDATED ALONG A CONIC TRAJECTORY, COMPUTES THE NEW, UPDATED STATE VECTOR.  THE TRAJECTORY MAY BE ANY CONIC
-# SECTION - CIRCULAR, ELLIPTIC, PARABOLIC, HYPERPOLIC, OR RECTILINEAR WITH RESPECT TO THE EARTH OR THE MOON.  THE
+# SECTION - CIRCULAR, ELLIPTIC, PARABOLIC, HYPERBOLIC, OR RECTILINEAR WITH RESPECT TO THE EARTH OR THE MOON.  THE
 # USE OF THE SUBROUTINE CAN BE EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT
-# INTRODUCING ANY CODING CHANGES, ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY.  AN ITERATION
+# INTRODUCING ANY CODING CHANGES, ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY.  AN ITERA-
-# TECHNIQUE IS UTILIZED IN THE COMPUTATION.
+# TION TECHNIQUE IS UTILIZED IN THE COMPUTATION.
-#
 #	IF A NEGATIVE TIME-OF-FLIGHT IS INPUT, THE PROGRAM WILL SOLVE FOR THE STATE WHICH WOULD BE PRODUCED BY
 # EXTRAPOLATING THE POSITION BACKWARD IN TIME.
-#
 #	IF THE ABSOLUTE VALUE OF THE DESIRED TRANSFER TIME EXCEEDS THE ORBITAL PERIOD, THE SUBROUTINE, THROUGH A
 #  MODULAR TECHNIQUE, WILL COMPUTE THE STATE CORRESPONDING TO THE DESIRED TIME (WHETHER POSITIVE OR NEGATIVE).
 #
 # THE RESTRICTIONS ARE -
 #	1. (PREVIOUS RESTRICTION ON THE NEGATIVE DESIRED TRANSFER TIME IS NOW DELETED.)
-#	2. THE PARAMETERS IN THE PROBLEM CANNOT EXCEED THEIR SCALING LIMITS AS SPECIFIED IN THE GSOP.  IF
+#	2.  THE PARAMETERS IN THE PROBLEM CANNOT EXCEED THEIR SCALING LIMITS AS SPECIFIED IN THE GSOP.  IF
-#	   ANY OF THESE LIMITS ARE EXCEEDED, THE RESULTING SOLUTION WILL BE MEANINGLESS.
+# ANY OF THESE LIMITS ARE EXCEEDED, THE RESULTING SOLUTION WILL BE MEANINGLESS.
 #
 # 	THE NUMBER OF ITERATIONS AND, THEREFORE, THE COMPUTATION SPEED IS DEPENDENT ON THE ACCURACY OF THE
-# GUESS, XKFPNEW.  THE AGC COMPUTATION TIME IS APPROXIMATELY .061 SECONDS FOR INITIALIZATION, .065 SECONDS FOR THE
+# GUESS, XKEPNEW.  THE AGC COMPUTATION TIME IS APPROXIMATELY .061 SECONDS FOR INITIALIZATION, .065 SECONDS FOR THE
 # FINAL COMPUTATIONS, PLUS .083 SECONDS FOR EACH ITERATION.
 #
+#
 # REFERENCES -
 #	R-479, MISSION PROGRAMMING DEFINITION MEMO NO. 10, LUNAR LANDING MISSION GSOP, SECTION 5.5, SGA
-#	MEMO 67-4.
+# MEMO 67-4.
+#
 #
 # INPUT - ERASABLE INITIALIZATION REQUIRED
-#			* SCALE FACTOR 	*
+#			* SCALE FACTOR *
-#	VARIABLE	*IN POWERS OF 2	* 		DESCRIPTION AND REMARKS
+#	VARIABLE	*IN POWERS OF 2* 		DESCRIPTION AND REMARKS
-#	--------	*--------------	*		-----------------------
+#	--------	*--------------*		-----------------------
-#	RRECT		* +29 FOR EARTH	*	DP INITIAL POSITION VECTOR IN METERS
+#	RRECT		* +29 FOR EARTH*	DP INITIAL POSITION VECTOR IN METERS
-#			* +27 FOR MOON	*
+#			* +27 FOR MOON *
 # Page 1161
 #	VRECT		* +7 FOR EARTH	*	DP INITIAL VELOCITY VECTOR IN METERS/CENTISECOND
 #			* +5 FOR MOON	*