proof(luminary099): page 1169

Luminary099/CONIC_SUBROUTINES.agc

@@ -420,18 +420,19 @@
 # MOD NO. -1							LOG SECTION - CONIC SUBROUTINES
 # MOD BY KRAUSE							ASSEMBLY - COLOSSUS REVISION 88
 #
+#
 # FUNCTIONAL DESCRIPTION -
 #
 #	THIS SUBROUTINE, GIVEN AN INITIAL STATE VECTOR AND A DESIRED RADIUS TO WHICH THE
 # STATE IS TO BE UPDATED ALONG A CONIC TRAJECTORY, CALCULATES THE CORRESPONDING TIME-OF-FLIGHT AND, IN ADDITION,
 # PROVIDES THE OPTION OF COMPUTING THE NEW UPDATED STATE VECTOR.  THE RESULTING TRAJECTORY MAY BE A SECTION OF A
 # CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON.  THE USE OF THE SUBROUTINE CAN BE
-#	EXTENDED USING OTHER PRIMARY BODIES BY SIMMPE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY CODING CHANGES,
+# 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.
-#
 #	IF THE DESIRED RADIUS IS BEYOND THE RADIUS OF APOCENTER OF THE CONIC OR BELOW THE RADIUS OF PERICENTER,
 # APSESW WILL BE SET AND THE SUBROUTINE WILL RETURN THE APOCENTER OR PERICENTER SOLUTION, RESPECTIVELY.
 #
+#
 # THE RESTRICTIONS ARE -
 #	1. THE ANGLE BETWEEN ANY POSITION VECTOR AND ITS VELOCITY VECTOR MUST BE GREATER THAN 1 DEGREE 47.5 MINUTES
 # AND LESS THAN 178 DEGREES 12.5 MINUTES.
@@ -441,12 +442,15 @@
 # RDESIRED INCREASE.  THIS WILL OCCUR NEAR EITHER APSIS OF THE CONIC AND WHEN THE CONIC IS NEARLY CIRCULAR.  IN
 # PARTICULAR, IF THE CONIC IS AN EXACT CIRCLE, THE PROBLEM IS UNDEFINED AND THE SUBROUTINE WILL ABORT.
 #
-#	THE AGC COMPUTATION TIME IS APPROXIMATELY .363 SECONDS.
+#	THE AGC COMPUTATION TIME IS APPROXIMATELY .363 SECONDS
+#
 #
 # REFERENCES -
 #	R-479, MISSION PROGRAMMING DEFINITION MEMO NO. 10, LUNAR LANDING MISSION GSOP-SECTION 5.5, SGA MEMO 67-8.
 #
-# INPUT - ERASABLE INITIALIZATION REQUIRED.
+#
+# INPUT - ERASABLE INITIALIZATION REQUIRED
+#
 #			* SCALE FACTOR *
 #	VARIABLE	*IN POWERS OF 2*	DESCRIPTION AND REMARKS
 #	--------	*--------------*	-----------------------
@@ -455,7 +459,7 @@
 #	VVEC		* +7 FOR EARTH *	DP INITIAL VELOCITY VECTOR IN METERS/CENTISECOND
 #			* +5 FOR MOON  *
 #	RDESIRED	* +29 FOR EARTH*	DP TERMINAL RADIAL DISTANCE ON CONIC TRAJECTORY FOR WHICH TRANSFER TIME IS TO BE
-#			* +27 FOR MOON	*		COMPUTED
+#			* +27 FOR MOON *	COMPUTED.
 #	SGNRDOT		* NONE	       *	SP TAG SET TO +.5 OR -.5 ACCORDING TO WHETHER THE RADIAL VELOCITY AT RDESIRED IS TO BE
 #			*	       *	POSITIVE OR NEGATIVE, RESPECTIVELY.   THIS TAG REDUCES THE DOUBLE-VALUED PROBLEM TO A
 # Page 1170