Proof P34-35_P74-75 #615 (pg: 0692-0702)

Luminary099/P34-35_P74-75.agc

@@ -961,15 +961,15 @@ GET45		EXIT
 		CADR	GOFLASH
 		TC	KILCLOCK	# TERMINATE
 		TC	N45PROC		# PROCEED
-		TC	CLUPDATE	# RECYCLE -- RETURN FOR INITIAL COMPUTATION
+		TC	CLUPDATE	# RECYCLE - RETURN FOR INITIAL COMPUTATION
 KILCLOCK	CA	Z
 		TS	DISPDEX
 # Page 681
 		TC	GOTOPOOH
 N45PROC		CS	FLAGWRD2
 		MASK	BIT6
 		EXTEND
-		BZF	KILCLOCK	# FINALFLG IS SET -- FLASH V37 -- AWAIT NEW PGM
+		BZF	KILCLOCK	# FINALFLG IS SET-FLASH V37-AWAIT NEW PGM
 		TC	PHASCHNG
 		OCT	04024
 		TC	UPFLAG		# SET
@@ -1055,13 +1055,13 @@ EPSFOUR		2DEC	.0416666666
 # Page 685
 # ***** INITVEL *****
 
-# MOD NO -1			LOG SECTION -- P34-P35, P74-P75
-# MOD BY WHITE, P.		DATE:  21 NOV 67
+# MOD NO -1			LOG SECTION - P34-P35, P74-P75
+# MOD BY WHITE.P		DATE  21NOV67
 #
-# FUNCTIONAL
+# FUNCTIONAL DESCRIPTION
 #
 #	THIS SUBROUTINE COMPUTES THE REQUIRED INITIAL VELOCITY VECTOR FOR
-#	A TRAJECTORY OF SPECIFIC TRANSFER TIME BETWEEN SPECIFIED INITIAL
+#	A TRAJECTORY OF SPECIFIED TRANSFER TIME BETWEEN SPECIFIED INITIAL
 #	AND TARGET POSITIONS.  THE TRAJECTORY MAY BE EITHER CONIC OR
 #	PRECISION DEPENDING ON AN INPUT PARAMETER (NAMELY, NUMBER OF
 #	OFFSETS).  IN ADDITION, IN THE PRECISION TRAJECTORY CASE, THE
@@ -1088,7 +1088,7 @@ EPSFOUR		2DEC	.0416666666
 #
 #	L	CALL
 #	L+1		INITVEL
-#	L+2	(RETURN -- ALWAYS)
+#	L+2	(RETURN - ALWAYS)
 #
 # INPUT
 #
@@ -1100,7 +1100,7 @@ EPSFOUR		2DEC	.0416666666
 #	(6)	0D		NUMBER OF ITERATIONS OF LAMBERT/INTEGRVS
 #	(7)	2D		ANGLE TO 180 DEGREES WHEN ROTATION STARTS
 #	(8)	RTX1		-2 FOR EARTH, -10D FOR LUNAR
-#	(9)	RTX2		COORDINATE SYSTEM ORIGIN -- 0 FOR EARTH, 2 FOR LUNAR
+#	(9)	RTX2		COORDINATE SYSTEM ORIGIN - 0 FOR EARTH, 2 FOR LUNAR
 #	PUSHLOC SET AT 4D
 #
 # Page 686
@@ -1148,8 +1148,8 @@ HAVEGUES	VLOAD	STQ
 
 INITVEL1	SSP	DLOAD		# SET ITCTR TO -1,LOAD MPAC WITH E4 (PL 2D)
 			ITCTR
-			0 	-1
-		COSINE	SR1		# CALCULATE COSINE (E4) (+2)
+			0 -1
+		COSINE	SR1		# CALCULATE COSINE (E4)   (+2)
 		STODL	COZY4		# SET COZY4 TO COSINE (E4) 	    (PL 0D)
 		LXA,2	SXA,2
 			MPAC
@@ -1170,7 +1170,7 @@ INITVEL1	SSP	DLOAD		# SET ITCTR TO -1,LOAD MPAC WITH E4 (PL 2D)
 			VINIT		# MPAC EQ UNIT(RI) X VI (+8)
 		STOVL	UN
 			RTARG1
-		UNIT	DOT		# TEMP*RT.URI (+2)		    (PL 0D)
+		UNIT	DOT		# TEMP*URT.URI (+2)		    (PL 0D)
 		DAD	CLEAR
 			COZY4
 			NORMSW
@@ -1179,7 +1179,7 @@ INITVEL2	BPL	SET
 			INITVEL3	# UN CALCULATED IN LAMBERT
 			NORMSW
 
-# ROTATE RC INTO YC PLANE -- SET UNIT NORMAL TO YC
+# ROTATE RC INTO YC PLANE - SET UNIT NORMAL TO YC
 
 		VLOAD	PUSH		#				    (PL 6D)
 			R2VEC		# RC TO 6D (+29)
@@ -1216,14 +1216,14 @@ INITVEL3	DLOAD	PDVL		#				    (PL 2D)
 		INCR,1	SLOAD
 			10D
 			X1
-		BHIZ	VLOAD		#				   (PL 14D)
+		BHIZ	VLOAD		#				   (PL14D)
 			+2
-		VCOMP	PUSH		#				   (PL 20D)
-		VLOAD			#				   (PL 14D)
-		VXV	DOT		#				    (PL 2D)
-		BPL	DLOAD		#				    (PL 0D)
+		VCOMP	PUSH		#				   (PL20D)
+		VLOAD			#				   (PL14D)
+		VXV	DOT		#				   (PL 2D)
+		BPL	DLOAD		#				   (PL 0D)
 			INITVEL4
-		DCOMP	PUSH		#				    (PL 2D)
+		DCOMP	PUSH		#				   (PL 2D)
 INITVEL4	LXA,2	SXA,2
 			0D
 			GEOMSGN
@@ -1354,44 +1354,44 @@ INITVELX	LXA,1	DLOAD*
 # ***** MIDGIM *****
 
 # MOD NO. 0, BY WILLMAN, SUBROUTINE RENDGUID, LOG P34-P35, P74-P75
-# REVISION 03, 17 FEB 67
+#  REVISION 03, 17 FEB 67
 #
-# IF THE ACTIVE VEHICLE IS DOING THE COMPUTATION, MIDGIM COMPUTES
+#          IF THE ACTIVE VEHICLE IS DOING THE COMPUTATION, MIDGIM COMPUTES
 # THE POSITIVE MIDDLE GIMBAL ANGLE OF THE ACTIVE VEHICLE TO THE INPUT
 # DELTA VELOCITY VECTOR (0D IN PUSH LIST), OTHERWISE
 # MIDGIM CONVERTS THE INPUT DELTA VELOCITY VECTOR FROM INERTIAL COORDIN-
 # ATES TO LOCAL VERTICAL COORDINATES OF THE ACTIVE VEHICLE.
 #
 # ** INPUTS **
 #
-#	NAME	MEANING						UNITS/SCALING/MODE
+#	NAME	MEANING						 UNITS/SCALING/MODE
 #
-#	AVFLAG	INT FLAG -- 0 IS CSM ACTIVE, 1 IS LEM ACTIVE			BIT
+#	AVFLAG	INT FLAG - 0 IS CSM ACTIVE, 1 IS LEM ACTIVE			BIT
 #	RINIT	ACTIVE VEHICLE RADIUS VECTOR			METERS/CSEC (+7) VT
 #	VINIT	ACTIVE VEHICLE VELOCITY VECTOR			METERS/CSEC (+7) VT
 #	0D(PL)	ACTIVE VEHICLE DELTA VELOCITY VECTOR		METERS/CSEC (+7) VT
 #
 # ** OUTPUTS **
 #
-#    NAME	MEANING						UNITS/SCALING/MODE
+#    NAME	MEANING						 UNITS/SCALING/MODE
 #
 #    +MGA	+ MIDDLE GIMBAL ANGLE				REVOLUTIONS (+0) DP
 #    DELVLVC	DELTA VELOCITY VECTOR IN LV COORD.		METERS/CSEC (+7) VT
-#    MGLVFLAG	INT FLAG: 0 IS +MGA COMPUTED, 1 IS DELVLVC COMP.		BIT
+#    MGLVFLAG	INT FLAG - 0 IS +MGA COMPUTED, 1 IS DELVLVC COMP.	    -	BIT
 #
 # ** CALLING SEQUENCE **
 #
 #	L 	CALL
 #	L+1		MIDGIM
-#	L+2	(RETURN -- ALWAYS)
+#	L+2	(RETURN - ALWAYS)
 #
 # ** NO SUBROUTINES CALLED **
 #
-# ** DEBRIS -- ERASABLE TEMPORARY USAGE **
+# ** DEBRIS - ERASABLE TEMPORARY USAGE **
 #
 #	A,Q,L, PUSH LIST, MPAC.
 #
-# ** ALARMS -- NONE **
+# ** ALARMS - NONE **
 
 # Page 692
 # MIDDLE GIMBAL ANGLE COMPUTATION.
@@ -1403,7 +1403,7 @@ INITVELX	LXA,1	DLOAD*
 
 HALFREV		2DEC	1 B-1
 
-GET+MGA		VLOAD	UNIT		# (PL 0D) V (+7) TO MPAC UNITIZE UV (+1)
+GET+MGA		VLOAD	UNIT		# (PL 0D) V (+7) TO MPAC, UNITIZE UV (+1)
 		UNIT
 		DOT	SL1		# DOT UV WITH Y(STABLE MEMBER) AND RESCALE
 			REFSMMAT +6	# FROM +2 TO +1 FOR ASIN ROUTINE
@@ -1415,7 +1415,7 @@ GET+MGA		VLOAD	UNIT		# (PL 0D) V (+7) TO MPAC UNITIZE UV (+1)
 SETMGA		STORE	+MGA
 		CLR	RVQ		# CLEAR MGLVFLAG TO INDICATE +MGA CALC
 			MGLVFLAG	# AND EXIT
-GET.LVC		VLOAD	UNIT		# (PL 6D) R (+29) IN MPAC UNITIZE UR
+GET.LVC		VLOAD	UNIT		# (PL 6D) R (+29) IN MPAC, UNITIZE UR
 			RINIT
 		VCOMP			# U(-R)
 		STORE	18D		# U(-R) TO 18D
@@ -1468,14 +1468,14 @@ RTRNMU		STORE	RTMU
 # Page 694
 # ***** PERIAPO *****
 #
-# MOD NO -1			LOG SECTION -- P34-P35, P74-P75
-# MOD BY WHITE, P.		DATE 18 JAN 68
+# MOD NO -1			LOG SECTION - P34-P35, P74-P75
+# MOD BY WHITE.P		DATE  18JAN68
 #
 # FUNCTIONAL DESCRIPTION
 #
 #	THIS SUBROUTINE COMPUTES THE TWO BODY APOCENTER AND PERICENTER
 #	ALTITUDES GIVEN THE POSITION AND VELOCITY VECTORS FOR A POINT ON
-#	TRAJECTORY AND THE PRIMARY BODY.
+#	THE TRAJECTORY AND THE PRIMARY BODY.
 #
 #	SETRAD IS CALLED TO DETERMINE THE RADIUS OF THE PRIMARY BODY.
 #
@@ -1486,31 +1486,31 @@ RTRNMU		STORE	RTMU
 #
 #	L	CALL
 #	L+1		PERIAPO
-#	L+2	(RETURN -- ALWAYS)
+#	L+2	(RETURN - ALWAYS)
 #
 # INPUT
 #
 #	(1)	RVEC	POSITION VECTOR IN METERS
-#			SCALE FACTOR -- EARTH +29, MOON +27
+#			SCALE FACTOR - EARTH +29, MOON +27
 #	(2)	VVEC	VELOCITY VECTOR IN METERS/CENTISECOND
-#			SCALE FACTOR -- EARTH +7, MOON +5
+#			SCALE FACTOR - EARTH +7, MOON +5
 #	(3)	X1	PRIMARY BODY INDICATOR
 #			EARTH -1, MOON -10
 #
 # OUTPUT
 #
 #	(1)	2D	APOCENTER RADIUS IN METERS
-#			SCALE FACTOR -- EARTH +29, MOON +27
+#			SCALE FACTOR - EARTH +29, MOON +27
 #	(2)	4D	APOCENTER ALTITUDE IN METERS
-#			SCALE FACTOR -- EARTH +29, MOON +27
+#			SCALE FACTOR - EARTH +29, MOON +27
 #	(3)	6D	PERICENTER RADIUS IN METERS
-#			SCALE FACTOR -- EARTH +29, MOON +27
+#			SCALE FACTOR - EARTH +29, MOON +27
 #	(4)	8D	PERICENTER ALTITUDE IN METERS
-#			SCALE FACTOR -- EARTH +29, MOON +27
+#			SCALE FACTOR - EARTH +29, MOON +27
 #	(5)	ECC	ECCENTRICITY OF CONIC TRAJECTORY
-#			SCALE FACTOR -- +3
+#			SCALE FACTOR - +3
 #	(6)	XXXALT	RADIUS OF THE PRIMARY BODY IN METERS
-#			SCALE FACTOR -- EARTH +29, MOON +27
+#			SCALE FACTOR - EARTH +29, MOON +27
 #	(7)	PUSHLOC	EQUALS 10D
 #
 # SUBROUTINES USED
@@ -1524,7 +1524,7 @@ RTRNMU		STORE	RTMU
 
 		COUNT*	$$/PERAP
 
-RPAD		2DEC	6373338 B-29	# STANDARD RADIUS OF PAD 37-B.
+RPAD		2DEC	6373338 B-29	# STANDARD RADIUS  OF PAD 37-B.
 					# = 20 909 901.57 FT
 
 PERIAPO1	LXA,2	VSR*
@@ -1620,44 +1620,45 @@ SHIFTR1		LXA,2	SL*
 # FUNCTIONAL DESCRIPTION
 #
 # TO DISPLAY AT ASTRONAUT REQUEST LGC CALCULATED RENDEZVOUS
-# OUT-OF-PLANE PARAMETERS (Y, YDOT, PSI).  (REQUESTED BY DSKY).
+# OUT-OF-PLANE PARAMETERS (Y , YDOT , PSI).  (REQUESTED BY DSKY).
 #
 # CALLING SEQUENCE
 #
-#	ASTRONAUT REQUEST THROUGH DSKY V 90 E
+# ASTRONAUT REQUEST THROUGH DSKY V 90 E
 #
 # SUBROUTINES CALLED
 #
-#	EXDSPRET
-#	GOMARKF
-#	CSMPREC
-#	LEMPREC
-#	SGNAGREE
-#	LOADTIME
+# EXDSPRET
+# GOMARKF
+# CSMPREC
+# LEMPREC
+# SGNAGREE
+# LOADTIME
 #
 # NORMAL EXIT MODES
 #
-#	ASTRONAUT REQUEST THROUGH DSKY TO TERMINATE PROGRAM V 34 E
+# ASTRONAUT REQUEST THROUGH DSKY TO TERMINATE PROGRAM V 34 E
 #
 # ALARM OR ABORT EXIT MODES
 #
-#	NONE
+# NONE
 #
 # OUTPUT
 #
-#	DECIMAL DISPLAY OF TIME, Y, YDOT AND PSI
+# DECIMAL DISPLAY OF TIME , Y , YDOT AND PSI
 #
-#	DISPLAYED VALUES Y, YDOT, AND PSI, ARE STORED IN ERASABLE
-#	REGISTERS RANGE, RRATE, AND RTHETA RESPECTIVELY.
+# DISPLAYED VALUES Y , YDOT , AND PSI , ARE STORED IN ERASABLE
+# REGISTERS RANGE , RRATE AND RTHETA RESPECTIVELY.
 #
 # ERASABLE INITIALIZATION REQUIRED
 #
-#	CSM AND LEM STATE VECTORS
+# CSM AND LEM STATE VECTORS
 #
 # DEBRIS
 #
-#	CENTRALS A,Q,L
-#	OTHER:  THOSE USED BY THE ABOVE LISTED SUBROUTINES
+# CENTRALS A,Q,L
+#
+# OTHER THOSE USED BY THE ABOVE LISTED SUBROUTINES
 
 		BANK	20
 		SETLOC	R36LM
@@ -1690,8 +1691,9 @@ R36INT		STCALL	TDEC1
 			RATT		# _
 		STORE	RPASS36		# R
 		UNIT	PDVL		#  P
+		                        # _
 		VXV	UNIT
-		STADR			# _
+		STADR
 		STODL	UNP36		# U
 			TAT
 		STCALL	TDEC1
@@ -1712,9 +1714,9 @@ R36INT		STCALL	TDEC1
 		DOT	SL1
 			UNP36		# .   _   _
 		STOVL	RRATE		# Y = U . V
-			06D		#          A
+			06D		# _        A    _
 # Page 702
-					# _           _
+
 		UNIT	PUSH		# U  = UNIT ( R  )		18D
 		VXV	VXV		#  RA          A
 			00D		#  _    _     _     _
@@ -1731,7 +1733,7 @@ R36INT		STCALL	TDEC1
 		PUSH	DOT		# LOS PROJECTED INTO HORIZONTAL  12D
 			00D		# PLANE
 		SL1	ARCCOS		#              _   _
-		STOVL	RTHETA		# PSI = ARCCOS(U . U )
+		STOVL	RTHETA		# PSI = ARCCOS(U  .U )
 		VXV	DOT		#               A   L
 			00D
 		BPL	DLOAD
@@ -1745,15 +1747,15 @@ R36TAG2		DLOAD	RTB
 			SGNAGREE
 		STORE	DSPTEMX
 		EXIT
-		CAF	V06N90N		# DISPLAY Y, YDOT, AND PSI.
+		CAF	V06N90N		# DISPLAY Y , YDOT , AND PSI.
 		TC	BANKCALL
 		CADR	GOMARKF
 		TCF	ENDEXT		# TERMINATE
-		TCF	ENDEXT		# PROCEED, END OF PROGRAM
-		TCF	R36	+3	# REDISPLAY OUTPUT
+		TCF	ENDEXT		# PROCEED , END OF PROGRAM
+		TCF	R36 +3		# REDISPLAY OUTPUT
 LREGCHK		XCH	L
 		EXTEND
-		BZF	ENTTIM2		# L-REG ZERO, SET TIME = PRESENT TIME
+		BZF	ENTTIM2		# L-REG ZERO ,SET TIME = PRESENT TIME
 		XCH	L		# L-REG NON ZERO, TIME = ASTRO INPUT TIME
 		TCF	ASTROTIM
 ENTTIM2		TC	INTPRET