Merge remote-tracking branch 'upstream/master'

Comanche055/AGC_BLOCK_TWO_SELF-CHECK.agc

@@ -29,23 +29,21 @@
 #            Colossus 2A
 
 # Page 1394
-# PROGRAM DESCRIPTION				DATE:  20 DECEMBER 1967
-# PROGRAM NAME -- SELF-CHECK			LOG SECTION:  AGC BLOCK TWO SELF-CHECK
-# MOD NO -- 1					ASSEMBLY SUBROUTINE UTILITYM REV 25
-# MOD BY -- GAUNTT
+# PROGRAM DESCRIPTION				DATE  20 DECEMBER 1967
+# PROGRAM NAME - SELF-CHECK			LOG SECTION  AGC BLOCK TWO SELF-CHECK
+# MOD NO - 1					ASSEMBLY SUBROUTINE UTILITYM REV 25
+# MOD BY - GAUNTT
+#
 #
 # FUNCTIONAL DESCRIPTION
+#
 # 	PROGRAM HAS TWO MAIN PARTS. THE FIRST IS SELF-CHECK WHICH RUNS AS A ZERO PRIORITY JOB WITH NO CORE SET, AS
 # PART OF THE BACK-UP IDLE LOOP. THE SECOND IS SHOW-BANKSUM WHICH RUNS AS A REGULAR EXECUTIVE JOB WITH ITS OWN
 #  STARTING VERB.
-#
 # 	THE PURPOSE OF SELF-CHECK IS TO CHECK OUT VARIOUS PARTS OF THE COMPUTER AS OUTLINED BELOW IN THE OPTIONS.
-#
 # 	THE PURPOSE OF SHOW-BANKSUM IS TO DISPLAY THE SUM OF EACH BANK , ONE AT A TIME.
-#
 # 	IN ALL THERE ARE  7 POSSIBLE OPTIONS IN THIS BLOCK II VERSION OF SELF-CHECK. MORE DETAIL DESCRIPTION MAY BE
 # FOUND IN E-2065 BLOCK II AGC SELF-CHECK AND SHOW BANKSUM BY EDWIN D. SMALLY DECEMBER 1966, AND ADDENDA 2 AND 3.
-#
 # 	THE DIFFERENT OPTIONS ARE CONTROLLED BY PUTTING DIFFERENT NUMBERS IN THE SMODE REGISTER (NOUN 27). BELOW IS
 # A DESCRIPTION OF WHAT PARTS OF THE COMPUTER THAT ARE CHECKED BY THE OPTIONS, AND THE CORRESPONDING NUMBER, IN
 # OCTAL, TO LOAD INTO SMODE.
@@ -55,24 +53,29 @@
 # -0		SAME AS +-10 UNTIL AN ERROR IS DETECTED.
 # +0		NO CHECK, PUTS COMPUTER INTO THE BACKUP IDLE LOOP.
 #
+#
 # WARNINGS
 # 	USE OF E MEMORY RESERVED FOR SELF-CHECK (EVEN IN IDLE LOOP) AS TEMP STORAGE BY OTHER PROGRAMS IS DANGEROUS.
 # 	SMODE SET GREATER THAN OCT 10 PUTS COMPUTER INTO BACKUP IDLE LOOP.
 #
+#
 # CALLING SEQUENCE
+#
 # 	TO CALL SELF-CHECK KEY IN
 # 		V 21 N 27 E	OPTION NUMBER E
 # 	TO CALL SHOW-BANKSUM KEY IN
 # 		V 91 E		DISPLAYS FIRST BANK
 # 		V 33 E		PROCEED, DISPLAYS NEXT BANK
 #
+#
 # EXIT MODES, NORMAL AND ALARM
+#
 # 	SELF-CHECK NORMALLY CONTINUES INDEFINITELY UNLESS THERE IS AN ERROR DETECTED. IF SO + OPTION NUMBERS PUT
 # COMPUTER INTO BACKUP IDLE LOOP, - OPTION NUMBERS RESTART THE OPTION.
-#
 # 	THE -0 OPTION PROCEEDS FROM THE LINE FOLLOWING THE LINE WHERE THE ERROR WAS DETECTED.
+# 	SHOW-BANKSUM PROCEEDS UNTIL A TERMINATE IS KEYED IN (V 34 E). THE COMPUTER IS PUT INTO THE BACKUP IDLE LOOP
+#
 #
-#	SHOW-BANKSUM PROCEEDS UNTIL A TERMINATE IS KEYED IN (V 34 E).  THE COMPUTER IS PUT INTO THE BACKUP IDLE LOOP.
 #
 # OUTPUT
 # Page 1395
@@ -81,10 +84,10 @@
 # INFORMATION HE MAY KEY IN V 05 N 08 E, THE DSKY DISPLAY IN R1 WILL BE ADDRESS+1 OF WHERE THE ERROR WAS DETECTED,
 # IN R2 THE BBCON OF SELF-CHECK, AND IN R3 THE TOTAL NUMBER OF ERRORS DETECTED BY SELF-CHECK SINCE THE LAST MAN
 # INITIATED FRESH START (SLAP1).
-#
 # 	SHOW-BANKSUM STARTING WITH BANK 0 DISPLAYS IN R1 THE BANK SUM (A +-NUMBER EQUAL TO THE BANK NUMBER), IN R2
 # THE BANK NUMBER, AND IN R3 THE BUGGER WORD.
 #
+#
 # ERASABLE INITIALIZATION REQUIRED
 # 	ACCOMPLISHED BY FRESH START
 # 		SMODE SET TO +0
@@ -227,9 +230,7 @@ SELFCHK		TC	SMODECHK	# ** CHARLEY, COME IN HERE
 # Page 1398
 # SKEEP3 HOLDS LAST ADDRESS BEING CHECKED (HIGHEST ADDRESS).
 # SKEEP2 CONTROLS CHECKING OF NON-SWITCHABLE ERASABLE MEMORY WITH BANK NUMBERS IN EB.
-#
-# ERASCHK TAKES APPROXIMATELY 7 SECONDS.
-
+# ERASCHK TAKES APPROXMATELY 7 SECONDS
 ERASCHK		CA	S+1
 		TS	SKEEP2
 0EBANK		CA	S+ZERO
@@ -322,10 +323,8 @@ ELOOPFIN	RELINT
 		TC	E134567B	# GO TO EBANKS 1,3,4,5,6, AND 7
 		CA	ERASCON6	# END OF ERASCHK
 		TS	EBANK
-
 # CNTRCHK PERFORMS A CS OF ALL REGISTERS FROM OCT. 60 THROUGH OCT. 10.
 # INCLUDED ARE ALL COUNTERS, T6-1, CYCLE AND SHIFT, AND ALL RUPT REGISTERS
-
 CNTRCHK		CA	CNTRCON		# 00050
 CNTRLOOP	TS	SKEEP2
 		AD	SBIT4		# +10 OCTAL
@@ -336,7 +335,6 @@ CNTRLOOP	TS	SKEEP2
 		TC	CNTRLOOP
 
 # CYCLSHFT CHECKS THE CYCLE AND SHIFT REGISTERS
-
 CYCLSHFT	CA	CONC+S1		# 25252
 		TS	CYR		# C(CYR) = 12525
 		TS	CYL		# C(CYL) = 52524
@@ -357,7 +355,6 @@ CYCLSHFT	CA	CONC+S1		# 25252
 
 		INCR	SCOUNT +1
 		TC	SMODECHK
-
 # SKEEP1 HOLDS SUM
 # SKEEP2 HOLDS PRESENT CONTENTS OF ADDRESS IN ROPECHK AND SHOWSUM ROUTINES
 # SKEEP2 HOLDS BANK NUMBER IN LOW ORDER BITS DURING SHOWSUM DISPLAY
@@ -367,7 +364,7 @@ CYCLSHFT	CA	CONC+S1		# 25252
 # SKEEP4 HOLDS BANK NUMBER AND SUPER BANK NUMBER
 # SKEEP5 COUNTS 2 SUCCESSIVE TC SELF WORDS
 # SKEEP6 CONTROLS ROPECHK OR SHOWSUM OPTION
-# SKEEP7 CONTROLS WHEN ROUTINE IS IN COMMON FIXED OR FIXED FIXED BANKS
+# SKEEP7 CONTROLS WHEN ROUNTINE IS IN COMMON FIXED OR FIXED FIXED BANKS
 
 ROPECHK		CA	S-ZERO		# *
 		TS	SKEEP6		# * -0 FOR ROPECHK
@@ -514,5 +511,3 @@ BNKCHK		CS	L		# = - BANK NUMBER
 		EBANK=	NEWJOB
 LSTBNKCH	BBCON*			# * CONSTANT, LAST BANK.
 		SBANK=	LOWSUPER
-
-

Comanche055/ALARM_AND_ABORT.agc

@@ -31,7 +31,7 @@
 # Refer directly to the online document mentioned above for further
 # information.  Please report any errors to info@sandroid.org.
 
-# Page 1483
+# Page 1493
 # 	THE FOLLOWING SUBROUTINE MAY BE CALLED TO DISPLAY A NON-ABORTIVE ALARM CONDITION. IT MAY BE CALLED
 # EITHER IN INTERRUPT OR UNDER EXECUTIVE CONTROL.
 #
@@ -120,14 +120,15 @@ MULTFAIL	CA	L
 		BANK
 
 		COUNT	10/DSPLA
-PRIOLARM	INHINT			# * * * KEEP IN DISPLAY ROUTINE'S BANK
+
+PRIOLARM	INHINT			# * * * KEEP IN DISPLAY ROUTINES BANK
 		TS	L		# SAVE ALARM CODE
 
 		CA	BUF2		# 2 CADR OF PRIOLARM USER
 		TS	ALMCADR
 		CA	BUF2 +1
 		TC	PRIOENT +1	# * LEAVE L ALONE
--2SEC		DEC	-200		# *** DON'T MOVE
+-2SEC		DEC	-200		# *** DONT MOVE
 		CAF	V05N09
 		TCF	PRIODSPR
 
@@ -172,11 +173,12 @@ P00DOO		INHINT
 		INDEX	ALMCADR
 		CAF	0
 ABORT2		TC	BORTENT
-OCT77770	OCT	77770		# DON'T MOVE
+
+OCT77770	OCT	77770		# DONT MOVE
 		CA	V37FLBIT	# IS AVERAGE G ON
 		MASK	FLAGWRD7
 		CCS	A
-		TC	WHIMPER -1	# YES.  DON'T DO POODOO.  DO BAILOUT.
+		TC	WHIMPER -1	# YES.  DONT DO POODOO.  DO BAILOUT.
 
 		TC	DOWNFLAG
 		ADRES	STATEFLG
@@ -208,23 +210,20 @@ OCT217		OCT	00217
 		TC	ALMCADR		# RETURN TO USER
 
 DOALARM		EQUALS	ENDOFJOB
-
 # CALLING SEQUENCE FOR VARALARM
 #		CAF	(ALARM)
 #		TC	VARALARM
-# Page 1486
-
+#
 # VARALARM TURNS ON PROGRAM ALARM LIGHT BUT DOES NOT DISPLAY
-
 VARALARM	INHINT
 
-		TS	L		# SAVE USER'S ALARM CODE
+		TS	L		# SAVE USERS ALARM CODE
 
-		CA	Q		# SAVE USER'S Q
+		CA	Q		# SAVE USERS Q
 		TS	ALMCADR
 
 		TC	PRIOENT
-OCT14		OCT	14		# DON'T MOVE
+OCT14		OCT	14		# DONT MOVE
 
 		TC	ALMCADR		# RETURN TO USER
 

Comanche055/ANGLFIND.agc

@@ -107,7 +107,7 @@ SECAD		AXC,1	CALL		# MIS AND MFS ARRAYS CALCULATED		$2
 		DSU	DAD
 			DP1/4TH
 			MFI +8D
-		STORE	CAM		# CAM = (MFI0+MFI4+MFI8-1)/2 HALF-SCALE
+		STORE	CAM		# CAM = (MFI0+MFI4+MFI8-1)/2 HALF SCALE
 		ARCCOS
 		STORE	AM		# AM=ARCCOS(CAM)  (AM SCALED BY 2)
 		DSU	BPL
@@ -281,8 +281,8 @@ MXM3		SETPD			# MXM3 MULTIPLIES 2 3X3 MATRICES
 			0,1
 		GOTO
 			TRNSPSPD	# REVERSE ROWS AND COLS IN PD AND
-
 # RETURN WITH M1XM2 IN PD LIST
+
 TRANSPOS	SETPD	VLOAD*		# TRANSPOS TRANSPOSES A 3X3 MATRIX
 			0		#  AND LEAVES RESULT IN PD LIST
 			0,1		# MATRIX ADDRESS IN XR1
@@ -312,7 +312,6 @@ TRNSPSPD	DLOAD	PDDL		# ENTER WITH MATRIX IN PD LIST
 		RVQ			# RETURN WITH TRANSPOSED MATRIX IN PD LIST
 MINANG		DEC	.00069375
 MAXANG		DEC	.472222
-
 # GIMBAL LOCK CONSTANTS
 
 # D = MGA CORRESPONDING TO GIMBAL LOCK = 60 DEGREES
@@ -338,7 +337,7 @@ READCDUK	INHINT			# LOAD T(MPAC) WITH THE CURRENT CDU ANGLES
 		COUNT*	$$/KALC
 
 CDUTODCM	AXT,1	SSP		# SUBROUTINE TO COMPUTE  DIRECTION COSINE
-		OCT	3		# MATRIX RELATING S/C AXES TO STARLE
+		OCT	3		# MATRIX RELATING S/C AXES TO STABLE
 			S1		# MEMBER AXES FROM 3 CDU ANGLES IN T(MPAC)
 		OCT	1		# SET XR1, S1, AND PD FOR LOOP
 		STORE	7
@@ -430,14 +429,14 @@ ENDOCM		EQUALS
 
 # CALCULATION OF THE MATRIX DEL.......
 #
-#	*      *               __T           *
+#	*      *               --T           *
 #	DEL = (IDMATRIX)COS(A)+UU (1-COS(A))+UX SIN(A)		SCALED 1
 #
-#             _
+#             -
 #	WHERE U IS A UNIT VECTOR (DP SCALED 2) ALONG THE AXIS OF ROTATION.
-#	A IS THE ANGLE OF ROTATION (DP SCALED 2).
-#					   _
-#	UPON ENTRY THE STARTING ADDRESS OF U IS COF, AND A IS IN MPAC.
+#	A IS THE ANGLE OF ROTATION (DP SCALED 2)
+#					   -
+#	UPON ENTRY THE STARTING ADDRESS OF U IS COF, AND A IS IN MPAC
 
 		COUNT	22/KALC
 
@@ -479,7 +478,7 @@ DELCOMP		SETPD	PUSH		# MPAC CONTAINS THE ANGLE A
 			SIGNMPAC
 		STORE	DEL +16D	# UZ UZ(1-COS(A)) +COS(A)		$1
 
-# COMPUTE THE OFF-DIAGONAL TERMS OF DEL
+# COMPUTE THE OFF DIAGONAL TERMS OF DEL
 
 		DLOAD	DMP
 			COF
@@ -544,25 +543,18 @@ DELCOMP		SETPD	PUSH		# MPAC CONTAINS THE ANGLE A
 #
 #	C =COS(THETA)COS(PSI)
 #	 0
-#
 #	C =-COS(THETA)SIN(PSI)COS(PHI)+SIN(THETA)SIN(PHI)
 #	 1
-#
 #	C =COS(THETA)SIN(PSI)SIN(PHI)+SIN(THETA)COS(PHI)
 #	 2
-#
 #	C =SIN(PSI)
 #	 3
-#
 #	C =COS(PSI)COS(PHI)
 #	 4
-#
 #	C =-COS(PSI)SIN(PHI)
 #	 5
-#
 #	C =-SIN(THETA)COS(PSI)
 #	 6
-#
 #	C =SIN(THETA)SIN(PSI)COS(PHI)+COS(THETA)SIN(PHI)
 #	 7
 # Page 410
@@ -625,7 +617,7 @@ NOGO		INHINT
 		TC	STOPRATE
 
 					# TERMINATE MANEUVER
-		CAF	TWO		# NOTE: ALL RETURNS ARE NOW MADE VIA
+		CAF	TWO		# NOTE - ALL RETURNS ARE NOW MADE VIA
 		TC	WAITLIST	# GOODEND
 		EBANK=	BCDU
 		2CADR	ENDMANU

Comanche055/ASSEMBLY_AND_OPERATION_INFORMATION.agc

@@ -31,6 +31,8 @@
 # ASSEMBLY AND OPERATIONS INFORMATION
 # TAGS FOR RELATIVE SETLOC AND BLANK BANK CARDS
 # SUBROUTINE CALLS
+#
+#
 #	COMERASE
 #		ERASABLE ASSIGNMENTS
 #	COMAID
@@ -52,12 +54,12 @@
 #		SYSTEM TEST STANDARD LEAD INS
 #		IMU CALIBRATION AND ALIGNMENT
 #	COMEKISS
-#		GROUND TRACKING DETERMINATION PROGRAM -- P21
+#		GROUND TRACKING DETERMINATION PROGRAM - P21
 #		P34-P35, P74-P75
 #		R31
 #		P76
 #		R30
-#		STABLE ORBIT -- P38-P39
+#		STABLE ORBIT - P38-P39
 #	TROUBLE
 #		P11
 #		TP1 SEARCH
@@ -73,12 +75,9 @@
 #		CM BODY ATTITUDE
 #		P37,P70
 #		S-BAND ANTENNA FOR CM
-#		LUNAR LANDMARK SELECTION FOR CM
 #	TVCDAPS
 #		TVC INITIALIZE
-
 # Page 3
-
 #		TVC EXECUTIVE
 #		TVC MASSPROP
 #		TVC RESTARTS
@@ -120,16 +119,16 @@
 #		ALARM AND ABORT
 #		UPDATE PROGRAM
 #		RTB OP CODES
+#
+#
 #       SYMBOL TABLE LISTING
-# UNREFERENCED SYMBOL LISTING
+#       UNREFERANCED SYMBOL LISTING
 #       ERASABLE & EQUALS CROSS-REFERENCE TABLE
 #       SUMMARY OF SYMBOL TABLE LISTINGS
 #       MEMORY TYPE & AVAILABILITY DISPLAY
 #       COUNT TABLE
-# PARAGRAPHS GENERATED FOR THIS DISPLAY
-
+#       PARAGRAPHS GENERATED FOR THIS ASSEMBLY
 # Page 4
-
 #       OCTAL LISTING
 #       OCCUPIED LOCATIONS TABLE
 #       SUBROS CALLED & PROGRAM STATUS
@@ -184,30 +183,30 @@
 
 # EXTENDED VERBS
 
-# 40	ZERO CDU'S
-# 41	COARSE ALIGN CDU'S
-# 42	FINE ALIGN IMU'S
+# 40	ZERO CDU-S
+# 41	COARSE ALIGN CDU-S
+# 42	FINE ALIGN IMU-S
 # 43	LOAD IMU ATT ERROR METERS
 # 44	SET   SURFACE FLAG
 # 45	RESET SURFACE FLAG
 # 46	ESTABLISH G&C CONTROL
-# 47	MOVE LM STATE VECTOR INTO CM STATE VECTOR
+# 47	MOVE LM STATE VECTOR INTO CM STATE VECTOR.
 # 48	REQUEST DAP DATA LOAD ROUTINE (R03)
-# 49	REQUES CREW DEFINED MANEUVER ROUTINE (R62)
+# 49	REQUEST CREW DEFINED MANEUVER ROUTINE (R62)
 # 50	PLEASE PERFORM
 # 51	PLEASE MARK
 # 52	MARK ON OFFSET LANDING SITE
 # 53	PLEASE PERFORM ALTERNATE LOS MARK
-# 54	REQUEST RENDEZVOUS BACKUP SIGHTING MARK ROUTIEN (R23)
+# 54	REQUEST RENDEZVOUS BACKUP SIGHTING MARK ROUTINE (R23)
 # 55	INCREMENT AGC TIME (DECIMAL)
-# 56	TERMINATE TRACKING (P20 & P25)
+# 56	TERMINATE TRACKING (P20 + P25)
 # 57	REQUEST RENDEZVOUS SIGHTING MARK ROUTINE (R21)
 # 58	RESET STICK FLAG
 # 59	PLEASE CALIBRATE
 # 60	SET ASTRONAUT TOTAL ATTITUDE (N17) TO PRESENT ATTITUDE
 # 61	DISPLAY DAP ATTITUDE ERROR
-# 62	DISPLAY TOTAL ATTITUDE ERROR (W.R.T. N22 (THETAD))
-# 63	DISPLAY TOTAL ASTRONAUT ATTITUDE ERROR (W.R.T. N17 (CPHIX))
+# 62	DISPLAY TOTAL ATTITUDE ERROR (WRT N22 (THETAD))
+# 63	DISPLAY TOTAL ASTRONAUT ATTITUDE ERROR (WRT N17 (CPHIX))
 # 64	REQUEST S-BAND ANTENNA ROUTINE
 # 65	OPTICAL VERIFICATION OF PRELAUNCH ALIGNMENT
 # 66	VEHICLES ARE ATTACHED.  MOVE THIS VEHICLE STATE TO OTHER VEHICLE.
@@ -232,16 +231,14 @@
 # 85	REQUEST RENDEZVOUS PARAMETER DISPLAY NO. 2 (R34)
 # 86	REJECT RENDEZVOUS BACKUP SIGHTING MARK
 # 87	SET VHF RANGE FLAG
-
 # Page 7
-
 # 88	RESET VHF RANGE FLAG
 # 89	REQUEST RENDEZVOUS FINAL ATTITUDE ROUTINE (R63)
 # 90	REQUEST RENDEZVOUS OUT OF PLANE DISPLAY ROUTINE (R36)
 # 91	DISPLAY BANK SUM
 # 92	OPERATE IMU PERFORMANCE TEST (P07)
 # 93	ENABLE W MATRIX INITIALIZATION
-# 94	PERFORM SYSLUNAR ATTITUDE MANEUVER (P23)
+# 94	PERFORM CYSLUNAR ATTITUDE MANEUVER (P23)
 # 95	NO UPDATE OF EITHER STATE VECTOR (P20 OR P22)
 # 96	TERMINATE INTEGRATION AND GO TO P00
 # 97	PERFORM ENGINE FAIL PROCEDURE
@@ -249,18 +246,16 @@
 # 99	PLEASE ENABLE ENGINE
 
 # Page 8
-# IN THE FOLLOWING NOUN LIST THE 'NO LOAD' RESTRICTION MEANS THE NOUN
+# IN THE FOLLOWING NOUN LIST THE :NO LOAD: RESTRICTION MEANS THE NOUN
 # CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF
 # SCALE TYPE L (MIN/SEC) OR PP (2 INTEGERS).
-
 # IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22, OR 23
-# MAY BE USED TO LOAD ANY OF THE NOUN'S COMPONENTS WHICH ARE NOT OF THE
+# MAY BE USED TO LOAD ANY OF THE NOUN:S COMPONENTS WHICH ARE NOT OF THE
 # ABOVE SCALE TYPES.
+# THE :DEC ONLY: RESTRICTION MEANS ONLY DECIMAL OPERATION IS ALLOWED ON
+# EVERY COMPONENT IN THE NOUN. (NOTE THAT :NO LOAD: IMPLIES :DEC ONLY:.)
 
-# THE 'DEC ONLY' RESTRICTION MEANS ONLY DECIMAL OPERATION IS ALLOWED ON
-# EVERY COMPONENT IN THE NOUN.  (NOT THAT 'NO LOAD' IMLIES 'DEC ONLY'.)
-
-# NORMAL NOUNS				   COMPONENTS	SCALE & DECIMAL POINT	RESTRICTION
+# NORMAL NOUNS				   COMPONENTS	SCALE & DECIMAL POINT	RESTRICTIONS
 #
 # 00	NOT IN USE
 # 01	SPECIFY MACHINE ADDRESS (FRACTIONAL)	3COMP	.XXXXX FOR EACH
@@ -269,7 +264,7 @@
 # 04	SPARE
 # 05	ANGULAR ERROR/DIFFERENCE		1COMP	XXX.XX DEG
 # 06	OPTION CODE				2COMP	OCTAL ONLY FOR EACH
-# LOADING NOUN 07 WILL SET OR RESET SELECTED BITS IN ANY ERASABLE REGISTER.
+# LOADING NOUN 07 WILL SET OR RESET SELECTED BITS IN ANY ERASABLE REGISTER
 # 07	ECADR OF WORD TO BE MODIFIED		3COMP	OCTAL ONLY FOR EACH
 #	ONES FOR BITS TO BE MODIFIED
 #	1 TO SET OR 0 TO RESET SELECTED BITS
@@ -342,21 +337,21 @@
 
 # Page 11
 
-# MIXED NOUNS				   COMPONENTS	SCALE & DECIMAL POINT	RESTRICTION
+# MIXED NOUNS				   COMPONENTS	SCALE & DECIMAL POINT	RESTRICTIONS
 #
 # 40	TIME FROM IGNITION/CUTOFF		3COMP	XXBXX  MIN/SEC		NO LOAD, DEC ONLY
-#	VG						XXXX.X FT/SEC
+#	VG,						XXXX.X FT/SEC
 #	DELTA V (ACCUMULATED)				XXXX.X FT/SEC
-# 41	TARGET	AZIMUTH				2COMP	XXX.XX DEG
+# 41	TARGET	AZIMUTH,			2COMP	XXX.XX DEG
 #		ELEVATION				XX.XXX DEG
-# 42	APOGEE					3COMP	XXXX.X NAUT MI		DEC ONLY
-#	PERIGEE						XXXX.X NAUT MI
+# 42	APOGEE,					3COMP	XXXX.X NAUT MI		DEC ONLY
+#	PERIGEE,					XXXX.X NAUT MI
 #	DELTA V (REQUIRED)				XXXX.X FT/SEC
-# 43	LATITUDE				3COMP	XXX.XX DEG		DEC ONLY
-#	LONGITUDE					XXX.XX DEG
+# 43	LATITUDE,				3COMP	XXX.XX DEG		DEC ONLY
+#	LONGITUDE,					XXX.XX DEG
 #	ALTITUDE					XXXX.X NAUT MI
-# 44	APOGEE					3COMP	XXXX.X NAUT MI		NO LOAD, DEC ONLY
-#	PERIGEE						XXXX.X NAUT MI
+# 44	APOGEE,					3COMP	XXXX.X NAUT MI		NO LOAD, DEC ONLY
+#	PERIGEE,					XXXX.X NAUT MI
 #	TFF						XXBXX  MIN/SEC
 # 45	MARKS (VHF - OPTICS)			3COMP	+XXBXX			NO LOAD, DEC ONLY
 #	TFI OF NEXT BURN				XXBXX  MIN/SEC
@@ -365,67 +360,67 @@
 # 47	THIS VEHICLE WEIGHT			2COMP	XXXXX. LBS		DEC ONLY
 #	OTHER VEHICLE WEIGHT				XXXXX. LBS
 # 48	PITCH TRIM				2COMP	XXX.XX DEG		DEC ONLY
-#	YAW TRIM					XXX.XX DEG
+#	YAW TRIM,					XXX.XX DEG
 # 49	DELTA R					3COMP	XXXX.X NAUT MI		DEC ONLY
 #	DELTA V						XXXX.X FT/SEC
 #	VHF OR OPTICS CODE				XXXXX.
-# 50	SPLASH ERROR				3COMP	XXXX.X NAUT MI		NO LOAD, DEC ONLY
-#	PERIGEE						XXXX.X NAUT MI
+# 50	SPLASH ERROR,				3COMP	XXXX.X NAUT MI		NO LOAD, DEC ONLY
+#	PERIGEE,					XXXX.X NAUT MI
 #	TFF						XXBXX  MIN/SEC
 # 51	S-BAND ANTENNA ANGLES PITCH		2COMP	XXX.XX DEG		DEC ONLY
 #			       YAW			XXX.XX DEG
 # 52	CENTRAL ANGLE OF ACTIVE VEHICLE		1COMP	XXX.XX DEG
-# 53	RANGE					3COMP	XXX.XX NAUT MI		DEC ONLY
-#	RANGE RATE					XXXX.X FT/SEC
+# 53	RANGE,					3COMP	XXX.XX NAUT MI		DEC ONLY
+#	RANGE RATE,					XXXX.X FT/SEC
 #	PHI						XXX.X DEG
-# 54	RANGE					3COMP	XXX.XX NAUT MI		DEC ONLY
-#	RANGE RATE					XXXX.X FT/SEC
+# 54	RANGE,					3COMP	XXX.XX NAUT MI		DEC ONLY
+#	RANGE RATE,					XXXX.X FT/SEC
 #	THETA						XXX.XX DEG
 # 55	PERIGEE CODE				3COMP	XXXXX.			DEC ONLY
 #	ELEVATION ANGLE					XXX.XX DEG
 #	CENTRAL ANGLE OF PASSIVE VEHICLE		XXX.XX DEG
-# 56	REENTRY ANGLE				2COMP	XXX.XX DEG		DEC ONLY
+# 56	REENTRY ANGLE,				2COMP	XXX.XX DEG		DEC ONLY
 #	DELTA V						XXXXX. FT/SEC
 # 57	DELTA R					1COMP	XXXX.X NAUT MI		DEC ONLY
 # 58	PERIGEE ALT (POST TPI)			3COMP	XXXX.X NAUT MI		DEC ONLY
 #	DELTA V TPI					XXXX.X FT/SEC
 #	DELTA V TPF					XXXX.X FT/SEC
-# 59	DELTA VELOCITY LOS			3COMP	XXXX.X FT/SEC FOR EACH	DEC ONLY
-# 60	GMAX					3COMP	XXX.XX G		DEC ONLY
+# 59	DELTA VELOCITY LOS			3COMP	XXXX.X FT/SEC FOR EA.	DEC ONLY
+# 60	GMAX,					3COMP	XXX.XX G		DEC ONLY
 
 # Page 12
 
-#	VPRED						XXXXX. FT/SEC
+#	VPRED,						XXXXX. FT/SEC
 #	GAMMA EI					XXX.XX DEG
-# 61	IMPACT LATITUDE				3COMP	XXX.XX DEG		DEC ONLY
-#	IMPACT LONGITUDE				XXX.XX DEG
+# 61	IMPACT LATITUDE,			3COMP	XXX.XX DEG		DEC ONLY
+#	IMPACT LONGITUDE,				XXX.XX DEG
 #	HEADS UP/DOWN					+/- 00001
-# 62	INERTIAL VEL MAG (VI)			3COMP	XXXXX. FT/SEC		DEC ONLY
-#	ALT RATE CHANGE (HDOT)				XXXXX. FT/SEC
+# 62	INERTIAL VEL MAG (VI),			3COMP	XXXXX. FT/SEC		DEC ONLY
+#	ALT RATE CHANGE (HDOT),				XXXXX. FT/SEC
 #	ALT ABOVE PAD RADIUS (H)			XXXX.X NAUT MI
-# 63	RANGE 297,431 TO SPLASH (RTGO)		3COMP	XXXX.X NAUT MI		NO LOAD, DEC ONLY
-#	PREDICTED INERT VEL (VIO)			XXXXX. FT/SEC
-#	TIME FROM 297,431 (TFE)				XXBXX  MIN/SEC
-# 64	DRAG ACCELERATION			3COMP	XXX.XX G		DEC ONLY
-#	INERTIAL VELOCITY (VI)				XXXXX. FT/SEC
+# 63	RANGE 297,431 TO SPLASH (RTGO),		3COMP	XXXX.X NAUT MI		NO LOAD, DEC ONLY
+#	PREDICTED INERT VEL (VIO),			XXXXX. FT/SEC
+#	TIME FROM 297,431 (TFE),			XXBXX  MIN/SEC
+# 64	DRAG ACCELERATION,			3COMP	XXX.XX G		DEC ONLY
+#	INERTIAL VELOCITY (VI),				XXXXX. FT/SEC
 #	RANGE TO SPLASH					XXXX.X NAUT MI
 # 65	SAMPLED AGC TIME			3COMP	00XXX. HRS		DEC ONLY
-#	(FETCHED IN INTERRUPT)				000XX. MIN
+#	 (FETCHED IN INTERRUPT)				000XX. MIN              MUST LOAD 3 COMPS
 #							0XX.XX SEC
-# 66	COMMAND BANK ANGLE (BETA)		3COMP	XXX.XX DEG		DEC ONLY
-#	CROSS RANGE ERROR				XXXX.X NAUT MI
+# 66	COMMAND BANK ANGLE (BETA),		3COMP	XXX.XX DEG		DEC ONLY
+#	CROSS RANGE ERROR,				XXXX.X NAUT MI
 #	DOWN RANGE ERROR				XXXX.X NAUT MI
-# 67	RANGE TO TARGET				3COMP	XXXX.X NAUT MI		DEC ONLY
-#	PRESENT LATITUDE				XXX.XX DEG
+# 67	RANGE TO TARGET,			3COMP	XXXX.X NAUT MI		DEC ONLY
+#	PRESENT LATITUDE,				XXX.XX DEG
 #	PRESENT LONGITUDE				XXX.XX DEG
-# 68	COMMAND BANK ANGLE (BETA)		3COMP	XXX.XX DEG		DEC ONLY
-#	INERTIAL VELOCITY (VI)				XXXXX. FT/SEC
+# 68	COMMAND BANK ANGLE (BETA),		3COMP	XXX.XX DEG		DEC ONLY
+#	INERTIAL VELOCITY (VI),				XXXXX. FT/SEC
 #      ALT RATE CHANGE (RDOT)				XXXXX. FT/SEC
 # 69   BETA					3COMP	XXX.XX DEG
 #      DL						XXX.XX G
 #      VL						XXXXX. FT/SEC
-# 70	STAR CODE				3COMP	OCTAL ONLY
-#	LANDMARK DATA					OCTAL ONLY
+# 70	STAR CODE,				3COMP	OCTAL ONLY
+#	LANDMARK DATA,					OCTAL ONLY
 #	HORIZON DATA					OCTAL ONLY
 # 71	STAR CODE				3COMP	OCTAL ONLY
 #	LANDMARK DATA					OCTAL ONLY
@@ -456,18 +451,18 @@
 # 84	DELTA V (OTHER VEHICLE)			3COMP	XXXX.X FT/SEC FOR EACH	DEC ONLY
 # 85	VG (BODY)				3COMP	XXXX.X FT/SEC FOR EACH	DEC ONLY
 # 86	DELTA V (LV)				3COMP	XXXXX. FT/SEC FOR EACH	DEC ONLY
-# 87	MARK DATA	SHAFT			2COMP	XXX.XX DEG
+# 87	MARK DATA	SHAFT,			2COMP	XXX.XX DEG
 #			TRUNION				XX.XXX DEG
 # 88	HALF UNIT SUN OR PLANET VECTOR		3COMP	.XXXXX FOR EACH		DEC ONLY
-# 89	LANDMARK	LATITUDE		3COMP	XX.XXX DEG		DEC ONLY
-#			LONGITUDE/2			XX.XXX DEG
+# 89	LANDMARK	LATITUDE,		3COMP	XX.XXX DEG		DEC ONLY
+#			LONGITUDE/2,			XX.XXX DEG
 #			ALTITUDE			XXX.XX NAUT MI
 # 90	Y					3COMP	XXX.XX NM		DEC ONLY
 #	Y DOT						XXXX.X FPS
 #	PSI						XXX.XX DEG
-# 91	OCDU ANGLES	SHAFT			2COMP	XXX.XX DEG
+# 91	OCDU ANGLES	SHAFT,			2COMP	XXX.XX DEG
 #			TRUNION				XX.XXX DEG
-# 92	NEW OPTICS ANGLES	SHAFT		2COMP	XXX.XX DEG
+# 92	NEW OPTICS ANGLES	SHAFT,		2COMP	XXX.XX DEG
 #				TRUNON			XX.XXX DEG
 # 93	DELTA GYRO ANGLES			3COMP	XX.XXX DEG FOR EACH
 # 94	NEW OPTICS ANGLES	SHAFT		2COMP	XXX.XX DEG
@@ -478,7 +473,7 @@
 # 98	SYSTEM TEST RESULTS AND INPUTS		3COMP	XXXXX.
 #							.XXXXX
 #							XXXXX.
-# 99	RMS IN POSITION				3COMP	XXX.XX NAUT MI		DEC ONLY
+# 99	RMS IN POSITION				3COMP	XXXXX.FT	        DEC ONLY
 #	RMS IN VELOCITY					XXXX.X FT/SEC
 #	RMS OPTION					XXXXX.
 
@@ -489,7 +484,7 @@
 # NOUN	        REGISTER	SCALE TYPE
 #
 # 00	NOT IN USE
-# 01	SPECIFY ADDRESS		H
+# 01	SPECIFY ADDRESS		B
 # 02	SPECIFY ADDRESS		C
 # 03	SPECIFY ADDRESS		D
 # 04	SPARE
@@ -723,7 +718,7 @@
 # -D-								     15
 # CDU DEGREES		XXX.XX DEGREES		SP	BIT 1 = 360/2   DEGREES
 #			(MAX 359.99)			(USES 15 BITS FOR MAGNI-
-#							TUDE AND 2'S COMP.)
+#							 TUDE AND 2-S COMP.)
 #
 # -E-								    14
 # ELEVATION DEGREES	XX.XXX DEGREES		SP	BIT 1 = 90/2   DEGREES
@@ -740,13 +735,13 @@
 #
 # -H-
 # DP DEGREES (360)	XXX.XX DEGREES		DP	BIT 1 OF LOW REGISTER =
-#			(MAX 359.99)			     28
-#							360/2   DEGREES
+#			        			     28
+#			(MAX 359.99)			360/2   DEGREES
 #
 # -J-								    15
 # Y OPTICS DEGREES	XX.XXX DEGREES		SP	BIT 1 = 90/2   DEGREES
 #			(BIAS OF 19.775			(USES 15 BITS FOR MAGNI-
-#			DEGREES ADDED FOR		TUDE AND S'S COMP.)
+#			DEGREES ADDED FOR		TUDE AND 2-S COMP.)
 #			DISPLAY, SUBTRACTED
 #			FOR LOAD.)
 #			NOTE: NEGATIVE NUM-
@@ -800,7 +795,7 @@
 #
 # -Q-
 # POSITION 4		XXXX.XX NAUTICAL MILES	DP	BIT 1 OF LOW REGISTER =
-#							2 METERS.
+#							2 METERS
 #
 # -S-
 # VELOCITY 3		XXXX.X FT/SEC		DP	BIT 1 OF HIGH REGISTER =
@@ -836,15 +831,15 @@
 # -LL-
 # POSITION6		XXXX.X NAUT MI		DP	BIT 1 OF LOW REG =
 #									    -28
-#							(6,373,338)(2(PI))x2
+#							(6,373,338)(2(PI))X2
 #							-----------------------
 #								 1852
-#							NAUT MI.
+#							NAUT. MI.
 #
 # -MM-
 # DRAG ACCELERATION	XXX.XX G		DP	BIT 1 OF LOW REGISTER =
 #			MAX (024.99)			    -28
-#							25x2    G
+#							25X2    G
 #
 # -PP-
 # 2 INTEGERS		+XXBYY			DP	BIT 1 OF HIGH REGISTER =
@@ -852,8 +847,8 @@
 #			POSITION.  DECIMAL		BIT 1 OF LOW REGISTER =
 #			ONLY, DISPLAY, OR		 1 UNIT OF YY
 #			MONITOR ONLY. CANNOT		(EACH REGISTER MUST
-#			BE LOADED.)			LESS THAN 100.)
-#			(MAX 99B99)
+#			BE LOADED.)                     CONTAIN A POSITIVE INTEGER
+#			(MAX 99B99)                      LESS THAN 100)
 #
 # -UU-
 # VELOCITY/2VS		XXXXX. FEET/SEC		DP	FRACTIONAL PART OF
@@ -865,15 +860,15 @@
 # -VV-
 # POSITION8		XXXX.X NAUT MI		DP	BIT 1 OF LOW REGISTER =
 #									 -28
-#							4 x 6,373,338 x 2
+#							4 X 6,373,338 X 2
 #							--------------------
 #							      1852
 #							NAUT MI.
 #
 # -XX-
-# POSITION 9		XXX.XX NAUT MI		DP	BIT 1 OF LOW REGISTER =
-#			(MAX 283.09)			 -9
-#							2   METERS.
+# POSITION 9		XXXXX. FEET		DP	BIT 1 OF LOW REGISTER =
+#							 -9
+#							2   METERS
 #
 # -YY-
 # VELOCITY 4		XXXX.X FEET/SEC		DP	FRACTIONAL PART OF
@@ -884,14 +879,13 @@
 #							 -14
 #							2    UNITS
 
-
-# THAT'S ALL ON THE NOUNS.
+# THAT-S ALL ON THE NOUNS.
 
 # Page 23
 
 # ALARM CODES FOR 504
 
-# REPORT DEFICIENCIES TO JOHN SUTHERLAND:  MIT 617-864-6900 X1458
+# REPORT DEFICIENCIES TO JOHN SUTHERLAND @ MIT 617-864-6900 X1458
 
 # *9		*18						*60			                *25  COLUMN
 #
@@ -899,7 +893,7 @@
 #
 # 00110		NO MARK SINCE LAST MARK REJECT			SXTMARK			                ALARM
 # 00112		MARK NOT BEING ACCEPTED				SXTMARK			                ALARM
-# 00113		NO NBITS					SXTMARK			ALARM
+# 00113		NO INBITS					SXTMARK			                ALARM
 # 00114		MARK MADE BUT NOT DESIRED			SXTMARK			                ALARM
 # 00115		OPTICS TORQUE REQUESTWITH SWITCH NOT AT	        EXT VERB OPTICS CDU	                ALARM
 # 		 CGC
@@ -908,22 +902,21 @@
 # 00117		OPTICS TORQUE REQUEST WITH OPTICS NOT		EXT VERB OPTICS CDU	                ALARM
 #		 AVAILABLE (OPTIND=-0)
 # 00120		OPTICS TORQUE REQUEST WITH OPTICS		T4RUPT			                ALARM
-#			NOT ZEROED.
+#		 NOT ZEROED
 # 00121		CDUS NO GOOD AT TIME OF MARK			SXTMARK			                ALARM
 # 00122		MARKING NOT CALLED FOR				SXTMARK			                ALARM
 # 00124		P17 TPI SEARCH - NO SAFE PERICTR HERE.		TPI SEARCH		                ALARM
 # 00205		BAD PIPA READING				SERVICER		                ALARM
 # 00206		ZERO ENCODE NOT ALLOWED WITH COARSE ALIGN	IMU MODE SWITCHING	                ALARM
-# 			+ GIMBAL LOCK.
+# 		 + GIMBAL LOCK
 # 00207		ISS TURNON REQUEST NOT PRESENT FOR 90 SEC	T4RUPT			                ALARM
-# 00210		IMU NOT OPERATING				IMU MODE SWITCH,	ALARM, VARALARM
-#								IMU-2, R02, P51
+# 00210		IMU NOT OPERATING				IMU MODE SWITCH, IMU-2, R02, P51        ALARM,VARALARM
 # 00211		COARSE ALIGN ERROR - DRIVE > 2 DEGREES		IMU MODE SWITCH		                ALARM
 # 00212		PIPA FAIL BUT PIPA IS NOT BEING USED		IMU MODE SWITCH,T4RUPT	                ALARM
 # 00213		IMU NOT OPERATING WITH TURN-ON REQUEST		T4RUPT			                ALARM
 # 00214		PROGRAM USING IMU WHEN TURNED OFF		T4RUPT			                ALARM
 # 00215		PREFERRED ORIENTATION NOT SPECIFIED		P52,P54			                ALARM
-# 00217		BAD RETURN FROM STALL ROUTINES			CURTAINS		ALARM2
+# 00217		BAD RETURN FROM STALL ROUTINES.			CURTAINS		                ALARM2
 # 00220		IMU NOT ALIGNED - NO REFSMMAT			R02,P51			                VARALARM
 # 00401		DESIRED GIMBAL ANGLES YIELD GIMBAL LOCK		IMF ALIGN, IMU-2	                ALARM
 # 00404		TARGET OUT OF VIEW - TRUN ANGLE > 90 DEG	R52			                PRIOLARM
@@ -933,8 +926,8 @@
 # 00421		W-MATRIX OVERFLOW				INTEGRV			                ALARM
 # 00430	     *	INTEG. ABORT DUE TO SUBSURFACE S. V.		ALL CALLS TO INTEG	                POODOO
 # 00600		IMAGINARY ROOTS ON FIRST ITERATION		P32, P72		                VARALARM
-# 00601		PERIGEE ALTITUDE LT PMIN1			P32,P72			VARALARM
-# 00602		PERIGEE ALTITUDE LT PMIN2			P32,P72			VARALARM
+# 00601		PERIGEE ALTITUDE LT PMIN1			P32,P72,		                VARALARM
+# 00602		PERIGEE ALTITUDE LT PMIN2			P32,P72,		                VARALARM
 # 00603		CSI TO CDH TIME LT PMIN22			P32,P72,P33,P73		                VARALARM
 # 00604		CDH TO TPI TIME LT PMIN23			P32,P72			                VARALARM
 # 00605		NUMBER OF ITERATIONS EXCEEDS LOOP MAXIMUM	P32,P72,P37		                VARALARM
@@ -965,7 +958,7 @@
 # 01210	     *	TWO PROGRAMS USING DEVICE AT SAME TIME		IMU MODE SWITCH		                P00DOO
 # 01211      *	ILLEGAL INTERRUPT OF EXTENDED VERB		SXTMARK			                BAILOUT
 # 01301		ARCSIN-ARCCOS ARGUMENT TOO LARGE		INTERPRETER		                ALARM
-# 01302      *	SQRT CALLED WITH NEGATIVE ARGUMENT. ABORT.	INTERPRETER		P00DOO
+# 01302      *	SQRT CALLED WITH NEGATIVE ARGUMENT.ABORT	INTERPRETER		                P00DOO
 # 01407		VG INCREASING					S40.8			                ALARM
 # 01426		IMU UNSATISFACTORY				P61, P62			        ALARM
 # 01427		IMU REVERSED					P61, P62			        ALARM
@@ -975,7 +968,7 @@
 # 01520		V37 REQUEST NOT PERMITTED AT THIS TIME		V37			                ALARM
 # 01521	     *	P01 ILLEGALLY SELECTED				P01, P07                                POODOO
 # 01600		OVERFLOW IN DRIFT TEST				OPT PRE ALIGN CALIB	                ALARM
-# 01601      *	BAD IMU TORQUE - ABORT.				OPT PRE ALIGN CALIB	ALARM
+# 01601      	BAD IMU TORQUE  				OPT PRE ALIGN CALIB	                ALARM
 # 01602		BAD OPTICS DURING VERIFICATION			OPTALGN CALIB (CSM)	                ALARM
 # 01703		INSUF. TIME FOR INTEG., TIG WAS SLIPPED		R41			                ALARM
 # 03777		ICDU FAIL CAUSED THE ISS WARNING		T4RUPT			                VARALARM
@@ -983,15 +976,14 @@
 # 07777		IMU FAIL CAUSED THE ISS WARNING			T4RUPT			                VARALARM
 # 10777		IMU , PIPA FAILS CAUSED THE ISS WARNING		T4RUPT			                VARALARM
 # 13777		IMU , ICDU FAILS CAUSED THE ISS WARNING		T4RUPT			                VARALARM
-# 14777		IMU, ICDU, PIPA FAILS CAUSED THE ISS WARNING	T4RUPT			VARALARM
-#
+# 14777		IMU,ICDU,PIPA FAILS CAUSED THE ISSWNING	        T4RUPT			                VARALARM
 # 	     *	INDICATES ABORT TYPE.ALL OTHERS ARE NON-ABORTIVE
 
 # Page 25
 
 #               CHECKLIST CODES FOR 504
 
-# PLEASE REPORT ANY DEFICIENCIES IN THIS LIST TO JOHN SUTHERLAND.
+#               PLEASE REPORT ANY DEFICIENCIES IN THIS LIST TO JOHN SUTHERLAND
 
 # *9		*17		*26  COLUMN
 #
@@ -1006,8 +998,7 @@
 # 00203		SWITCH		TO CMC-AUTO
 # 00204		PERFORM		SPS GIMBAL TRIM
 # 00403		SWITCH		OPTICS TO MANUAL OR ZERO
-#
-#		SWITCH DENOTES CHANGE OF POSITION OF A CONSOLE SWITCH
+#		                  SWITCH DENOTES CHANGE POSITION OF A CONSOLE SWITCH
 #		                  PERFORM DENOTES START OF END OF A TASK
 #		                  KEY IN DENOTES KEY IN OF DATA THRU THE DSKY
 
@@ -1015,7 +1006,7 @@
 
 #          OPTION CODES FOR 504
 
-# PLEASE REPORT ANY DEFICIENCIES IN THIS LIST TO JOHN SUTHERLAND.
+#          PLEASE REPORT ANY DEFICIENCIES IN THIS LIST TO JOHN SUTHERLAND
 
 # THE SPECIFIED OPTION CODES WILL BE FLASHED IN COMPONENT R1 IN
 # CONJUNCTION WITH VERB04NOUN06 TO REQUEST THE ASTRONAUT TO LOAD INTO
@@ -1038,4 +1029,3 @@
 # 00011		SPEC. SEPARATION MONITOR PHASE	1=DELTAV 2=STATE VECTOR UPDATE	P46		LUMINARY
 # 00012		SPECIFY CSM ORBIT OPTION	1=NO ORBIT CHANGE 2=CHANGE	P22		LUMINARY
 #						ORBIT TO PASS OVER LM
-

Comanche055/P34-35_P74-75.agc

@@ -62,7 +62,7 @@
 #			HORIZONTAL PLANE DEFINED BY THE ACTIVE VEHICLE POSITION.
 #		(B)	THE TIME BETWEEN CDH IGNITION AND TPI IGNITION WAS
 #			COMPUTED TO BE GREATER THAN 10 MINUTES.
-#		(C)	THE VARIATION OF TEH ALTITUDE DIFFERENCE BETWEEN THE
+#		(C)	THE VARIATION OF THE ALTITUDE DIFFERENCE BETWEEN THE
 #			ORBITS WAS MINIMIZED.
 #		(D)	THE PERICENTER ALTITUDES OF ORBITS FOLLOWING CSI AND
 #			CDH WERE COMPUTED TO BE GREATER THAN 35,000 FT FOR LUNAR
@@ -86,7 +86,7 @@
 #		PREVIOUS SELECTION OF P20.  RADAR SIGHTING MARKS WILL BE MADE
 #		AUTOMATICALLY APPROXIMATELY ONCE A MINUTE WHEN ENABLED BY THE
 #		TRACK AND UPDATE FLAGS (SEE P20).  THE RENDEZVOUS TRACKING
-#		MARK COUNTER IS ZEROED BY TEH SELECTION OF P20 AND AFTER EACH
+#		MARK COUNTER IS ZEROED BY THE SELECTION OF P20 AND AFTER EACH
 #		THRUSTING MANEUVER.
 #	(5)	THE ISS NEED NOT BE ON TO COMPLETE THIS PROGRAM.
 #	(6)	THE OPERATION OF THE PROGRAM UTILIZES THE FOLLOWING FLAGS --
@@ -104,7 +104,7 @@
 #			PROGRAM SELECTED AFTER COMPLETION OF THIS PROGRAM.
 #
 #	(7)	ONCE THE PARAMETERS REQUIRED FOR COMPUTATION OF THE MANEUVER
-#		HAVE BEEN COMPLETELY SPECIFIED, TEH VALUE OF THE ACTIVE
+#		HAVE BEEN COMPLETELY SPECIFIED, THE VALUE OF THE ACTIVE
 #		VEHICLE CENTRAL ANGLE OF TRANSFER IS COMPUTED AND STORED.
 #		THIS NUMBER WILL BE AVAILABLE FOR DISPLAY TO THE ASTRONAUT
 #		THROUGH THE USE OF V06N52.

Comanche055/P51-P53.agc

@@ -1787,7 +1787,7 @@ S52.2.1		AXC,1	AXC,2
 # TARG1 AND TARG2 FLAGS ARE LOOKED AT TO DETERMINE IF THE TARGET IS THE
 # LEM, STAR, OR LANDMARK.  IN CASE OF LEM OR LMK, THE PRESENT TIME PLUS
 # 2 SECONDS IS SAVED IN AOPTIME (ALIAS STARAD, +1).  IF THE LEM IS 
-# THE TARGET THEN CONIC UPDATES OF TEH CSM AND LEM ARE MADE TO
+# THE TARGET THEN CONIC UPDATES OF THE CSM AND LEM ARE MADE TO
 # THE TIME IN AOPTIME.  THE UNIT OF THE DIFFERENCE OF LEM AND CSM
 # POSITION VECTORS BECOMES THE REFERENCE SIGHTING VECTOR USED IN THE
 # COMMON PART OF THE THIS PROGRAM.

Comanche055/PHASE_TABLE_MAINTENANCE.agc

@@ -96,7 +96,7 @@ DSPMMJOB	EQUALS	DSPMMJB
 #
 # THIS INFORMATION IS PUT INTO THE OCTAL WORD AFTER TC PHASCHNG AS FOLLOWS
 #	TL0 00P PPP PPP GGG
-# WHERE EACH LETTER OR NUMBER STANTS FOR A BIT.  THE G'S STAND FOR THE GROUP, OCTAL 1-7, THE P'S FOR THE PHASE,
+# WHERE EACH LETTER OR NUMBER STANDS FOR A BIT.  THE G'S STAND FOR THE GROUP, OCTAL 1-7, THE P'S FOR THE PHASE,
 # OCTAL 0 - 127.  0'S MUST BE 0.  IF ONE WISHES TO HAVE THE TBASE OF GROUP G TO BE SET AT THIS TIME,
 # T IS SET TO 1, OTHERWISE IT IS SET TO 0.  SIMILARLY IF ONE WISHES TO SET LONGBASE, THEN L IS SET TO 1, OTHERWISE
 # IT IS SET TO 0.  SOME EXAMPLES,

Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.agc

@@ -3471,7 +3471,7 @@ FLASHOFF	CS	BIT6		# TURN OFF V/N FLASH
 # HAS BEEN REMOVED AND THE INTERNAL USER NO LONGER HAS THE PROTECTION THIS
 # OFFERED.
 #
-# THERE ARE TWO WAYS A JOB CAN BE PUT TO SLEEP BY TEH KEYBOARD + DISPLAY
+# THERE ARE TWO WAYS A JOB CAN BE PUT TO SLEEP BY THE KEYBOARD + DISPLAY
 # PROGRAM.	1)	BY ENDIDLE
 #		2)	BY NVSUBUSY
 # THE BASIC CONVENTION IS THAT ONLY ONE JOB WILL BE PERITTED ASLEEP VIA

Luminary099/AGC_BLOCK_TWO_SELF_CHECK.agc

@@ -469,7 +469,7 @@ CHKSUPR		MASK	HI5
 		ADS	SKEEP4
 		TC	GONXTBNK
 NXTSUPR		AD	SUPRCON		# SET BNK 30 + INCR SUPR BNK AND CANCEL
-		ADS	SKEEP4		# ERC BIT OF TEH 37 TO 40 ADVANCE.
+		ADS	SKEEP4		# ERC BIT OF THE 37 TO 40 ADVANCE.
 GONXTBNK	CCS	SKEEP7
 		TC	COMMFX
 		CA	S+1

Luminary099/DAP_INTERFACE_SUBROUTINES.agc

@@ -70,7 +70,7 @@
 #	PFLITEDB -- SET DEADBAND TO 1.0 DEGREE AND ZERO THE COMMANDED ATTITUDE CHANGE AND COMMANDED RATE
 #
 #	ALL ENTRIES SET UP A NOVAC JOB TO DO 1/ACCS SO THAT THE TJETLAW SWITCH CURVES ARE POSITIONED TO
-#	REFLECT TEH NEW DEADBAND.  IT SHOULD BE NOTED THAT THE DEADBAND REFERS TO THE ATTITUDE IN THE P-, U-, AND V-AXES.
+#	REFLECT THE NEW DEADBAND.  IT SHOULD BE NOTED THAT THE DEADBAND REFERS TO THE ATTITUDE IN THE P-, U-, AND V-AXES.
 #
 # SUBROUTINE CALLED:	NOVAC
 #