Fixed typos

Comanche055/AGC_BLOCK_TWO_SELF-CHECK.s

@@ -82,7 +82,7 @@
 #	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 WTIH BANK 0 DISPLAYS IN R1 THE BANK SUM (A +-NUMBER EQUAL TO THE BANK NUMBER), IN R2
+#	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

Comanche055/ASSEMBLY_AND_OPERATION_INFORMATION.s

@@ -250,7 +250,7 @@
 
 # Page 8
 # IN THE FOLLOWING NOUN LIST THE 'NO LOAD' RESTRICTION MEANS THE NOUN
-# CONTAINS AT LEAST ONE COMONENT WHICH CANNOT BE LOADED, I.E. OF
+# 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
@@ -1033,7 +1033,7 @@
 # 00005		SPECIFY SOR PHASE		1=FIRST 2=SECOND		P38		COLOSSUS + LUMINARY
 # 00006		SPECIFY RR COARSE ALIGN OPTION	1=LOCKON 2=CONTINUOUS DESIG.	V41N72		SUNDANCE + LUMINARY
 # 00007		SPECIFY PROPULSION SYSTEM	1=SPS 2=RCS			P37		COLOSSUS
-# 00010		SPECIFY ALIGNEMENT MODE		0=ANY TIME 1=REFSMMAT + G	P57		LUMINARY	
+# 00010		SPECIFY ALIGNMENT MODE		0=ANY TIME 1=REFSMMAT + G	P57		LUMINARY	
 #						2=TWO BODIES 3=ONE BODY + G
 # 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

Comanche055/AUTOMATIC_MANEUVERS.s

@@ -490,7 +490,7 @@ ZEROCMDS	CAF	ZERO
 		TS	TAU1
 		TS	TAU2
 T6PROG		EXTEND			# WHEN THE ROTATION COMMANDS (TAUS)
-		DCA	JETADDR		# HAVE BEEN DETERINED
+		DCA	JETADDR		# HAVE BEEN DETERMINED
 		DXCH	T5LOC		# RESET T5LOC FOR PHASE3
 		TCF	RESUME
 

Comanche055/CM_ENTRY_DIGITAL_AUTOPILOT.s

@@ -32,7 +32,7 @@
 
 # Page 1063
 # SUBROUTINE TO READ GIMBAL ANGLES AND FORM DIFFERENCES.  GIMBAL ANGLES ARE SAVED IN 2'S COMPLEMENT, BUT THE
-# DIFFERENECES ARE IN 1'S COMP.  ENTER AND READ ANGLES EACH .1 SEC.
+# DIFFERENCES ARE IN 1'S COMP.  ENTER AND READ ANGLES EACH .1 SEC.
 #
 #	CM/DSTBY = 1 FOR DAP OPERATION
 #	CM/DSTBY = 0 TO TERMINATE DAP OPERATION
@@ -289,7 +289,7 @@ T5IDLER1	2CADR	T5IDLOC
 
 # Page 1070
 # THIS SECTION CALCULATES THE ANGULAR BODY RATES EACH .1 SEC.  THE ANGULAR RATES ARE THOSE ALONG THE BODY AXES
-# XB, YB, ZB, AND ARE NORMALLY DESIGNATED P, Q, R.	REQIREMENT:  TEMPORARILY ERASE.  JETEM, JETEM +1
+# XB, YB, ZB, AND ARE NORMALLY DESIGNATED P, Q, R.	REQUIREMENT:  TEMPORARILY ERASE.  JETEM, JETEM +1
 #
 # SINCE RESTARTS ZERO THE JET OUTPUT CHANNELS, NO ATTEMPT IS MADE TO RESTART THE ENTRY DAPS.  THAT IS,
 # THE 0.1 SEC DAPS WILL MISS A CYCLE, AND WILL PICK UP AT THE NEXT 0.1 SEC UPDATE.  MOST OF THE TIME THE 2 SEC
@@ -1079,7 +1079,7 @@ TIMETST5	CS	ONE
 
 # SECTION  JETCALL  EXAMINES CONTENTS OF JET TIMES IN LIST, ESTABLISHES WTLST ENTRIES, AND EXECUTES CORRESPONDING
 # JET CODES.  A POSITIVE NZ NUMBER IN A TIME REGISTER INDICATES THAT A WTLST CALL IS TO BE MADE, AND ITS JET BITS
-# EXECUTED.  A +0 INDICATES THAT THE TIME INTERVAL DOES NOT APPLY, BUT THE CORRESPOINDING JET BITS ARE TO BE
+# EXECUTED.  A +0 INDICATES THAT THE TIME INTERVAL DOES NOT APPLY, BUT THE CORRESPONDING JET BITS ARE TO BE
 # EXECUTED.  A NEG NUMBER INDICATES THAT THE TIME INTERVAL HAS BEEN PROCESSED.  IN EVENT OF +0 OR -1, THE 
 # SUBSEQUENT TIME REGISTER IS EXAMINED FOR POSSIBLE ACTION.  THUS JET BITS TO BE EXECUTED MAY COME FROM MORE
 # THAN ONE REGISTER.

Comanche055/CONIC_SUBROUTINES.s

@@ -106,7 +106,7 @@
 #							RESPECTIVELY, IS THE CENTRAL BODY
 #	TAU		+28			DESIRED TRANSFER TIME IN CENTISECONDS (DP)
 #							MAY BE POS OR NEG AND ABSOLUTE VALUE MAY BE GREATER OR LESS THAN ONE ORBITAL PERIOD.
-#	XKEPNEW		+17 FOR EARTH		DP GUESS OF ROOT X OF KEPLERS EQN IN SQRT(METERS).SIGN SHOULD AGREE WTIH THAT OF TAU.
+#	XKEPNEW		+17 FOR EARTH		DP GUESS OF ROOT X OF KEPLERS EQN IN SQRT(METERS).SIGN SHOULD AGREE WITH THAT OF TAU.
 #			+16 FOR MOON			AND ABS VALUE SHOULD BE LESS THAN THAT CORRESPONDING TO A PERIOD, VIZ, 2PI SQRT(SEMI-
 #							MAJOR AXIS), FOR SPEED OF CONVERGENCE, BUT IF EITHER CONDITION FAILS, XKEPNEW IS RESET
 #							BY KEPLER TO A POOR BUT VALID GUESS.
@@ -286,7 +286,7 @@
 #	STATE IS TO BE UPDATED ALONG A CONIC TRAJECTORY, CALCULATES THE CORRESPONDING TIME-OF-FLIGHT AND, IN ADDITION,
 #	PROVIDES THE OPTION OF COMUTING 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 SIMPLE ADDITIONS TO THE MUTABLE WTIHOUT 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.
 #
 # THE RESTRICTIONS ARE --
@@ -1776,7 +1776,7 @@ MUTABLE		2DEC*	3.986032 E10 B-36*	# MUE
 
 LDPOSMAX	EQUALS 	LODPMAX			# DPPOSMAX IN LOW MEMORY.
 
-# ERASABLE ASSIGNEMENTS
+# ERASABLE ASSIGNMENTS
 
 # KEPLER SUBROUTINE
 

Comanche055/CSM_GEOMETRY.s

@@ -33,7 +33,7 @@
 		BANK
 
 # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT
-# VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WTIH THE SEXTANT LINE OF SIGHT.
+# VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WITH THE SEXTANT LINE OF SIGHT.
 #
 # THE INPUTS ARE:  1) THE SEXTAND SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE
 # MARK VAC AREA.  2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR

Comanche055/DISPLAY_INTERFACE_ROUTINES.s

@@ -485,7 +485,7 @@
 #	5.  IT IS ALWAYS GOOD PRACTICE TO TERMINATE AN EXTENDED VERB BEFORE ASKING FOR ANOTHER ONE OR THE SAME ONE
 #	    OVER AGAIN.
 #
-# SPECIAL CONSIDERATONS --
+# SPECIAL CONSIDERATIONS --
 # Page 1464
 #	1.  MPAC +2 SAVED ONLY IN MARK DISPLAYS
 #	2.  GODSP(R), REGODSP(R), GOMARK(R) ALWAYS TURN ON THE FLASH IF ENTERED WITH A PASTE VERB REQUEST.
@@ -638,7 +638,7 @@ COPYPACS	INDEX	COPINDEX
 
 		TC	Q
 
-# PINCHEK CHECKS TO SEE IF THE CURRENT MARK REQUEST IS MADE BY THE ASTRONAUT WHILE INTERUPTING A GOPLAY DISPLAY
+# PINCHEK CHECKS TO SEE IF THE CURRENT MARK REQUEST IS MADE BY THE ASTRONAUT WHILE INTERRUPTING A GOPLAY DISPLAY
 # (A NORMAL OR A PRIO).  IF THE ASTRONAUT TRIES TO MARK DURING A PRIO, THE CHECK FAIL LIGHT GOES ON AND THE MARK
 # REQUEST IS ENDED.  IF HE TRIES TO MARK DURING A NORM, THE MARK IS ALLOWED.  IN THIS CASE THE NORM IS PUT TO SLEEP
 # UNTIL ALL MARKING IS FINISHED.

Comanche055/DOWN-TELEMETRY_PROGRAM.s

@@ -106,7 +106,7 @@
 # 1.	DOWNLISTS.  DOWNLISTS MUST BE COMPILED IN THE SAME BANK AS THE
 #	DOWN-TELEMETRY PROGRAM.  THIS IS DONE FOR EASE OF CODING, FASTER
 #	EXECUTION.
-# 2.	EACH DOWNLINK LIST CONSISTES OF A CONTROL LIST AND A NUMBER OF
+# 2.	EACH DOWNLINK LIST CONSISTS OF A CONTROL LIST AND A NUMBER OF
 #	SUBLISTS.
 # 3.	A SUBLIST REFERS TO A SNAPSHOT OR DATA COMMON TO THE SAME OR OTHER
 #	DOWNLINK LISTS.  ANY SUBLIST CONTAINING COMMON DATA NEEDS TO BE
@@ -122,7 +122,7 @@
 #		SAME AS ECADR, BUT USED WHEN THE WORD ADDRESSED IS THE LEFT
 #		HALF OF A DOUBLE-PRECISION WORD FOR DOWN TELEMETRY.
 #	B.	2DNADR - 6DNADR		N-WORD DOWNLIST ADDRESS, N = 2 - 6.
-#		SAME AS 1DNADR, BUT WTIH THE 4 UNUSED BITS OF THE ECADR FORMAT
+#		SAME AS 1DNADR, BUT WITH THE 4 UNUSED BITS OF THE ECADR FORMAT
 #		FILLED IN WITH 0001-0101.  USED TO POINT TO A LIST OF N DOUBLE-
 #		PRECISION WORDS, STORED CONSECUTIVELY, FOR DOWN TELEMETRY.
 #	C.	DNCHAN			DOWNLIST CHANNEL ADDRESS.
@@ -347,7 +347,7 @@ SUBLIST		EQUALS 	DNQ
 #	AFTER KEYING IN V74E THE CURRENT DOWNLIST WILL BE IMMEDIATELY TERMINATED AND THE DOWNLINK ERASABLE DUMP
 #	WILL BEGIN.
 #
-#	ONCE INITITIATED THE DOWNLINK ERASABLE DUMP CAN BE TERMINATED (AND INTERRUPTED DOWNLIST REINSTATED) ONLY
+#	ONCE INITIATED THE DOWNLINK ERASABLE DUMP CAN BE TERMINATED (AND INTERRUPTED DOWNLIST REINSTATED) ONLY
 #	BY THE FOLLOWING:
 #
 #	1.	A FRESH START

Comanche055/EXECUTIVE.s

@@ -47,7 +47,7 @@ NOVAC		INHINT
 		TS	EXECTEM1
 		TCF	NOVAC2		# ENTER EXECUTIVE BANK.
 
-# TO ENTER A JOB REQUEST REQUIREING A VAC AREA -- E.G., ALL (PARTIALLY) INTERPRETIVE JOBS.
+# TO ENTER A JOB REQUEST REQUIRING A VAC AREA -- E.G., ALL (PARTIALLY) INTERPRETIVE JOBS.
 
 FINDVAC		INHINT
 		TS	NEWPRIO
@@ -157,7 +157,7 @@ NOVAC2		CAF	ZERO		# NOVAC ENTERS HERE.  FIND A CORE SET.
 NOVAC3		TS	EXECTEM2
 		INDEX	LOCCTR
 		CCS	PRIORITY	# EACH PRIORITY REGISTER CONTAINS -0 IF
-		TCF	NEXTCORE	# THE CORESPONDING CORE SET IS AVAILABLE.
+		TCF	NEXTCORE	# THE CORRESPONDING CORE SET IS AVAILABLE.
 NO.CORES	DEC	6
 		TCF	NEXTCORE	# AN ACTIVE JOB HAS A POSITIVE PRIORITY
 					# BUT A DORMANT JOB'S PRIORITY IS NEGATIVE
@@ -319,7 +319,7 @@ JOBWAKE3	CAF	COREINC
 		ADS	LOCCTR
 		CCS	EXECTEM2
 		TCF	JOBWAKE4
-		CS	ONE		# EXIT IF SLEEPIG JOB NOT FOUND.
+		CS	ONE		# EXIT IF SLEEPING JOB NOT FOUND.
 		TS	LOCCTR
 		TCF	ENDFIND
 

Comanche055/FRESH_START_AND_RESTART.s

@@ -99,7 +99,7 @@
 #
 #	1.	INTIALIZE OUTBIT CHANNELS 11,12,13, AND 14
 #	2.	REPLACE ALL TASKS ON WAITLIST WITH ENDTASK
-#	3.	MAKE ALL EXECUTEVE REGISTERS AVAILABLE
+#	3.	MAKE ALL EXECUTIVE REGISTERS AVAILABLE
 #	4.	MAKE ALL VAC AREAS AVAILABLE
 #	5.	CLEAR DSKY REGISTERS
 #	6.	ZERO NUMEROUS SWITCHES
@@ -130,7 +130,7 @@
 #	B.	ALARMS
 #
 #		1107	PHASE TABLE ERROR
-#		1110	RESTART WTIH NO ACTIVE GROUPS
+#		1110	RESTART WITH NO ACTIVE GROUPS
 
 # Page 183
 		BANK	10

Comanche055/INTERPRETER.s

@@ -2626,7 +2626,7 @@ NORMTEST	CCS	CYL		# SEE IF ARGUMENT NOW NORMALIZED AT
 
 # Page 1187
 # TRIGONOMETRIC FUNCTION PACKAGE.
-#	THE FOLLOWING TRIGONOMETRIC FUNCTIONS ARE AVAIALABLE AS INTERPRETIVE OPERATIONS:
+#	THE FOLLOWING TRIGONOMETRIC FUNCTIONS ARE AVAILABLE AS INTERPRETIVE OPERATIONS:
 #	1.	SIN		COMPUTES (1/2)SINE(2 PI MPAC).
 #	2.	COS		COMPUTES (1/2)COSINE(2 PI MPAC).
 #	3.	ASIN		COMPUTES (1/2PI)ARCSINE(2 MPAC).

Comanche055/JET_SELECTION_LOGIC.s

@@ -365,7 +365,7 @@ NOACY		CA	RWORD1		# Y-TRANSLATION NOT ACCEPTED
 # FAILURES.  IF THERE ARE BD FAILURES, Z-TRANSLATION COMMANDS WILL BE IGNORED, IN WHICH CASE THE ASTRONAUT SHOULD
 # SWITCH TO AC ROLL.
 #
-# NOTE THAT IF ONE QUAD FAILS (E.G. B FAILED), Z-TRANSLATION IS STILL POSSIBLE AND THAT THE UNDESIREABLE ROLL
+# NOTE THAT IF ONE QUAD FAILS (E.G. B FAILED), Z-TRANSLATION IS STILL POSSIBLE AND THAT THE UNDESIRABLE ROLL
 # INTRODUCED BY THIS TRANSLATION WILL BE COMPENSATED BY THE TWO AC ROLL JETS ACTUATED BY THE AUTOPILOT LOGIC.
 #
 # 					   WORD MAKE UP....RTABLE
@@ -386,7 +386,7 @@ NOACY		CA	RWORD1		# Y-TRANSLATION NOT ACCEPTED
 # THIS WORD MAY THEN BE ADDED TO THE WORD SELECTED FROM THE YZ-TRANSLATION TABLE, WHICH HAS THE SAME TYPE OF
 # CODING AS ABOVE, AND THE NET ROLL DETERMINED BY SHIFTING THE RESULTANT WORD RIGHT 8 PLACES AND SUBTRACTING FOUR.
 #
-# THE WORD CORRESPONDING TO THE BD ROLL HAS A SIMILAR INTEPRETATION, EXCEPT THAT BITS 12, 13, 14 ARE CODED
+# THE WORD CORRESPONDING TO THE BD ROLL HAS A SIMILAR INTERPRETATION, EXCEPT THAT BITS 12, 13, 14 ARE CODED
 # (AS ABOVE) TO GIVE THE NET ROLL TORQUE.
 
 					# ROLL 		TRANS		QUADFAIL	BIAS

Comanche055/KALCMANU_STEERING.s

@@ -89,7 +89,7 @@ INCRDCDU	TS	KSPNDX
 		TCF	INCRDCDU	# LOOP FOR THREE AXES
 
 		RELINT		
-# COMPARE PRESENT TIME WTIH TIME TO TERMINATE MANEUVER
+# COMPARE PRESENT TIME WITH TIME TO TERMINATE MANEUVER
 
 TMANUCHK	TC	TIMECHK
 		TC	POSTJUMP

Comanche055/KEYRUPT_UPRUPT.s

@@ -127,7 +127,7 @@ ELRCODE		OCT	22
 # THE RECEPTION OF A BAD CODE (I.E., CCC FAILURE) LOCKS OUT FURTHER UPLINK ACTIVITY BY SETTING BIT4 OF FLAGWRD7 = 1.
 # THIS INDICATION WILL BE TRANSFERRED TO THE GROUND BY THE DOWNLINK WHICH DOWNLINKS ALL FLAGWORDS.
 # WHEN UPLINK ACTIVITY IS LOCKED OUT, IT CAN BE ALLOWED WHEN THE GROUND UPLINKS AND `ERROR RESET' CODE.
-# (IT IS RECOMMENDED THAT THE `ERROR LIGHT RESET' CODE IS PRECEEDED BY 16 BITS THE FIRST OF WHICH IS 1 FOLLOWED
+# (IT IS RECOMMENDED THAT THE `ERROR LIGHT RESET' CODE IS PRECEDED BY 16 BITS THE FIRST OF WHICH IS 1 FOLLOWED
 # BY 15 ZEROS.  THIS WILL ELIMINATE EXTRANEOUS BITS FROM INLINK WHICH MAY HAVE BEEN LEFT OVER FROM THE ORIGINAL
 # FAILURE).
 #

Comanche055/P20-P25.s

@@ -420,7 +420,7 @@ DE-GR-50	TC	2PHSCHNG
 #
 # ABORT MODES:  P23 ABORT IF MARKING SYSTEM OR EXTENDED VERB ACTIVE
 #
-# INPUT:  NONE REQURIES, NORMALLY CALLED BY P23
+# INPUT:  NONE REQUIRES, NORMALLY CALLED BY P23
 #
 # OUTPUT:  TRUNNION BIAS ANGLE: ANGLE DETERMINED WHEN SHAFT LINE OF SIGHT
 #	(SLOS) AND LANDMARK LINE OF SIGHT (LLOS) ARE SUPERIMPOSED.  THIS ANGLE
@@ -1407,7 +1407,7 @@ INITB		STORE	W +90D,1	# CLEAR 54 - 89
 #
 #		OMETATHSM = (REFSMMAT)(OMEGATH).
 #
-#	(10)	OBTAIN GIMBAL ANGLE INCREMETNS FOR 0.1 SECOND.
+#	(10)	OBTAIN GIMBAL ANGLE INCREMENTS FOR 0.1 SECOND.
 #
 #		DTHETASM = (0.1)(OMEGATHSM)
 #
@@ -1776,7 +1776,7 @@ FURST3		EQUALS	13,14,15	# CONSTANT FOR AUTOCK (OCT 70000).
 # ..... S22.1 ORBITAL NAVIGATION ROUTINE
 # MOD 1
 #
-# FUNCTONAL DESCRIPTION
+# FUNCTIONAL DESCRIPTION
 #	1.  UPDATE CSM STATE VECTOR
 #	2.  UPDATE LANDMARK POSITION
 #	3.  CONVERT W MATRIX FROM 9 TO 6 DIMENSIONS

Comanche055/P32-P33_P72-P73.s

@@ -42,7 +42,7 @@
 # MOD BY WHITE, P.	DATE 1 JUNE 67
 #
 # PURPOSE
-#	(1)	TO CALCULATE PARAMETERS ASSOCIATED WTIH THE FOLLOWING
+#	(1)	TO CALCULATE PARAMETERS ASSOCIATED WITH THE FOLLOWING
 #		CONCENTRIC FLIGHT PLAN MANEUVERS -- THE CO-ELLIPTIC SEQUENCE
 #		INITIATION (CSI) MANEUVER AND THE CONSTANT DELTA ALTITUDE
 #		(CDH) MANEUVER.

Comanche055/P34-35_P74-75.s

@@ -31,7 +31,7 @@
 
 
 # Page 460
-# TRANSFER PHASE INITITIATION (TPI) PROGRAMS (P34 AND P74)
+# TRANSFER PHASE INITIATION (TPI) PROGRAMS (P34 AND P74)
 # MOD NO -1			LOG SECTION -- P32-P35, P72-P75
 # MOD BY WHITE, P.		DATE: 1 JUNE 67
 #

Comanche055/P37_P70.s

@@ -44,7 +44,7 @@
 # DESCRIPTION
 #	A RETURN TO EARTH TRAJECTORY IS COMPUTED PROVIDED THE CSM IS OUTSIDE THE LUNAR SPHERE OF INFLUENCE AT THE
 #	TIME OF IGNITION.  INITIALLY A CONIC TRAJECTORY IS DETERMINED AND RESULTING IGNITION AND REENTRY PARAMETERS ARE
-# 	DISPLAYED TO THE ASTRONAUT.  THEN IF THE ASTRONAUT SO DESIRES, A PRECISION TRAJECTORY IS DETERMINED WTIH THE
+# 	DISPLAYED TO THE ASTRONAUT.  THEN IF THE ASTRONAUT SO DESIRES, A PRECISION TRAJECTORY IS DETERMINED WITH THE
 # 	RESULTING IGNITION AND REENTRY PARAMETERS DISPLAYED.  UPON FINAL ACCEPTANCE BY THE ASTRONAUT, THE PROGRAM
 # 	COMPUTES AND STORES THE TARGET PARAMETERS FOR RETURN TO EARTH FOR USE BY SPS PROGRAM (P40) OR RCS PROGRAM (P41).
 #

Comanche055/P51-P53.s

@@ -318,7 +318,7 @@ V06N89*		VN	0689
 # FUNCTION -- TO DISPLAY THE LANDING SITE LATITUDE,
 # LONGITUDE AND ALTITUDE.  TO ACCEPT NEW DATA VIA
 # THE KEYBOARD.  TO COMPUT THE LANDING SITE
-# ORIENTATIION FOR P52 OR P54.
+# ORIENTATION FOR P52 OR P54.
 #
 # LET:
 #	RLS  = LANDING SITE VECTOR IN REF COORDINATES
@@ -1633,7 +1633,7 @@ MKDNCDR		ECADR	MARKDOWN
 # MOD. NO. 2						21 DEC 66
 # MOD. BY STURLAUGSON
 #
-# FUNCTIONAL DESCRIPTIION:
+# FUNCTIONAL DESCRIPTION:
 #
 #	TO PERFORM A SATISFACTORY NUMBER OF SIGHTING MARKS FOR THE REQUESTING PROGRAM (OR ROUTINE).  SIGHTINGS
 # 	CAN BE MADE ON A STAR OR LANDMARK.  WHEN THE CMC ACCEPTS A MARK IT RECORDS AND STORES 5 ANGLES (3 ICDUS AND 2
@@ -1682,7 +1682,7 @@ R53A		CA	MARKINDX	# NUMBER OF MARKS
 		CADR	OPTSTALL
 		TC	CURTAINS
 		INDEX	MARKSTAT
-		CCS	QPRET		# NUMNBER OF MARKS ACTUALLY DONE
+		CCS	QPRET		# NUMBER OF MARKS ACTUALLY DONE
 		TCF	R53B
 		TCF	+2		# ZERO
 		TCF	+1		# CCS HOLE

Comanche055/P61-P67.s

@@ -343,7 +343,7 @@ POSECADR	2CADR	CM/POSE
 # MOD BY:	R. HIRSCHKOP
 # MOD NO: 2	MOD BY: RR BAIRNSFATHER		DATE: 8 MAY 68		REVISED COMMENTS FOR COLOSSUS
 # FUNCTION:	1.  TO START ENTRY GUIDANCE AT .05G SELECTING ROLL ATTITUDE, CONSTANT DRAG LEVEL, AND
-#		    DRAG THRESHHOLD, KA, WHICH ARE KEYED TO THE .05G POINT.
+#		    DRAG THRESHOLD, KA, WHICH ARE KEYED TO THE .05G POINT.
 #		2.  SELECT FINAL PHASE P67 IF V < 27000 FPS WHEN .2G OCCURS.
 #		3.  ITERATE FOR UP-CONTROL SOLUTION P65 IF V > 27000 FPS AND IF ALTITUDE RATE AND DRAG
 #		    LEVEL CONDITIONS ARE SATISFIED.  ENTER P65 WHEN CONSTANT DRAG CONTROLLER HAS BROUGHT RANGE
@@ -950,7 +950,7 @@ DUMPFISH	GOTO
 # MOD NO: 2	MOD BY: RR BAIRNSFATHER		DATE: 21 NOV 67		VARIABLE MU ADDED.
 # MOD NO: 3	MOD BY: RR BAIRNSFATHER		DATE: 21 MAR 68		ACCEPT DIFFERENT EARTH/MOON SCALE
 #
-# FUNCTONAL DESCRIPTION:  EARTH CENTERED VIS VIVA CALCULATION OF TERMINAL VELOCITY AND GAMMA (REL TO
+# FUNCTIONAL DESCRIPTION:  EARTH CENTERED VIS VIVA CALCULATION OF TERMINAL VELOCITY AND GAMMA (REL TO
 #	HORIZONTAL) GIVEN THE SCALAR QUANTITIES:  PRESENT RADIUS AND VELOCITY AND THE TERMINAL RADIUS.
 #	THE USER MUST APPEND PROPER SIGN TO GAMMA, SINCE IT IS CALCULATED AS A POSITIVE NUMBER.
 #	THE EQUATIONS ARE

Comanche055/P76.s

@@ -37,7 +37,7 @@
 #	BEEN TRANSFORMED FROM LV TO REF COSYS).  USING INTEGRVS, THE PROGRAM THEN INTEGRATES THE OTHER
 #	VEHICLE STATE VECTOR TO THE STATE VECTOR OF THIS VEHICLE, THUS INSURING THAT THE W-MATRIX AND BOTH VEHICLE
 #	STATES CORRESPOND TO THE SAME TIME.
-# 3)	ERASABLE INIITIALIZATION REQUIRED -- NONE.
+# 3)	ERASABLE INITIALIZATION REQUIRED -- NONE.
 # 4)	CALLING SEQUENCES AND EXIT MODES -- CALLED BY ASTRONAUT REQUEST THRU DSKY V 37 E 76E.
 #	EXITS BY TCF ENDOFJOB.
 # 5)	OUTPUT -- OTHER VEHICLE STATE VECTOR INTEGRATED TO TIG AND INCREMENTED BY DELTA V IN REF COSYS.

Comanche055/PHASE_TABLE_MAINTENANCE.s

@@ -99,7 +99,7 @@ DSPMMJOB	EQUALS	DSPMMJB
 # 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,
 # 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 EXAMLES,
+# IT IS SET TO 0.  SOME EXAMPLES,
 #		TC	PHASCHNG	# THIS WILL CAUSE GROUP 3 TO BE SET TO 0,
 #		OCT	00003		# MAKING GROUP 3 INACTIVE
 #