Typo Fix - TEH to THE

swarad07 · Jul 14, 2016 · 4baa2e8 · 4baa2e8
1 parent bde049d
commit 4baa2e8
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Showing 6 changed files with 9 additions and 9 deletions.
diff --git a/Comanche055/P34-35_P74-75.s b/Comanche055/P34-35_P74-75.s
@@ -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.

diff --git a/Comanche055/P51-P53.s b/Comanche055/P51-P53.s
@@ -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.

diff --git a/Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s b/Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s
@@ -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

diff --git a/Luminary099/AGC_BLOCK_TWO_SELF_CHECK.s b/Luminary099/AGC_BLOCK_TWO_SELF_CHECK.s
@@ -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

diff --git a/Luminary099/DAP_INTERFACE_SUBROUTINES.s b/Luminary099/DAP_INTERFACE_SUBROUTINES.s
@@ -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
 #

diff --git a/Luminary099/P32-P35_P72-P75.s b/Luminary099/P32-P35_P72-P75.s
@@ -95,15 +95,15 @@
 #		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.
 
 #	(11)	THE ISS NEED NOT BE ON TO COMPLETE THIS PROGRAM.
 
 #	(12)	THE OPERATION OF THE PROGRAM UTILIZES THE FOLLOWING FLAGS --
 #
 #			ACTIVE VEHICLE FLAG -- DESIGNATES THE VEHICLE WHICH IS
-#			DOING RENDEZVOUS THRUSTING MANEUVERS TO TEH PROGRAM WHICH
+#			DOING RENDEZVOUS THRUSTING MANEUVERS TO THE PROGRAM WHICH
 #			CALCULATES THE MANEUVER PARAMETERS.  SET AT THE START OF
 #			EACH RENDEZVOUS PRE-THRUSTING PROGRAM.
 #