From 4baa2e8ac3580a150a295634a019820d2c9adcb8 Mon Sep 17 00:00:00 2001 From: prabhurajn Date: Thu, 14 Jul 2016 14:18:29 +0530 Subject: [PATCH] Typo Fix - TEH to THE --- Comanche055/P34-35_P74-75.s | 6 +++--- Comanche055/P51-P53.s | 2 +- Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s | 2 +- Luminary099/AGC_BLOCK_TWO_SELF_CHECK.s | 2 +- Luminary099/DAP_INTERFACE_SUBROUTINES.s | 2 +- Luminary099/P32-P35_P72-P75.s | 4 ++-- 6 files changed, 9 insertions(+), 9 deletions(-) diff --git a/Comanche055/P34-35_P74-75.s b/Comanche055/P34-35_P74-75.s index eea2d1e1e..4d08d5136 100644 --- 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 index cf7fe50a2..45a488c88 100644 --- 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 index 2da9bfef8..263520c9f 100644 --- 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 index e2dc67cbc..d5d22b19e 100644 --- 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 index 689e4662f..23af0cc6f 100644 --- 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 index 061c7fd67..e4133c6f8 100644 --- a/Luminary099/P32-P35_P72-P75.s +++ b/Luminary099/P32-P35_P72-P75.s @@ -95,7 +95,7 @@ # 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. # (11) THE ISS NEED NOT BE ON TO COMPLETE THIS PROGRAM. @@ -103,7 +103,7 @@ # (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. #