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Merge pull request #131 from Prabhurajn/master

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Typo Fix - TEH to THE
This commit is contained in:
Chris Garry
2016-07-16 11:45:46 -04:00
committed by GitHub
parent 9e0ef60171 a3f0b90065
commit 6abbce8d49
6 changed files with 9 additions and 9 deletions
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6
Comanche055/P34-35_P74-75.agc
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@@ -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.

2
Comanche055/P51-P53.agc
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@@ -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.

2
Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.agc
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@@ -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

2
Luminary099/AGC_BLOCK_TWO_SELF_CHECK.agc
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@@ -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

2
Luminary099/DAP_INTERFACE_SUBROUTINES.agc
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@@ -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
#

4
Luminary099/P32-P35_P72-P75.agc
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@@ -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.
#