typo: fix misspelling of THE

Signed-off-by: Eden G. Adogla <eden@edengrail.io>
This commit is contained in:
Eden G. Adogla 2016-07-12 02:56:32 -07:00
parent 339768f665
commit 203561e2ef
13 changed files with 16 additions and 16 deletions

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@ -420,7 +420,7 @@ PIPFREE INHINT # PROGRAM DONE WITH PIPAS. DON'T LIGHT
# Page 1430
# THE FOLLOWING ROUTINE TORQUES THE IRIGS ACCORDING TO DOUBLE PRECISION INPUTS IN THE SIX REGISTERS
# BEGINNING AT THE ECADR ARRIVING IN A. THE MINIMUM SIZE OF ANY PULSE TRAIN IS 16 PULSES (.25 CDU COUNTS). THE
# UNSENT PORTION OF THE COMMAND IS LEFT INTACT AT TEH INPUT COMMAND REGISTERS.
# UNSENT PORTION OF THE COMMAND IS LEFT INTACT AT THE INPUT COMMAND REGISTERS.
EBANK= 1400 # VARIABLE, ACTUALLY.

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@ -2287,7 +2287,7 @@ LARGE2 INDEX FIXLOC
# Page 1178
# IF THE LENGTH OF THE ARGUMENT VECTOR WAS LESS THAN 2(-28), EACH COMPONENT MUST BE SHIFTED LEFT AT LEAST
# 14 PLACES BEFORE TEH DIVIDE, NOTE THAT IN THIS CASE, THE MAJOR PART OF EACH COMPONENT IS ZERO.
# 14 PLACES BEFORE THE DIVIDE, NOTE THAT IN THIS CASE, THE MAJOR PART OF EACH COMPONENT IS ZERO.
SMALL TS MPTEMP # NEGATIVE OF PRE-DIVIDE SHIFT COUNT.

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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.

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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.

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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

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@ -250,7 +250,7 @@ TRANSP2 CAF XNB1EB
# 2. GENERATE IN MPAC THE SIGNUM FUNCTION OF MPAC:
# ENTRY: RTB
# SIGNMPAC
# IN EITHER CASE, RETURN IS TO TEH NEXT INTERPRETIVE INSTRUCTION IN THE CALLING SEQUENCE.
# IN EITHER CASE, RETURN IS TO THE NEXT INTERPRETIVE INSTRUCTION IN THE CALLING SEQUENCE.
SIGNMPAC EXTEND
DCA DPOSMAX

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@ -45,7 +45,7 @@
#
# THE S17.2 ROUTINE FURTHER DEFINES THE SEARCH SECTOR BY COMPUTING ANGULAR LIMITS AND USES THE TIME THETA
# SUBROUTINE TO COMPUTE THE SEARCH START AND END TIMES. THE SEARCH IS THEN MADE IN AN ITERATIVE LOOP USING THE
# LAMBERT SUBROUTINE TO COMPUTE TEH VELOCITIES REQUIRED AT TPI TIME AND AT TPF TIME. EXIT FROM THE SEARCH LOOP
# LAMBERT SUBROUTINE TO COMPUTE THE VELOCITIES REQUIRED AT TPI TIME AND AT TPF TIME. EXIT FROM THE SEARCH LOOP
# IS MADE WHEN SOLUTION CRITERIA ARE MET (NORMAL EXIT) OR AS SOON AS IT IS EVIDENT THAT NO SOLUTION EXISTS IN
# THE SECTOR SEARCHED.
#

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@ -149,7 +149,7 @@ GAINCHNG TC IBNKCALL # UPDATE IXX, IAVG, IAVG/TLX
CAF NINETEEN # RESET THE VARIABLE-GAIN UPDATE COUNTER
TS VCNTRTMP
EXECCOPY INCR TVCEXPHS # RESTART-PROTECT TEH COPYCYCLE (1)
EXECCOPY INCR TVCEXPHS # RESTART-PROTECT THE COPYCYCLE (1)
CAE MASSTMP # CSMMASS KG B+16
TS CSMMASS

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@ -123,7 +123,7 @@
# CONTROL ACCELERATION CONACC, OR ITS RECIPROCAL, 1/CONACC, THE TVC
# ROLL DAP GAIN (SEE TVCEXECUTIVE VARIABLE GAIN PACKAGE). JET
# FIRING TIME IS SIMPLY THAT REQUIRED TO ACHIEVE THE DESIRED OGARATE,
# SUBJECT TO TEH LIMITATIONS DISCUSSED UNDER FUNCTIONAL DESCRIPTION,
# SUBJECT TO THE LIMITATIONS DISCUSSED UNDER FUNCTIONAL DESCRIPTION,
# ABOVE.
#
# THE THREE CONTROL REGIONS (+, -, AND ZERO TORQUE) ARE COMPRISED OF

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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

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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
#

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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.
#

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@ -167,7 +167,7 @@ PULSEIMU INDEX FIXLOC # ADDRESS OF GYRO COMMANDS SHOULD BE IN X1
# 2. GENERATE IN MPAC THE SIGNUM FUNCTION OF MPAC:
# ENTRY: RTB
# SIGNMPAC
# IN EITHER CASE, RETURN IS TO TEH NEXT INTERPRETIVE INSTRUCTION IN THE CALLING SEQUENCE.
# IN EITHER CASE, RETURN IS TO THE NEXT INTERPRETIVE INSTRUCTION IN THE CALLING SEQUENCE.
SIGNMPAC EXTEND
DCA DPOSMAX