Typo Fix - TEH to THE
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@ -62,7 +62,7 @@
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# HORIZONTAL PLANE DEFINED BY THE ACTIVE VEHICLE POSITION.
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# (B) THE TIME BETWEEN CDH IGNITION AND TPI IGNITION WAS
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# COMPUTED TO BE GREATER THAN 10 MINUTES.
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# (C) THE VARIATION OF TEH ALTITUDE DIFFERENCE BETWEEN THE
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# (C) THE VARIATION OF THE ALTITUDE DIFFERENCE BETWEEN THE
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# ORBITS WAS MINIMIZED.
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# (D) THE PERICENTER ALTITUDES OF ORBITS FOLLOWING CSI AND
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# CDH WERE COMPUTED TO BE GREATER THAN 35,000 FT FOR LUNAR
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@ -86,7 +86,7 @@
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# PREVIOUS SELECTION OF P20. RADAR SIGHTING MARKS WILL BE MADE
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# AUTOMATICALLY APPROXIMATELY ONCE A MINUTE WHEN ENABLED BY THE
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# TRACK AND UPDATE FLAGS (SEE P20). THE RENDEZVOUS TRACKING
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# MARK COUNTER IS ZEROED BY TEH SELECTION OF P20 AND AFTER EACH
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# MARK COUNTER IS ZEROED BY THE SELECTION OF P20 AND AFTER EACH
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# THRUSTING MANEUVER.
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# (5) THE ISS NEED NOT BE ON TO COMPLETE THIS PROGRAM.
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# (6) THE OPERATION OF THE PROGRAM UTILIZES THE FOLLOWING FLAGS --
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@ -104,7 +104,7 @@
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# PROGRAM SELECTED AFTER COMPLETION OF THIS PROGRAM.
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#
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# (7) ONCE THE PARAMETERS REQUIRED FOR COMPUTATION OF THE MANEUVER
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# HAVE BEEN COMPLETELY SPECIFIED, TEH VALUE OF THE ACTIVE
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# HAVE BEEN COMPLETELY SPECIFIED, THE VALUE OF THE ACTIVE
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# VEHICLE CENTRAL ANGLE OF TRANSFER IS COMPUTED AND STORED.
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# THIS NUMBER WILL BE AVAILABLE FOR DISPLAY TO THE ASTRONAUT
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# THROUGH THE USE OF V06N52.
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@ -1787,7 +1787,7 @@ S52.2.1 AXC,1 AXC,2
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# TARG1 AND TARG2 FLAGS ARE LOOKED AT TO DETERMINE IF THE TARGET IS THE
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# LEM, STAR, OR LANDMARK. IN CASE OF LEM OR LMK, THE PRESENT TIME PLUS
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# 2 SECONDS IS SAVED IN AOPTIME (ALIAS STARAD, +1). IF THE LEM IS
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# THE TARGET THEN CONIC UPDATES OF TEH CSM AND LEM ARE MADE TO
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# THE TARGET THEN CONIC UPDATES OF THE CSM AND LEM ARE MADE TO
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# THE TIME IN AOPTIME. THE UNIT OF THE DIFFERENCE OF LEM AND CSM
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# POSITION VECTORS BECOMES THE REFERENCE SIGHTING VECTOR USED IN THE
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# COMMON PART OF THE THIS PROGRAM.
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@ -3471,7 +3471,7 @@ FLASHOFF CS BIT6 # TURN OFF V/N FLASH
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# HAS BEEN REMOVED AND THE INTERNAL USER NO LONGER HAS THE PROTECTION THIS
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# OFFERED.
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#
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# THERE ARE TWO WAYS A JOB CAN BE PUT TO SLEEP BY TEH KEYBOARD + DISPLAY
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# THERE ARE TWO WAYS A JOB CAN BE PUT TO SLEEP BY THE KEYBOARD + DISPLAY
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# PROGRAM. 1) BY ENDIDLE
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# 2) BY NVSUBUSY
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# THE BASIC CONVENTION IS THAT ONLY ONE JOB WILL BE PERITTED ASLEEP VIA
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@ -469,7 +469,7 @@ CHKSUPR MASK HI5
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ADS SKEEP4
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TC GONXTBNK
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NXTSUPR AD SUPRCON # SET BNK 30 + INCR SUPR BNK AND CANCEL
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ADS SKEEP4 # ERC BIT OF TEH 37 TO 40 ADVANCE.
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ADS SKEEP4 # ERC BIT OF THE 37 TO 40 ADVANCE.
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GONXTBNK CCS SKEEP7
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TC COMMFX
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CA S+1
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@ -70,7 +70,7 @@
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# PFLITEDB -- SET DEADBAND TO 1.0 DEGREE AND ZERO THE COMMANDED ATTITUDE CHANGE AND COMMANDED RATE
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#
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# ALL ENTRIES SET UP A NOVAC JOB TO DO 1/ACCS SO THAT THE TJETLAW SWITCH CURVES ARE POSITIONED TO
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# REFLECT TEH NEW DEADBAND. IT SHOULD BE NOTED THAT THE DEADBAND REFERS TO THE ATTITUDE IN THE P-, U-, AND V-AXES.
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# REFLECT THE NEW DEADBAND. IT SHOULD BE NOTED THAT THE DEADBAND REFERS TO THE ATTITUDE IN THE P-, U-, AND V-AXES.
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#
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# SUBROUTINE CALLED: NOVAC
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#
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@ -95,7 +95,7 @@
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# PREVIOUS SELECTION OF P20. RADAR SIGHTING MARKS WILL BE MADE
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# AUTOMATICALLY APPROXIMATELY ONCE A MINUTE WHEN ENABLED BY THE
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# TRACK AND UPDATE FLAGS (SEE P20). THE RENDEZVOUS TRACKING
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# MARK COUNTER IS ZEROED BY TEH SELECTION OF P20 AND AFTER EACH
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# MARK COUNTER IS ZEROED BY THE SELECTION OF P20 AND AFTER EACH
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# THRUSTING MANEUVER.
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# (11) THE ISS NEED NOT BE ON TO COMPLETE THIS PROGRAM.
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@ -103,7 +103,7 @@
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# (12) THE OPERATION OF THE PROGRAM UTILIZES THE FOLLOWING FLAGS --
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#
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# ACTIVE VEHICLE FLAG -- DESIGNATES THE VEHICLE WHICH IS
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# DOING RENDEZVOUS THRUSTING MANEUVERS TO TEH PROGRAM WHICH
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# DOING RENDEZVOUS THRUSTING MANEUVERS TO THE PROGRAM WHICH
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# CALCULATES THE MANEUVER PARAMETERS. SET AT THE START OF
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# EACH RENDEZVOUS PRE-THRUSTING PROGRAM.
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#
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