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https://www.ibiblio.org/apollo/ScansForConversion/Luminary099/0619.jpg

R0045 (L82) add missing period
R0054 (L94) correct "BY" → "ON"
R0061 (L103) remove extra hyphen
R0062 (L105) remove extra hyphen
R0066 (L114) remove extra hyphen
R0075 (L122) add missing hyphen
R0077 (L126) remove word "THE" not in scan
Remove line (L131) at end of page (after R0111) not reflected in scan
Comment out empty lines within comment blocks, for consistency
This commit is contained in:
Nathan Scott 2020-10-20 00:36:21 +11:00
parent 173e615208
commit 1313143b44
1 changed files with 15 additions and 16 deletions
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31
Luminary099/P32-P35_P72-P75.agc
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@ -79,39 +79,39 @@
# PARALLEL TO THE PLANE OF THE CSM ORBIT. HOWEVER CREW # PARALLEL TO THE PLANE OF THE CSM ORBIT. HOWEVER CREW
# Page 619 # Page 619
# MODIFICATION OF DELTA V (LV) COMPONENTS MAY RESULT IN AN # MODIFICATION OF DELTA V (LV) COMPONENTS MAY RESULT IN AN
# OUT-OF-PLANE CSI MANEUVER # OUT-OF-PLANE CSI MANEUVER.
#
# (8) STATE VECTOR UPDATES BY P27 ARE DISALLOWED DURING AUTOMATIC # (8) STATE VECTOR UPDATES BY P27 ARE DISALLOWED DURING AUTOMATIC
# STATE VECTOR UPDATING INITIATED BY P20 (SEE ASSUMPTION 10). # STATE VECTOR UPDATING INITIATED BY P20 (SEE ASSUMPTION 10).
#
# (9) COMPUTED VARIABLES MAY BE STORED FOR LATER VERIFICATION BY # (9) COMPUTED VARIABLES MAY BE STORED FOR LATER VERIFICATION BY
# THE GROUND. THESE STORAGE CAPABILITIES ARE NORMALLY LIMITED # THE GROUND. THESE STORAGE CAPABILITIES ARE NORMALLY LIMITED
# ONLY TO THE PARAMETERS FOR ONE THRUSTING MANEUVER AT A TIME # ONLY TO THE PARAMETERS FOR ONE THRUSTING MANEUVER AT A TIME
# EXCEPT FOR CONCENTRIC FLIGHT PLAN MANEUVER SEQUENCES. # EXCEPT FOR CONCENTRIC FLIGHT PLAN MANEUVER SEQUENCES.
#
# (10) THE RENDEZVOUS RADAR MAY OR MAY NOT BE USED TO UPDATE THE LM # (10) THE RENDEZVOUS RADAR MAY OR MAY NOT BE USED TO UPDATE THE LM
# OR CSM STATE VECTORS FOR THIS PROGRAM. IF RADAR USE IS # OR CSM STATE VECTORS FOR THIS PROGRAM. IF RADAR USE IS
# DESIRED THE RADAR WAS TURNED ON AND LOCKED BY THE CSM BY # DESIRED THE RADAR WAS TURNED ON AND LOCKED ON THE CSM BY
# PREVIOUS SELECTION OF P20. RADAR SIGHTING MARKS WILL BE MADE # PREVIOUS SELECTION OF P20. RADAR SIGHTING MARKS WILL BE MADE
# AUTOMATICALLY APPROXIMATELY ONCE A MINUTE WHEN ENABLED BY THE # AUTOMATICALLY APPROXIMATELY ONCE A MINUTE WHEN ENABLED BY THE
# TRACK AND UPDATE FLAGS (SEE P20). THE RENDEZVOUS TRACKING # TRACK AND UPDATE FLAGS (SEE P20). THE RENDEZVOUS TRACKING
# MARK COUNTER IS ZEROED BY THE SELECTION OF P20 AND AFTER EACH # MARK COUNTER IS ZEROED BY THE SELECTION OF P20 AND AFTER EACH
# THRUSTING MANEUVER. # 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 # (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 THE PROGRAM WHICH # DOING RENDEZVOUS THRUSTING MANEUVERS TO THE PROGRAM WHICH
# CALCULATES THE MANEUVER PARAMETERS. SET AT THE START OF # CALCULATES THE MANEUVER PARAMETERS. SET AT THE START OF
# EACH RENDEZVOUS PRE-THRUSTING PROGRAM. # EACH RENDEZVOUS PRE-THRUSTING PROGRAM.
# #
# FINAL FLAG -- SELECTS FINAL PROGRAM DISPLAYS AFTER CREW HAS # FINAL FLAG - SELECTS FINAL PROGRAM DISPLAYS AFTER CREW HAS
# COMPLETED THE FINAL MANEUVER COMPUTATION AND DISPLAY # COMPLETED THE FINAL MANEUVER COMPUTATION AND DISPLAY
# CYCLE. # CYCLE.
# #
# EXTERNAL DELTA V STEERING FLAG -- DESIGNATES THE TYPE OF # EXTERNAL DELTA V STEERING FLAG - DESIGNATES THE TYPE OF
# STEERING REQUIRED FOR EXECUTION OF THIS MANEUVER BY THE # STEERING REQUIRED FOR EXECUTION OF THIS MANEUVER BY THE
# THRUSTING PROGRAM SELECTED AFTER COMPLETION OF THIS # THRUSTING PROGRAM SELECTED AFTER COMPLETION OF THIS
# PROGRAM. # PROGRAM.
@ -119,16 +119,15 @@
# (13) IT IS NORMALLY REQUIRED THAT THE ISS BE ON FOR 1 HOUR PRIOR TO # (13) IT IS NORMALLY REQUIRED THAT THE ISS BE ON FOR 1 HOUR PRIOR TO
# A THRUSTING MANEUVER. # A THRUSTING MANEUVER.
# #
# (14) THIS PROGRAM IS SELECTED BY THE ASTRONAUT BY DSKY ENTRY # (14) THIS PROGRAM IS SELECTED BY THE ASTRONAUT BY DSKY ENTRY -
# #
# P32 IF THIS VEHICLE IS ACTIVE VEHICLE. # P32 IF THIS VEHICLE IS ACTIVE VEHICLE.
# #
# P72 IF THIS VEHICLE IS THE PASSIVE VEHICLE. # P72 IF THIS VEHICLE IS PASSIVE VEHICLE.
# #
# INPUT # INPUT
#
# (1) TCSI TIME OF THE CSI MANEUVER # (1) TCSI TIME OF THE CSI MANEUVER
# Page 620 # Page 620
# (2) NN NUMBER OF APSIDAL CROSSINGS THRU WHICH THE ACTIVE # (2) NN NUMBER OF APSIDAL CROSSINGS THRU WHICH THE ACTIVE
# VEHICLE ORBIT CAN BE ADVANCED TO OBTAIN THE CDH # VEHICLE ORBIT CAN BE ADVANCED TO OBTAIN THE CDH