diff --git a/Luminary099/P34-35_P74-75.agc b/Luminary099/P34-35_P74-75.agc index cb8a0dcf9..e4c3e2330 100644 --- a/Luminary099/P34-35_P74-75.agc +++ b/Luminary099/P34-35_P74-75.agc @@ -34,13 +34,13 @@ # TRANSFER PHASE INITITIATION (TPI) PROGRAMS (P34 AND P74) # MOD NO -1 LOG SECTION -- P32-P35, P72-P75 -# MOD BY WHITE, P. DATE: 1 JUNE 67 +# MOD BY WHITE.P DATE 1JUNE67 # # PURPOSE # # (1) TO CALCULATE THE REQUIRED DELTA V AND OTHER INITIAL CONDITIONS # REQUIRED BY THE ACTIVE VEHICLE FOR EXECUTION OF THE TRANSFER -# PHASE INITITATION (TPI) MANEUVER, GIVEN -- +# PHASE INITITATION (TPI) MANEUVER, GIVEN - # (A) TIME OF IGNITION TIG (TPI) OR THE ELEVATION ANGLE (E) OF # THE ACTIVE/PASSIVE VEHICLE LOS AT TIG (TPI). @@ -62,9 +62,9 @@ # # ASSUMPTIONS -# (1) LM ONLY -- THIS PROGRAM IS BASED UPON PREVIOUS COMPLETION OF +# (1) LM ONLY - THIS PROGRAM IS BASED UPON PREVIOUS COMPLETION OF # THE CONSTANT DELTA ALTITUDE (CDH) PROGRAM (P33/P73). -# THEREFORE -- +# THEREFORE - # (A) AT A SELECTED TPI TIME (NOW IN STORAGE) THE LINE OF SIGHT # BETWEEN THE ACTIVE AND PASSIVE VEHICLES WAS SELECTED TO BE @@ -108,23 +108,23 @@ # (5) THE ISS NEED NOT BE ON TO COMPLETE THIS PROGRAM. -# (6) THE OPERATION OF THE PROGRAM UTILIZES THE FOLLOWING FLAGS -- +# (6) THE OPERATION OF THE PROGRAM UTILIZES THE FOLLOWING FLAGS - # -# ACTIVE VEHICLE FLAG -- DESIGNATES THE VEHICLE WHICH IS +# ACTIVE VEHICLE FLAG - DESIGNATES THE VEHICLE WHICH IS # DOING RENDEZVOUS THRUSTING MANEUVERS TO THE PROGRAM WHICH # CALCULATES THE MANEUVER PARAMETERS. SET AT THE START OF # EACH RENDEZVOUS PRE-THRUSTING PROGRAM. # -# FINAL FLAG -- SELECTS FINAL PROGRAM DISPLAYS AFTER CREW HAS +# FINAL FLAG - SELECTS FINAL PROGRAM DISPLAYS AFTER CREW HAS # SELECTED THE FINAL MANEUVER COMPUTATION CYCLE. # -# EXTERNAL DELTA V FLAG -- DESIGNATES THE TYPE OF STEERING +# EXTERNAL DELTA V FLAG - DESIGNATES THE TYPE OF STEERING # REQUIRED FOR EXECUTION OF THIS MANEUVER BY THE THRUSTING # PROGRAM SELECTED AFTER COMPLETION OF THIS PROGRAM. # -# (7) ONCE THE PARAMETERS REQUIRED FOR COMPUTATION OF THE MANEUVER +# (7) ONCE THE PARAMETWRS REQUIRED FOR COMPUTATION OF THE MANEUVER # HAVE BEEN COMPLETELY SPECIFIED, THE VALUE OF THE ACTIVE -# VEHICLE CENTRAL ANGLE OF TRANSFER IS COMPUTED AND STURED. +# VEHICLE CENTRAL ANGLE OF TRANSFER IS COMPUTED AND STORED. # THIS NUMBER WILL BE AVAILABLE FOR DISPLAY TO THE ASTRONAUT # THROUGH THE USE OF V06N52. # @@ -132,10 +132,10 @@ # CENTRAL ANGLE OF TRANSFER OF THE ACTIVE VEHICLE IS NOT WITHIN # Page 660 # 170 TO 190 DEGREES. IF THE ANGLE IS WITHIN THIS ZONE THE -# ASTRONAUT SHOULD REASSES THE INPUT TARGETING PARAMETERS BASED +# ASTRONAUT SHOULD REASSESS THE INPUT TARGETING PARAMETERS BASED # UPON DELTA V AND EXPECTED MANEUVER TIME. # -# (8) THIS PROGRAM IS SELECTED BY THE ASTRONAUT BY DSKY ENTRY -- +# (8) THIS PROGRAM IS SELECTED BY THE ASTRONAUT BY DSKY ENTRY - # # P34 IF THIS VEHICLE IS ACTIVE VEHICLE. # @@ -159,8 +159,8 @@ # (5) POSTTPI PERIGEE ALTITUDE AFTER THE TPI MANEUVER # (6) DELVTPI MAGNITUDE OF DELTA V AT TPI # (7) DELVTPF MAGNITUDE OF DELTA V AT INTERCEPT -# (8) DVLOS DELTA VELOCITY AT TPI -- LINE OF SIGHT -# (9) DELVLVC DELTA VELOCITY AT TPI -- LOCAL VERTICAL COORDINATES +# (8) DVLOS DELTA VELOCITY AT TPI - LINE OF SIGHT +# (9) DELVLVC DELTA VELOCITY AT TPI - LOCAL VERTICAL COORDINATES # # DOWNLINK # @@ -169,7 +169,7 @@ # (3) ELEV DESIRED LOS ANGLE AT TPI # (4) CENTANG ORBITAL CENTRAL ANGLE OF THE PASSIVE VEHICLE DURING # TRANSFER FROM TPI TO TIME OF INTERCEPT -# (5) DELVEET3 DELTA VELOCITY AT TPI -- REFERENCE COORDINATES +# (5) DELVEET3 DELTA VELOCITY AT TPI - REFERENCE COORDINATES # (6) TPASS4 TIME OF INTERCEPT # # COMMUNICATION TO THRUSTING PROGRAMS @@ -323,14 +323,14 @@ P34/P74E TC INTPRET # Page 664 # RENDEZVOUS MID-COURSE MANEUVER PROGRAMS (P35 AND P75) -# MOD NO -1 LOG SECTION -- P32-P35, P72-P75 -# MOD BY WHITE, P. DATE: 1 JUNE 67 +# MOD NO -1 LOG SECTION - P32-P35, P72-P75 +# MOD BY WHITE.P DATE 1JUNE67 # # PURPOSE # # (1) TO CALCULATE THE REQUIRED DELTA V AND OTHER INITIAL CONDITIONS # REQUIRED BY THE ACTIVE VEHICLE FOR EXECUTION OF THE NEXT -# MID-COURSE CORRECTION OF THE TRANSFER PHASE OF AN ACTIVE +# MIDCOURSE CORRECTION OF THE TRANSFER PHASE OF AN ACTIVE # VEHICLE RENDEZVOUS. # # (2) TO DISPLAY TO THE ASTRONAUT AND THE GROUND CERTAIN DEPENDENT @@ -354,17 +354,17 @@ P34/P74E TC INTPRET # RENDEZVOUS TRACKING MARK COUNTER IS ZEROED BY THE SELECTION OF # P20 AND AFTER EACH THRUSTING MANEUVER. # -# (4) THE OPERATION OF THE PROGRAM UTILIZES THE FOLLOWING FLAGS -- +# (4) THE OPERATION OF THE PROGRAM UTILIZES THE FOLLOWING FLAGS - # -# THE ACTIVE VEHICLE FLAG -- DESIGNATES THE VEHICLE WHICH IS +# ACTIVE VEHICLE FLAG - DESIGNATES THE VEHICLE WHICH IS # DOING RENDEZVOUS THRUSTING MANEUVERS TO THE PROGRAM WHICH # CALCULATES THE MANEUVER PARAMETERS. SET AT THE START OF # EACH RENDEZVOUS PRE-THRUSTING PROGRAM. # -# FINAL FLAG -- SELECTS FINAL PROGRAM DISPLAYS AFTER CREW HAS +# FINAL FLAG - SELECTS FINAL PROGRAM DISPLAYS AFTER CREW HAS # SELECTED THE FINAL MANEUVER COMPUTATION CYCLE. # -# EXTERNAL DELTA V FLAG -- DESIGNATES THE TYPE OF STEERING +# EXTERNAL DELTA V FLAG - DESIGNATES THE TYPE OF STEERING # REQUIRED FOR EXECUTION OF THIS MANEUVER BY THE THRUSTING # PROGRAM SELECTED AFTER COMPLETION OF THIS PROGRAM. # @@ -385,7 +385,7 @@ P34/P74E TC INTPRET # ASTRONAUT SHOULD REASSESS THE INPUT TARGETING PARAMETERS BASED # UPON DELTA V AND EXPECTED MANEUVER TIME. # -# (7) THIS PROGRAM IS SELECTED BY THE ASTRONAUT BY DSKY ENTRY -- +# (7) THIS PROGRAM IS SELECTED BY THE ASTRONAUT BY DSKY ENTRY - # # P35 IF THIS VEHICLE IS ACTIVE VEHICLE. # @@ -393,28 +393,27 @@ P34/P74E TC INTPRET # # INPUT # -# (1) TPASS4 TIME OF INTERCEPT -- SAVED FROM P34/P74 +# (1) TPASS4 TIME OF INTERCEPT - SAVED FROM P34/P74 # # OUTPUT # # (1) TRKMKCNT NUMBER OF MARKS # (2) TTOGO TIME TO GO -# (3) +MGA MIDOLF GIMBAL ANGLE -# (4) DVLOS DELTA VELOCITY AT MID -- LINE OF SIGHT -# (5) DELVLVC DELTA VELOCITY AT MID -- LOCAL VERTICAL COORDINATES +# (3) +MGA MIDDLE GIMBAL ANGLE +# (4) DVLOS DELTA VELOCITY AT MID - LINE OF SIGHT +# (5) DELVLVC DELTA VELOCITY AT MID - LOCAL VERTICAL COORDINATES # # DOWNLINK # # (1) TIG TIME OF THE TPM MANEUVER -# (2) DELVEET3 DELTA VELOCITY AT TPM -- REFERENCE COORDINATES +# (2) DELVEET3 DELTA VELOCITY AT TPM - REFERENCE COORDINATES # (3) TPASS4 TIME OF INTERCEPT -# # COMMUNICATION TO THRUSTING PROGRAMS # # (1) TIG TIME OF THE TPM MANEUVER # (2) RTARG OFFSET TARGET POSITION # (3) TPASS4 TIME OF INTERCEPT -# (4) XDELVFLG RESET TO INDICATE LAMBERT (AIMPOINT) VG COMPUTATION. +# (4) XDELVFLG RESET TO INDICATE LAMBERT (AIMPOINT) VG COMPUTATION # # SUBROUTINES USED #