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@ -26,32 +26,32 @@
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# 16:27 JULY 14, 1969
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# 16:27 JULY 14, 1969
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# Page 926
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# Page 926
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# PROGRAM NAME -- PROG52 DATE -- JAN 9, 1967
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# PROGRAM NAME- PROG52 DATE- JAN 9, 1967
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# MOD NO -- 0 LOG SECTION -- P51-P53
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# MOD NO- 0 LOG SECTION- P51-P53
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# MODIFICATION BY -- LONSKE ASSEMBLY -- SUNDANCE REV 46
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# MODIFICATION BY- LONSKE ASSEMBLY- SUNDANCE REV 46
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#
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#
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# FUNCTIONAL DESCRIPTION --
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# FUNCTIONAL DESCRIPTION-
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#
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#
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# ALIGNS THE IMU TO ONE OF THREE ORIENTATIONS SELECTED BY THE ASTRONAUT. THE PRESENT IMU ORIENTATION IS KNOWN
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# ALIGNS THE IMU TO ONE OF THREE ORIENTATIONS SELECTED BY THE ASTRONAUT. THE PRESENT IMU ORIENTATION IS KNOWN
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# AND IS STORED IN REFSMMAT. THE THREE POSSIBLE ORIENTATIONS MAY BE:
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# AND IS STORED IN REFSMMAT. THE THREE POSSIBLE ORIENTATIONS MAY BE_
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#
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#
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# (A) PREFERRED ORIENTATION
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# (A) PREFERRED ORIENTATION
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#
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#
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# AN OPTIMUM ORIENTATION FOR A PREVIOUSLY CALCULATED MANEUVER. THIS ORIENTATION MUST BE CALCULATED AND
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# AN OPTIMUM ORIENTATION FOR A PREVIOUSLY CALCULATED MANEUVER. THIS ORIENTATION MUST BE CALCULATED AND
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# STORED BY A PREVIOUSLY SELECTED PROGRAM.
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# STORED BY A PREVIOUSLY SELECTED PROGRAM.
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#
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#
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# (B) NOMINAL ORIENTATION
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# (B) NOMINAL ORIENTATION
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#
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#
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# X = UNIT ( R )
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# X = UNIT ( R )
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# -SM
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# -SM
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#
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#
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# Y = UNIT (V X R)
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# Y = UNIT (V X R)
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# SM
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# SM
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#
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#
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# Z = UNIT (X X Y )
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# Z = UNIT (X X Y )
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# SM SM SM
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# SM SM SM
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#
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#
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# WHERE:
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# WHERE_
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#
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#
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# R = THE GEOCENTRIC RADIUS VECTOR AT TIME T(ALIGN) SELECTED BY THE ASTRONAUT
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# R = THE GEOCENTRIC RADIUS VECTOR AT TIME T(ALIGN) SELECTED BY THE ASTRONAUT
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# -
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# -
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@ -59,28 +59,28 @@
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# V = THE INERTIAL VELOCITY VECTOR AT TIME T(ALIGN) SELECTED BY THE ASTRONAUT
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# V = THE INERTIAL VELOCITY VECTOR AT TIME T(ALIGN) SELECTED BY THE ASTRONAUT
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# -
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# -
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#
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#
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# (C) RERSMMAT ORIENTATION
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# (C) REFSMMAT ORIENTATION
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#
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#
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# (D) LANDING SITE -- THIS IS NOT AVAILABLE IN SUNDANCE
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# (D) LANDING SITE - THIS IS NOT AVAILIBLE IN SUNDANCE
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#
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#
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# THIS SELECTION CORRECTS THE PRESENT IMU ORIENTATION. THE PRESENT ORIENTATION DIFFERS FROM THAT TO WHICH IT
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# THIS SELECTION CORRECTS THE PRESENT IMU ORIENTATION. THE PRESENT ORIENTATION DIFFERS FROM THAT TO WHICH IT
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# WAS LAST ALIGNED ONLY DUE TO GYRO DRIFT (I.E., NEITHER GIMBAL LOCK NOR IMU POWER INTERRUPTION HAS OCCURRED
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# WAS LAST ALIGNED ONLY DUE TO GYRO DRIFT (I.E. NEITHER GIMBAL LOCK NOR IMU POWER INTERRUPTION HAS OCCURRED
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# SINCE THE LAST ALIGNMENT).
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# SINCE THE LAST ALIGNMENT).
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#
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#
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# AFTER A IMU ORIENTATION HAS BEEN SELECTED ROUTINE S52.2 IS OPERATED TO COMPUTE THE GIMBAL ANGLES USING THE
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# AFTER A IMU ORIENTATION HAS BEEN SELECTED ROUTINE S52.2 IS OPERATED TO COMPUTE THE GIMBAL ANGLES USING THE
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# NEW ORIENTATION AND THE PRESENT VEHICLE ATTITUDE. CAL52A THEN USES THESE ANGLES, STORED IN THETAD,+1,+2, TO
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# NEW ORIENTATION AND THE PRESENT VEHICLE ATTITUDE. CAL52A THEN USES THESE ANGLES, STORED IN THETAD,+1,+2, TO
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# COARSE ALIGN THE IMU. THE STARS SELECTION ROUTINE, R56, IS THEN OPERATED. IF 2 STARS ARE NOT AVAILABLE AN ALARM
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# COARSE ALIGN THE IMU. THE STAR SELECTION ROUTINE, R56, IS THEN OPERATED. IF 2 STARS ARE NOT AVAILABLE AN ALARM
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# IS FLASHED TO NOTIFY THE ASTRONAUT. AT THIS POINT THE ASTRONAUT WILL MANEUVER THE VEHICLE AND SELECT 2 STARS
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# IS FLASHED TO NOTIFY THE ASTRONAUT. AT THIS POINT THE ASTRONAUT WILL MANEUVER THE VEHICLE AND SELECT 2 STARS
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# EITHER MANUALLY OR AUTOMATICALLY. AFTER 2 STARS HAVE BEEN SELECTED THE IMU IS FINE ALIGNED USING ROUTINE R51. IF
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# EITHER MANUALLY OR AUTOMATICALLY. AFTER 2 STARS HAVE BEEN SELECTED THE IMU IS FINE ALIGNED USING ROUTINE R51. IF
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# THE RENDEZVOUS NAVIGATION PROCESS IS OPERATING (INDICATED BY RNDVZFLG) P20 IS DISPLAYED. OTHERWISE P00 IS
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# THE RENDEZVOUS NAVIGATION PROCESS IS OPERATING(INDICATED BY RNDVZFLG) P20 IS DISPLAYED. OTHERWISE P00 IS
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# REQUESTED.
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# REQUESTED.
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#
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#
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# CALLING SEQUENCE --
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# CALLING SEQUENCE-
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#
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#
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# Page 927
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# Page 927
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# THE PROGRAM IS CALLED BY THE ASTRONAUT BY DSKY ENTRY.
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# THE PROGRAM IS CALLED BY THE ASTRONAUT BY DSKY ENTRY.
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#
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#
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# SUBROUTINES CALLED --
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# SUBROUTINES CALLED-
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#
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#
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# 1. FLAGDOWN 7. S52.2 13. NEWMODEX
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# 1. FLAGDOWN 7. S52.2 13. NEWMODEX
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# 2. R02BOTH 8. CAL53A 14. PRIOLARM
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# 2. R02BOTH 8. CAL53A 14. PRIOLARM
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# 5. GOFLASH 11. R51
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# 5. GOFLASH 11. R51
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# 6. S52.3 12. GOPERF3
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# 6. S52.3 12. GOPERF3
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#
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#
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# NORMAL EXIT MODES --
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# NORMAL EXIT MODES-
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#
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#
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# EXITS TO ENDOFJOB
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# EXITS TO ENDOFJOB
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#
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#
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# ALARM OR ABORT EXIT MODES --
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# ALARM OR ABORT EXIT MODES-
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#
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#
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# NONE
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# NONE
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#
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#
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# OUTPUT --
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# OUTPUT-
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#
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#
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# THE FOLLOWING MAY BE FLASHED ON THE DSKY
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# THE FOLLOWING MAY BE FLASHED ON THE DSKY
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# 1. IMU ORIENTATION CODE
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# 1. IMU ORIENTATION CODE
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# 2. ALARM CODE 215 -- PREFERRED IMU ORIENTATION NOT SPECIFIED
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# 2. ALARM CODE 215 -PREFERRED IMU ORIENTATION NOT SPECIFIED
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# 3. TIME OF NEXT IGNITION
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# 3. TIME OF NEXT IGNITION
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# 4. GIMBAL ANGLES
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# 4. GIMBAL ANGLES
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# 5. ALARM CODE 405 -- TWO STARS NOT AVAILABLE
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# 5. ALARM CODE 405 -TWO STARS NOT AVAILABLE
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# 6. PLEASE PERFORM P00
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# 6. PLEASE PERFORM P00
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# THE MODE DISPLAY MAY BE CHANGED TO 20
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# THE MODE DISPLAY MAY BE CHANGED TO 20
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#
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#
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# ERASABLE INITIALIZATION REQUIRED --
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# ERASABLE INITIALIZATION REQUIRED-
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#
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# PFRATFLG SHOULD BE SET IF A PREFERRED ORIENTATION HAS BEEN COMPUTED. IF IT HAS BEEN COMPUTED IT IS STORED IN
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# XSMD, YSMD, ZSMD.
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#
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#
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# PFRATFLG SHOULD BE SET IF A PREFERRED ORIENTATION HAS BEEN COMPUTED.IF IT HAS BEEN COMPUTED IT IS STORED IN
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# XSMD,YSMD,ZSMD.
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# RNDVZFLG INDICATES WHETHER THE RENDEZVOUS NAVIGATION PROCESS IS OPERATING.
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# RNDVZFLG INDICATES WHETHER THE RENDEZVOUS NAVIGATION PROCESS IS OPERATING.
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#
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#
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# DEBRIS --
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# DEBRIS-
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#
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#
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# WORK AREA
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# WORK AREA
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TC BANKCALL # FLASH OPTION CODE AND ORIENTATION CODE
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TC BANKCALL # FLASH OPTION CODE AND ORIENTATION CODE
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CADR GOPERF4R # FLASH V04N06
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CADR GOPERF4R # FLASH V04N06
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TC GOTOPOOH
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TC GOTOPOOH
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TCF +5 # V33 -- PROCEED
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TCF +5 # V33-PROCEED
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TC P52B # NEW CODE -- NEW ORIENTATION CODE INPUT
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TC P52B # NEW CODE - NEW ORIENTATION CODE INPUT
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TC PHASCHNG # DISPLAY RETURN
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TC PHASCHNG # DISPLAY RETURN
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OCT 00014
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OCT 00014
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TC ENDOFJOB
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TC ENDOFJOB
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CCS A
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CCS A
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TC P52W
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TC P52W
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# Page 929
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# Page 929
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TC INTPRET # OPTION 4 -- GET LS ORIENTATION
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TC INTPRET # OPTION 4 - GET LS ORIENTATION
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GOTO
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GOTO
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P52LS
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P52LS
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XSMD
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XSMD
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STCALL YSMD
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STCALL YSMD
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QMAJ
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QMAJ
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