Merge branch 'chrislgarry-master'
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52accb294f
@ -425,7 +425,7 @@ PIPFREE INHINT # PROGRAM DONE WITH PIPAS. DON'T LIGHT
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EBANK= 1400 # VARIABLE, ACTUALLY.
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IMUPULSE TS MPAC +5 # SAVE ARRIVING ECADR.
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TC CAGETSTJ # DON'T PROCEED IF IMU BEING CAGED.
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TC CAGETSTJ # DONT PROCEED IF IMU BEING CAGED.
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CCS LGYRO # SEE IF GYROS BUSY.
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TC GYROBUSY # SLEEP.
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@ -660,7 +660,7 @@ C(30)LIM 2DEC .566985 # = 1.0 - .5 COS(30)
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# PROGRAM CALCULATES ENTRY DISPLAY OF MAXIMUM ACCELERATION EXPECTED (GMAX) AND ALSO THE EXPECTED
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# INERTIAL VELOCITY (VPRED) AND ENTRY ANGLE (GAMMAEI) THAT WILL OBTAIN AT 400K FT ABOVE THE FISCHER
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# ELLIPSOID. PROGRAM ALSO CALCULATES A SECOND DISPLAY RELATIVE TO THE EMSALT ABOVE FISCHER ELLIPSOID
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# AND CONSISTS OF RANGE TO SPLASH FOM NOW (RTGO) , PREDICTED INERTIAL VELOCITY (VIO) , AND THE TIME TO
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# AND CONSISTS OF RANGE TO SPLASH FROM NOW (RTGO) , PREDICTED INERTIAL VELOCITY (VIO) , AND THE TIME TO
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# GO FROM NOW (TTE) .
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#
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# CALLING SEQUENCE: CALL
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@ -44,7 +44,7 @@
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# FUNCT. DESCR.: P27 (THE UPDATE PROGRAM) PROCESSES COMMANDS AND DATA
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# INSERTIONS REQUESTED BY THE GROUND VIA UPLINK.
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# THE P27 PROGRAM WILL ACCEPT UPDATES
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# ONLY DURING P00 FOR THE LM, AND ONLY DURINT P00,
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# ONLY DURING P00 FOR THE LM, AND ONLY DURING P00,
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# P02, AND FRESH START FOR THE CSM.
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#
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# CALLING SEQ: PROGRAM IS INITIATED BY UPLINK ENTRY OF VERBS 70, 71, 72, AND 73.
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@ -236,7 +236,7 @@ WAIT2 TS WAITBANK # BBANK OF CALLING PROGRAM.
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# NOTE THAT THIS PROGRAM SECTION IS NEVER ENTERED WHEN T-T1 G/E -1,
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# SINCE TD-T1+1 = (TD-T) + (T-T1+1), AND DELTA T = TD-T G/E +1. (G/E
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# SYMBOL MEANS GREATER THAN OR EQUAL TO). THUS THERE NEED BE NO CON-
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# CERN OVER A PREVIOUS OR IMMINENT OVEFLOW OF TIME3 HERE.
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# CERN OVER A PREVIOUS OR IMMINENT OVERFLOW OF TIME3 HERE.
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AD POS1/2 # WHEN TD IS NEXT, FORM QUANTITY
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AD POS1/2 # 1.0 - DELTA T = 1.0 - (TD - T)
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@ -26,7 +26,7 @@
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# Page 206
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# PROGRAM NAME: AGS INITIALIZIZATION (R47)
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# PROGRAM NAME: AGS INITIALIZATION (R47)
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#
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# WRITTEN BY: RHODE/KILROY/FOLLETT
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#
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@ -264,9 +264,9 @@ JACCUV CS COEFFQ
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TCF STCTR1
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# THIS SECTION COMPUTES THE RATE OF CHANGE OF ACCELERATION DUE TO THE ROTATION OF THE GIMBALS. THE EQUATION
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# IMPLEMENTED IN BOTH THE Y-X PLANE AND THE Z-X PLANE IS -- D(ALPHA)/DT = TL/I*D(DELTA)/DT, WEHRE
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# IMPLEMENTED IN BOTH THE Y-X PLANE AND THE Z-X PLANE IS -- D(ALPHA)/DT = TL/I*D(DELTA)/DT, WHERE
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# T = ENGINE THRUST FORCE
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# L = PIVIT TO CG DISTANCE OF ENGINE
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# L = PIVOT TO CG DISTANCE OF ENGINE
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# I = MOMENT OF INERTIA
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LRESC CAE ABDELV # SCALED AT 2(13) CM/SEC(2)
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