diff --git a/Luminary099/INTEGRATION_INITIALIZATION.agc b/Luminary099/INTEGRATION_INITIALIZATION.agc index 956d867..5fe4135 100644 --- a/Luminary099/INTEGRATION_INITIALIZATION.agc +++ b/Luminary099/INTEGRATION_INITIALIZATION.agc @@ -205,7 +205,7 @@ # OUTPUT # THE DATA LISTED IN SECTION 3.0 PLUS # RQVV POSITION VECTOR OF VEHICLE WITH RESPECT TO SECONDARY -# BODY... METERS B-29 ONLY IF MIDFLAG = DIMOFLAG = 1 +# BODY... METERS B-29 ONLY IF MIDFLAG = DIM0FLAG = 1 # B) CONIC INTEGRATION. CSMCONIC, LEMCONIC ENTRANCES # L-X STORE TIME IN PUSH LIST (TDEC1) # L CALL @@ -249,7 +249,7 @@ # L-5 VINTFLAG 1=CSM, 0=LM # L-4 INTYPFLAG 1=CONIC, 0=PRECISION # L-3 SET(CLEAR) SET(CLEAR) -# L-2 DIMOFLAG 1=W-MATRIX, 0=NO W-MATRIX +# L-2 DIM0FLAG 1=W-MATRIX, 0=NO W-MATRIX # L-1 D6OR9FLG 1=9X9, 0=6X6 # L SET DLOAD # L+1 STATEFLG DESIRE PERMANENT UPDATE @@ -257,7 +257,7 @@ # L+3 STCALL RFINAL # L+4 INTEGRV # L CALL NORMAL USE -- WILL UPDATE STATE -# L+1 INTEGRV VECTOR IF DIMOFLAG=1. (STATEFLG IS +# L+1 INTEGRV VECTOR IF DIM0FLAG=1. (STATEFLG IS # L+2 RETURN ALWAYS RESET IN INTEGRATION AFTER # IT IS USED.) # INPUT @@ -311,7 +311,7 @@ SETIFLGS SET CLEAR STATEFLG INTYPFLG CLEAR CLEAR - DIMOFLAG + DIM0FLAG D6OR9FLG RVQ NOINT EXIT @@ -479,7 +479,7 @@ INTBANK BBCON INTEGRV # CSMPREC CSMCONIC LEMPREC LEMCONIC # VINTFLAG SET SET CLEAR CLEAR # INTYPFLG CLEAR SET CLEAR SET -# DIMOFLAG CLEAR CLEAR CLEAR CLEAR +# DIM0FLAG CLEAR CLEAR CLEAR CLEAR # # CALLING SEQUENCE # L-X STORE TDEC1 @@ -508,7 +508,7 @@ CSMPREC STQ CALL IFLAGP SET CLEAR PRECIFLG - DIMOFLAG + DIM0FLAG CLRGO INTYPFLG INTEGRV1 @@ -527,7 +527,7 @@ CSMCONIC STQ CALL IRETURN VINTFLAG IFLAGC CLEAR SETGO - DIMOFLAG + DIM0FLAG INTYPFLG INTEGRV1 LEMCONIC STQ CALL @@ -555,7 +555,7 @@ INTEGRVS SET SSP STCALL TNUV RECTIFY CLEAR SET - DIMOFLAG + DIM0FLAG NEWIFLG SETGO RPQFLAG @@ -572,14 +572,14 @@ INTEGRVS SET SSP # THE FLAGS WHICH SHOULD BE SET OR CLEARED ARE # VINTFLAG (IGNORED WHEN ENTERED FROM INTEGRVS) # INTYPFLG -# DIMOFLAG +# DIM0FLAG # D6OR9FLG # # CALLING SEQUENCE # L-X CALL # L-Y INTSTALL # L-1 SET OR CLEAR ALL FOUR FLAGS. ALSO CAN SET STATEFLG IF DESIRED -# AND DIMOFLAG IS CLEAR. +# AND DIM0FLAG IS CLEAR. # L CALL # L+1 INTEGRV # @@ -768,8 +768,8 @@ POOHCHK DLOAD ABS BMN # NO BACKWARD INTEGRATION INTEXIT PDDL SR4 - DT/2 # IS 4(DT) LS (TDEC - TET) - SR2R BDSU + DT/2 # IS 4(DT) LS(TDEC - TET) + SR2R BDSU # NO BMN GOTO INTEXIT TIMESTEP @@ -795,7 +795,7 @@ INTWAKE CS RASFLAG # IS THIS INTSTALLED ROUTINE TO BE INDEX FIXLOC CA QPRET - TS TBASE2 # YES, DON'T RESTART WITH SOMEONE ELSE'S Q + TS TBASE2 # YES, DONT RESTART WITH SOMEONE ELSES Q TC PHASCHNG OCT 04022 @@ -807,7 +807,7 @@ INTWAKE CS RASFLAG # IS THIS INTSTALLED ROUTINE TO BE CAF REINTBIT MASK RASFLAG EXTEND - BZF GOBAC # DON'T INTWAKE IF WE CAME HERE VIA RESTART + BZF GOBAC # DONT INTWAKE IF WE CAME HERE VIA RESTART INTWAKE1 CAF WAKESTAL INHINT @@ -832,15 +832,15 @@ INTBITAB OCT 20100 # AVETOMID # # THIS ROUTINE PERFORMS THE TRANSITION FROM A THRUSTING PHASE TO THE COAST -# PHASE BY INITIALIZING THIS VEHICLE'S PERMANENT STATE VECTOR WITH THE +# PHASE BY INITIALIZING THIS VEHICLES PERMANENT STATE VECTOR WITH THE # VALUES LEFT BY THE AVERAGEG ROUTINE IN RN,VN,PIPTIME. # -# BEFORE THIS IS DONE THE W-MATRIX, IF ITS VALID (OR WFLAG OR RENDWFLT IS +# BEFORE THIS IS DONE THE W-MATRIX, IF ITS VALID (ORWFLAG OR RENDWFLG IS # SET) IS INTEGRATED FORWARD TO PIPTIME WITH THE PRE-THRUST STATE VECTOR. # # IN ADDITION, THE OTHER VEHICLE IS INTEGRATED (PERMANENT) TO PIPTIME. # -# FINALLY TRKMKCNT IS ZEROED. +# FINALLY TRKMKCNT IS ZEROED SETLOC INTINIT BANK @@ -894,7 +894,7 @@ INT/W DLOAD CALL INTSTALL SET SET DIM0FLAG # DO W-MATRIX - AVEMIDSW # SO WON'T CLOBBER RN,VN,PIPTIME + AVEMIDSW # SO WONT CLOBBER RN,VN,PIPTIME SET CLEAR D6OR9FLG # 9X9 FOR LM VINTFLAG # LM @@ -908,22 +908,22 @@ INT/W DLOAD CALL # # THIS ROUTINE INTEGRATES (PRECISION) TO THE TIME SPECIFIED IN TDEC1. # IF, AT THE END OF AN INTEGRATION TIME STEP, CURRENT TIME PLUS A DELTA -# TIME (SEE TIMEDELT.....BASED ON THE COMPUTATION TIME FOR ONE TIME STEP) +# TIME (SEE TIMEDELT.....BASED ON THE COMPUTATUON TIME FOR ONE TIME STEP) # IS GREATER THAN THE DESIRED TIME, ALARM 1703 IS SET AND THE INTEGRATION # IS DONE TO THE CURRENT TIME. # RETURN IS IN BASIC TO THE RETURN ADDRESS PLUS ONE. # # IF THE INTEGRATION IS FINISHED TO THE DESIRED TIME, RETURN IS IN BASIC -# TO THE RETURN ADDRESS. +# TO THE RETURN ADDRESS # -# IN EITHER CASE, BEFORE RETURNING, THE EXTRAPOLATED STATE VECTOR IS TRANSFERRED -# FROM R,VATT TO R,VN1-PIPTIME1 IS SET TO THE FINISHING INTEGRATION -# TIME AND MPAC IS SET TO THE DELTA TIME -- -# TAT MINUS CURRENT TIME +# IN EITHER CASE, BEFORE RETURNING, THE EXTRAPOLATED STATE VECTOR IS TRAN +# FERRED FROM R,VATT TO R,VN1-PIPTIME1 IS SET TO THE FINISHING INTEGRA- +# TION TIME AND MPAC IS SET TO THE DELTA TIME -- +# TAT MINUS CURRENT TIME. # MIDTOAV2 # -# THIS ROUTINE INTEGRATES THIS VEHICLE'S STATE VECTOR TO THE CURRENT TIME. +# THIS ROUTINE INTEGRATES THIS VEHICLES STATE VECTOR TO THE CURRENT TIME. # NO INPUTS ARE REQUIRED OF THE CALLER. RETURN IS IN BASIC TO THE RETURN # ADDRESS WITH THE ABOVE TRANSFERS TO R,VN1-PIPTIME1-AND MPAC DONE @@ -958,7 +958,7 @@ ENTMID1 CALL THISVINT CLEAR SET INTYPFLG - MIDAVFLG # LET INTEG. KNOW THE CALL IS FOR MIDTOAV. + MIDAVFLG # LET INTEG. KNOW THE CALL IS FOR MIDTOAV. CALL INTEGRV # GO INTEGRATE CLEAR VLOAD @@ -1077,10 +1077,10 @@ INTWAKLM CALL # UPDATE LM STATE VECTOR INTWAKEX CLEAR RENDWFLG -INTWAKUP SSP CALL # REMOVE `UPDATE STATE VECTOR INDICATOR' +INTWAKUP SSP CALL # REMOVE :UPDATE STATE VECTOR INDICATOR: UPSVFLAG 0 - INTWAKE0 # RELEASE `GRAB' OF ORBIT INTEG. + INTWAKE0 # RELEASE :GRAB: OF ORBIT INTEG. EXIT TC PHASCHNG