VOYAGER
Voyager LECP Data Analysis Handbook
Instrument Modeling Reports
by Sheela Shodhan
E.5 TDHPCG
******************************************************************* * THIS PROGRAM IS THE DIFFERENTIAL EQUATION SOLVER-DHPCG WHICH * * USES THE HAMMING'S MODIFIED FOURTH ORDER PREDICTOR-CORRECTOR * * DOUBLE-PRECISION METHOD. * * THIS IS A MODIFICATION OF SUBROUTINE DHPCG FROM THE * * SCIENTIFIC SUBROUTINE PACKAGE (SSP) PUBLISHED BY * * IBM. THE ORIGINAL VERSION OF THE ROUTINE WAS WRITTEN IN * * FORTRAN-4 WITH NO INDENTATION AS WELL AS POORLY * * STRUCTURED. * * THE FOLLOWING VERSION IS VERY MUCH MODERNIZED TO A STRUCTURED * * CODE AND INDENTED IN FORTRAN-77. THE USERS ARE REFERED TO THE * * MANUAL OF SSP FOR FURTHER IMFORMATION ABOUT THE METHODS AND * * DETAILED DESCRIPTION. * *******************************************************************
SUBROUTINE DHPCG(PRMT,PV,DERY,NDIM,IHLF,FCT,OUTP,AUX)
REAL*8 PRMT(1),X,H,Z,DELT,PV(1),DERY(1),AUX(16,1) INTEGER NHIT COMMON /NHIT/NHIT
NHIT=0 N=1 IHLF1=0 IHLF=0 X=PRMT(1) H=PRMT(3) PRMT(5)=0.D0 DO I=1,NDIM AUX(16,I)=0.D0 AUX(15,I)=DERY(I) AUX(1,I)=PV(I) END DO C ERROR RETURNS IF((H*PRMT(2)).LT.X*H) THEN IHLF=13 ELSE IF((H*PRMT(2)).EQ.X*H) THEN IHLF=12 END IF ISW=0 C **************************************************************** C C COMPUTATION OF DERY FOR STARTING VALUES C BLOCK 1 VS OLD LABELS 4_20 C C *************************************************************** DO WHILE (ISW.NE.4) IF(ISW.EQ.0) THEN IHLF1=0 CALL FCT(X,PV,DERY) C RECORDING OF STARTING VALUES CALL OUTP(X,PV,DERY,IHLF,NDIM,PRMT,NHIT) IF (NHIT.NE.0) RETURN IF(PRMT(5).NE.0.) THEN RETURN END IF DO I=1,NDIM AUX(8,I)=DERY(I) END DO C COMPUTATION OF AUX(2,I) ISW=1 ELSE IF(ISW.EQ.1) THEN IF(IHLF1.NE.1) THEN X=X+H DO I=1,NDIM AUX(2,I)=PV(I) END DO END IF IHLF1=0 C INCREMENT IS TESTED BY MEANS OF BISECTION IHLF=IHLF+1 X=X-H DO I=1,NDIM AUX(4,I)=AUX(2,I) END DO H=.5D0*H N=1 ISW=2 ELSE IF(ISW.EQ.2) THEN X=X+H CALL FCT(X,PV,DERY) N=2 DO I=1,NDIM AUX(2,I)=PV(I) AUX(9,I)=DERY(I) ENDDO ISW=3 ELSE IF(ISW.EQ.3) THEN C COMPUTATION OF TEST VALUE DELT DELT=0.D0 DO I=1,NDIM DELT=DELT+AUX(15,I)*DABS(PV(I)-AUX(4,I)) ENDDO DELT=.66666666667D-1*DELT IF(DELE.LE.PRMT(4)) THEN ISW=5 ELSE IF(IHLF.GE.10) THEN IHLF=11 X=X+H ISW=0 IHLF1=2 ELSE C NO SATISFACTORY ACCURACY AFTER 10 BISECTIONS. ERROR MESSAGE. IHLF1=1 ISW=1 ENDIF ENDIF ELSE IF(ISW.EQ.5) THEN C THERE IS SATISFACTORY ACCURACY AFTER LESS THAN 11 BISECTIONS. X=X+H CALL FCT(X,PV,DERY) DO I=1,NDIM AUX(3,I)=PV(I) AUX(10,I)=DERY(I) ENDDO N=3 ISW=4 ENDIF C ******************************************************************* C C THE FOLLOWING PART OF SUBROUTINE HPCG COMPUTES BY MEANS OF C RUNGE-KUTTA METHOD STARTING VALUES FOR THE NOT SELF-STARTING C PREDICTOR-CORRECTOR METHOD. C BLOCK 2 VS OLD LABELS 100_104 C C ******************************************************************* IF(ISW.NE.5.AND.IHLF1.EQ.0) THEN DO I=1,NDIM Z=H*AUX(N+7,I) AUX(5,I)=Z PV(I)=AUX(N,I)+.4D0*Z ENDDO C Z IS AN AUXILIARY STORAGE LOCATION Z=X+.4D0*H CALL FCT(X,PV,DERY) DO I=1,NDIM Z=H*DERY(I) AUX(6,I)=Z PV(I)=AUX(N,I)+.29697760925D0*AUX(5,I)+.15875964497D0*Z ENDDO Z=X+.45573725422D0*H CALL FCT(X,PV,DERY) DO I=1,NDIM Z=H*DERY(I) AUX(7,I)=Z PV(I)=AUX(N,I)+0.21810038823D0*AUX(5,I)-3.0509651487D0*AUX(6,I) * + 3.8328647605D0*Z ENDDO Z=X+H CALL FCT(X,PV,DERY) DO I=1,NDIM PV(I)=AUX(N,I)+.17476028223D0*AUX(5,I)-.55148066288D0*AUX(6,I) * +1.2055355994D0*AUX(7,I)+.17118478122D0*H*DERY(I) ENDDO ENDIF ENDDO C ******************************************************************* C C BLOCK 3 VS OLD LABELS 21_22 C C ******************************************************************* N=1 X=X+H CALL FCT(X,PV,DERY) X=PRMT(1) DO I=1,NDIM AUX(11,I)=DERY(I) PV(I)=AUX(1,I)+H*(.375D0*AUX(8,I)+.79166666667D0*AUX(9,I) * -.20833333333D0*AUX(10,I)+.41666666667D-1*DERY(I)) ENDDO C ********************************************************************* C C BLOCK 4 VS OLD LABELS 23_30 C C ********************************************************************* DO WHILE (N.LT.4) X=X+H N=N+1 CALL FCT(X,PV,DERY) CALL OUTP(X,PV,DERY,IHLF,NDIM,PRMT,NHIT) IF (NHIT.NE.0) RETURN IF(PRMT(5).NE.0) THEN RETURN ELSE IF((N-4).LT.0) THEN DO I=1,NDIM AUX(N,I)=PV(I) AUX(N+7,I)=DERY(I) ENDDO IF(N.LT.3) THEN DO I=1,NDIM DELT=AUX(9,I)+AUX(9,I) DELT=DELT+DELT PV(I)=AUX(1,I)+.33333333333D0*H*(AUX(8,I)+DELT+AUX(10,I)) ENDDO ELSE DO I=1,NDIM DELT=AUX(9,I)+AUX(10,I) DELT=DELT+DELT+DELT PV(I)=AUX(1,I)+.375D0*H*(AUX(8,I)+DELT+AUX(11,I)) ENDDO ENDIF ENDIF ENDDO ISW=6 C ****************************************************************** C C POSSIBLE BREAK POINT FOR LINKAGE C STARTING VALUES ARE COMPUTED C NOW START HAMMINGS MODIFIED PREDICTOR-CORRECTOR METHOD. C BLOCK 5 VS OLD LABELS 200_226 C C ****************************************************************** ISTEP=3 DO WHILE (ISW.GE.6) IF(ISW.EQ.6) THEN IF(N.EQ.8) THEN C N=8 CAUSES THE ROWS OF AUX TO CHANGE THEIR STORAGE LOCATIONS DO N=2,7 DO I=1,NDIM AUX(N-1,I)=AUX(N,I) AUX(N+6,I)=AUX(N+7,I) ENDDO ENDDO N=7 ENDIF C N LESS THAN 8 CAUSES N+1 TO GET N N=N+1 C COMPUTATION OF NEXT VECTOR PV DO I=1,NDIM AUX(N-1,I)=PV(I) AUX(N+6,I)=DERY(I) ENDDO X=X+H ISW=7 ELSE IF(ISW.EQ.7) THEN ISTEP=ISTEP+1 DO I=1,NDIM DELT=AUX(N-4,I)+1.3333333333D0*H*(AUX(N+6,I)+AUX(N+6,I) * -AUX(N+5,I)+AUX(N+4,I)+AUX(N+4,I)) PV(I)=DELT-.92561983471D0*AUX(16,I) AUX(16,I)=DELT ENDDO C PREDICTOR IS NOW GENERATED IN ROW 16 OF AUX, MODIFIED PREDICTOR C IS GENERATED I PV. DELT MEANS AN AUXILIARY STORAGE. CALL FCT(X,PV,DERY) C DERIVATIVE OF MODIFIED PREDICTOR IS GENERATED IN DERY DO I=1,NDIM DELT=.125D0*(9.D0*AUX(N-1,I)-AUX(N-3,I)+3.D0*H*(DERY(I) * +AUX(N+6,I)+AUX(N+6,I)-AUX(N+5,I))) AUX(16,I)=AUX(16,I)-DELT PV(I)=DELT+.7438016529D-1*AUX(16,I) ENDDO C TEST WHETHER H MUST BE HALVED OR DOUBLED DELT=0.D0 DO I=1,NDIM DELT=DELT+AUX(15,I)*DABS(AUX(16,I)) ENDDO ISW=8 ELSE IF(ISW.EQ.8) THEN IF(DELT.LT.PRMT(4).OR.IHLF1.EQ.5) THEN IHLF1=0 C H MUST NOT BE HALVED. THAT MEANS PV(I) ARE GOOD. CALL FCT(X,PV,DERY) CALL OUTP(X,PV,DERY,IHLF,NDIM,PRMT,NHIT) IF (NHIT.NE.0) RETURN IF(PRMT(5).NE.0.OR.IHLF.GE.11.OR.(H*(X-PRMT(2))).GE.0 * .OR.DABS(X-PRMT(2)).LT.0.1D0*DABS(H)) THEN 1150 FORMAT(I5) RETURN ELSE IF(DELT.LE..2D-1*PRMT(4).AND.IHLF.GT.0.AND.N.GE.7.AND. * ISTEP.GE.4) THEN C H COULD BE DOUBLED IF ALL NECESSARY PRECEEDING VALUES ARE AVAILABLE IMOD=ISTEP/2 IF((ISTEP-IMOD-IMOD).EQ.0) THEN H=H+H IHLF=IHLF-1 ISTEP=0 DO I=1,NDIM AUX(N-1,I)=AUX(N-2,I) AUX(N-2,I)=AUX(N-4,I) AUX(N-3,I)=AUX(N-6,I) AUX(N+6,I)=AUX(N+5,I) AUX(N+5,I)=AUX(N+3,I) AUX(N+4,I)=AUX(N+1,I) DELT=AUX(N+6,I)+AUX(N+5,I) DELT=DELT+DELT+DELT AUX(16,I)=8.962962963D0*(PV(I)-AUX(N-3,I))-3.361111111D0*H* * (DERY(I)+DELT+AUX(N+4,I)) ENDDO ISW=6 ELSE ISW=6 ENDIF ELSE ISW=6 ENDIF ENDIF ISW=6 ELSE ISW=9 ENDIF ELSE IF(ISW.EQ.9) THEN C H MUST BE HALVED IHLF=IHLF+1 IF(IHLF.LE.10) THEN ISW=10 ELSE ISW=8 IHLF1=5 ENDIF ELSE IF(ISW.EQ.10) THEN H=.5D0*H ISTEP=0 DO I=1,NDIM PV(I)=.390625D-2*(8.D1*AUX(N-1,I)+135.D0*AUX(N-2,I) * + 4.D1*AUX(N-1,I)+AUX(N-4,I))-.1171875D0*(AUX(N+6,I) * - 6.D0*AUX(N+5,I)-AUX(N+4,I))*H AUX(N-4,I)=.390625D-2*(12.D0*AUX(N-1,I)+135.D0*AUX(N-2,I)+ * 08.D0*AUX(N-3,I)+AUX(N-4,I))-.234375D-1*(AUX(N+6,I)+ * 8.D0*AUX(N+5,I)-9.D0*AUX(N+4,I))*H AUX(N-3,I)=AUX(N-2,I) AUX(N+4,I)=AUX(N+5,I) ENDDO X=X-H DELT=X-(H+H) CALL FCT(X,PV,DERY) DO I=1,NDIM AUX(N-2,I)=PV(I) AUX(N+5,I)=DERY(I) PV(I)=AUX(N-4,I) ENDDO DELT=DELT-(H+H) CALL FCT(X,PV,DERY) DO I=1,NDIM DELT=AUX(N+5,I)+AUX(N+4,I) DELT=DELT+DELT+DELT AUX(16,I)=8.9629696296D0*(AUX(N-1,I)-PV(I)) * - 3.3611111111D0*H*(AUX(N+6,I)+DELT+DERY(I)) AUX(N+3,I)=DERY(I) ENDDO ISW=7 ENDIF ENDDO END C----------------------------------------------------------------------- C-----------------------------------------------------------------------
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Updated 8/9/19, Cameron Crane
VOYAGER 1 ELAPSED TIME
--:--:--:--
Days: Hours:
Minutes: Seconds
*Since official launch
September 5, 1977, 12:56:00:00 UTC
*Since official launch
September 5, 1977, 12:56:00:00 UTC
VOYAGER 2 ELAPSED TIME
--:--:--:--
Days: Hours:
Minutes: Seconds
*Since official launch
August 20, 1977, 14:29:00:00 UTC
*Since official launch
August 20, 1977, 14:29:00:00 UTC
QUICK FACTS
Manufacturer:
Voyagers 1 and 2 were built in the Jet Propulsion
Laboratory in Southern California.
Mission Duration: 40+ years have elapsed for both Voyager 1 and Voyager 2 (both are ongoing).
Destination: Their original destinations were Saturn and Jupiter. Their current destination is interstellar space.
Mission Duration: 40+ years have elapsed for both Voyager 1 and Voyager 2 (both are ongoing).
Destination: Their original destinations were Saturn and Jupiter. Their current destination is interstellar space.