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tkmap.f
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C ---------------------------------------------------------------
PROGRAM TKMAP
C
C Program plots dropwindsonde mission flight tracks, and
C tabulates turn and drop points.
C ---------------------------------------------------------------
C Modified by Paul A. Leighton, Jul 2015, for corrections requested by
C Jason Dunion. See "! pal" comment on lines added or amended.
C
PARAMETER (MPTS = 1000, MAXTRAX = 4)
C
CHARACTER*1 TYPE(MPTS), ANS
CHARACTER*8 TAKEOFF
CHARACTER*12 FNAME
CHARACTER*30 STRING, STMNAME, STRINGA, STRINGZ
CHARACTER*50 LIBNAME, CURNAME
C
DIMENSION DTYPE(MPTS),
1 SPEED(MPTS)
LOGICAL SKIP
C
C Set LUs
C ------------------------------------------------
deg2rad=3.1415927/180.
OPEN(1, FILE = '/dev/tty') ! pal for print to screen.
LUFI = 14 !FLIGHT TRACK FILE
C
do IFILE=1,MAXTRAX
FNAME = 'current .ftk'
WRITE(FNAME(8:8),'(i1)')IFILE
C
C Calculate track distance tables
C -------------------------------
CALL TRACKDIS(IFILE,FNAME)
end do
STOP '99'
C
END
C
C ----------------------------------------------------
SUBROUTINE TRACKDIS(IFILE,FNAME)
C Computes great circle distance from files
C containing turns points of flight tracks.
C All latitude and longitude values must be positive.
C James Franklin 7/86, 2/89, 2/96
C ----------------------------------------------------
C2345678911234567892123456789312345678941234567895123456789612345678971X34567890
PARAMETER (MPTS = 100)
C
DIMENSION RLAT(MPTS),RLON(MPTS),IPOS(10),DTYPE(MPTS),SPEED(MPTS)
DIMENSION SRRAD(MPTS), SRAZM(MPTS)
C
CHARACTER*1 TYPE(MPTS), FLAG(MPTS), TEE
CHARACTER*7 FNAMEP
CHARACTER*8 TAKEOFF,FNAMEHUR
CHARACTER*10 FILEOUT,FILEOUTD
CHARACTER*12 FNAME
CHARACTER*30 STRING,NAME(10),STMNAME,STRINGA,STRINGZ
CHARACTER*30 TTYP
LOGICAL globalhawk, climb, ipset, climbdleg ! pal used to not include inserted drops in turn file.
C
160 FORMAT(1X,I2,A1,4X,A16,12X,1X,f5.0,3X,f5.0,4X,I2,':',I2.2)
161 FORMAT(1X,I2,A1,2X,2(I4,1X,I2.2,2X),12X,
* 1X,f5.0,3X,f5.0,4X,I2,':',I2.2)
162 FORMAT(1X,I2,A1,2X,2(I4,1X,I2.2,2X),
* 2X,I3,'/',i3.3,4X,f5.0,3X,f5.0,4X,I2,':',I2.2)
171 FORMAT(1X,I2,A1,2X,2(I4,1X,I2.2,2X),13X,I2,':',I2.2)
172 FORMAT(1X,I2,A1,2X,2(I4,1X,I2.2,2X),3X,I3,'/',I3.3,
1 3X,I2,':',I2.2)
500 FORMAT(2F8.3,1x,a1)
501 FORMAT(2F8.3)
901 FORMAT(1X,72("="),/,
* 1x,'MISSION PLAN: ',a20,//,
* 1X,'Prepared by the Hurricane Research Division',
* 1x,'File: ',A,//,
* 1X,'Aircraft: N',i2,'RF Proposed takeoff: ',A8,/,
* 1x,72("="),///
* 1x,A30,/)
902 FORMAT(1X,
*'===========================================================')
903 FORMAT
* (1X,' # LAT LON RAD/AZM LEG TOTAL TIME'/
* ' (d m) (d/m) (nm/dg) (nm) (nm) (h:mm)')
904 FORMAT(1X,
*'-----------------------------------------------------------')
907 FORMAT(1X,'==========================================')
908 FORMAT(1X,' # LAT LON RAD/AZM TIME',/,
* ' (d m) (d m) (nm/dg) (h:mm)')
909 FORMAT(1X,'------------------------------------------')
910 FORMAT(1X,'------------------------------------------')
C2345678911234567892123456789312345678941234567895123456789612345678971X34567890
C
TEE='T'
LUT = 8
LUP = 9 ! pal
LUFO = 7
LUFI = 14
deg2rad=3.1415927/180. ! pal
globalhawk = .false. ! pal
climb = .false. ! pal
ipset = .true. ! pal
climbdleg = .true. ! pal
inserted = 0
C Get track file name, reset variables
C ------------------------------------
C2345678911234567892123456789312345678941234567895123456789612345678971X34567890
OPEN(LUFI,FILE=FNAME,STATUS='OLD',ERR=9010)
WRITE(1, '(1X, A12)') FNAME
WRITE(FILEOUT,'("turns",I1.1,".txt")') IFILE
OPEN(LUFO,FILE=FILEOUT,STATUS='UNKNOWN',ERR=9011)
WRITE(FILEOUTD,'("drops",I1.1,".txt")') IFILE
OPEN(LUT,FILE=FILEOUTD,STATUS='UNKNOWN',ERR=9012)
WRITE(FNAMEP,'("points",I1.1)') IFILE
OPEN(LUP,FILE=FNAMEP,STATUS='UNKNOWN',ERR=9013)
WRITE(FNAMEHUR,'("hurrloc",I1.1)') IFILE
OPEN(UNIT=72,FILE=FNAMEHUR,STATUS='UNKNOWN',ERR=9014)
C
DO L = 1,MPTS
FLAG(L) = ' '
END DO
C
C Read header line
C ----------------
READ(LUFI,'(I2,1X,8A,1X,A20)') IAC,TAKEOFF,STMNAME
WRITE(1, '(I2, 1X, 8A, 1X, A20)') iac, takeoff, stmname ! pal
IALT1 = 0
IALT2 = 0
IF (IAC.EQ.42 .OR. IAC.EQ.43) THEN
globalhawk = .true. ! pal boolean for non-included drops to turns.
DO IJK=1,MPTS
SPEED(IJK) = 330. ! jpd modified to correct for faster ferry speeds
END DO
SPEED(1) = 330.
IALT1 = 0
IALT2 = 10
ENDIF
IF (IAC.EQ.49) THEN
globalhawk = .true. ! pal boolean for non-included drops to turns.
DO IJK=1,MPTS
SPEED(IJK) = 442.
END DO
IALT1 = 41
IALT2 = 45
ENDIF
c
c 50 is AFC130-J
c
if (iac.eq.50)then
globalhawk = .true. ! pal boolean for non-included drops to turns.
DO IJK=1,MPTS
SPEED(IJK) = 290.
END DO
ialt1 = 18
ialt2 = 25
endif
c
c 51 is NASA DC-8
c
if (iac.eq.51)then
globalhawk = .true. ! pal boolean for non-included drops to turns.
DO IJK=1,MPTS
SPEED(IJK) = 440.
END DO
ialt1 = 18
ialt2 = 38
endif
c
c 52 is Global Hawk
c
if (iac.eq.52)then
globalhawk = .true. ! pal boolean for non-included drops to turns.
DO IJK=1,MPTS
SPEED(IJK) = 335.
END DO
ialt1 = 55
ialt2 = 60
endif
c
c 57 is AF WB-57
c
if (iac.eq.57)then
globalhawk = .true. ! pal sets 57 to act same as globalhawk for inserts
DO IJK=1,MPTS
SPEED(IJK) = 300.
END DO
ialt1 = 40
ialt2 = 60
endif
speed(2)=speed(1)
I = 0
DLEG = 0.
TOTAL = 0.
TIME = 0.
NS = 0
C
C2345678911234567892123456789312345678941234567895123456789612345678971X34567890
C
C Begin reading in input file
C ---------------------------
INSERT = 0
100 I = I+1
READ(LUFI,'(A1,1X,A)',END=800) TYPE(I), STRING
SRRAD(I) = -99.
CALL UPPERCASE(TYPE(I))
DO L = 1,20
CALL UPPERCASE(STMNAME(L:L))
CALL UPPERCASE(STRING(L:L))
END DO
C
FLAG(I) = ' '
IF (TYPE(I).EQ.'E' .OR. TYPE(I).EQ.'F') FLAG(I)='E'
IF (TYPE(I).EQ.'I') THEN
READ(STRING,*) INSERT,ALT
WRITE(1, '("I", I2, 1X, F7.1)') insert, alt ! pal
do ijk=i,i+insert
IF((IAC.EQ.42.OR.IAC.EQ.43.OR.IAC.EQ.57).AND.I.GT.3)
1 CALL GETSPEED(IAC,ALT,SPEED(ijk))
end do
rlat(i) = insert
rlon(i) = alt
GOTO 100
ENDIF
C
IF (TYPE(I).EQ.'C') THEN
READ(STRING,*) IALT1,IALT2
I = I-1
GOTO 100
ENDIF
C
IF (TYPE(I).EQ.'H') THEN
read(string,*,err=120)rlat(i),rlon(i),isdir,isspd
sdir=float(isdir)
sspd=float(isspd)
call uvcomp(sdir,sspd)
stormu=-sdir
stormv=-sspd
OPEN(UNIT=72,FILE=FNAMEHUR)
SLAT = RLAT(I)
SLON = -RLON(I)
write(72,*)slat,slon
close(72)
goto 100
ENDIF
C
C Position input is a name or stmrel position
C -------------------------------------------
120 IF (TYPE(I).EQ.'S') THEN
READ(STRING(1:20),*) RDIS,THETA,ALT
WRITE(1, '("S", 3(F6.0, 1X))') rdis, theta, alt ! pal
IF((IAC.EQ.42.OR.IAC.EQ.43.OR.IAC.EQ.57).AND.I.GT.3)
1 CALL GETSPEED(IAC,ALT,SPEED(I))
RDIS = RDIS*111.1/60.
CALL SRLATLON(SLAT,SLON,THETA,RDIS,XLAT,XLON)
rlat(i)=xlat
rlon(i)=-xlon
rlat(i)=(xlat-slat)*60. ! pal
rlon(i)=(xlon-slon)*60.*cos(deg2rad*0.5*(xlat+slat)) ! pal
FLAG(I) = 'S'
SRRAD(I) = RDIS*60./111.1
SRAZM(I) = THETA
insert = 0
GOTO 100
ENDIF
IF (TYPE(I).EQ.'A'.OR.TYPE(I).EQ.'Z')THEN
CALL CITY(0,STRING,RLAT(I),RLON(I))
WRITE(1, '(A1, 1X, A30)') type(i), string ! pal
IF (RLAT(I).EQ.-99.) GOTO 900
SRRAD(I) = -99.
NS = NS+1
IPOS(NS) = I
IF(TYPE(I).EQ.'A') THEN
STRINGA=STRING
name(ns) = string ! pal set first name
ENDIF
IF(TYPE(I).EQ.'Z')then
stringz = string ! pal from above but set name(ns) only at end
IF(IAC.EQ.42.OR.IAC.EQ.43)SPEED(I)=330.
IF(IAC.EQ.57)SPEED(I)=300. ! jpd modified
IF (insert.GT.0.AND.(type(i-2).NE.'S')) THEN
ipos(ns) = i + insert - 1
name(ns) = string
GOTO 130 ! pal insert final leg
ENDIF
name(ns) = string
insert = 0
GOTO 800
ENDIF
goto 100
ELSE
READ(STRING,*,ERR=120) RLAT(I),RLON(I),ALT
WRITE(1, '(3(F8.2, 1X))') rlat(i), rlon(i), alt ! pal
IF((IAC.EQ.42.OR.IAC.EQ.43.OR.IAC.EQ.57).AND.I.GT.3)
1 CALL GETSPEED(IAC,ALT,SPEED(I))
IF(insert.eq.0) goto 100
ENDIF
C
C
130 CONTINUE
DTYPE(I) = 1.0
IF (INSERT.GT.0) THEN
K = I+INSERT-1
RLAT(K) = RLAT(I)
RLON(K) = RLON(I)
TYPE(K) = TYPE(I)
FLAG(K) = FLAG(I)
DTYPE(K) = DTYPE(I)
SRRAD(K) = SRRAD(I)
SRAZM(K) = SRAZM(I)
RLATINC = (RLAT(k) - RLAT(I-2))/FLOAT(INSERT+1)
RLONINC = (RLON(k) - RLON(I-2))/FLOAT(INSERT+1)
DO L = 1,INSERT
J = I-2+L
RLAT(J) = RLAT(I-2)+FLOAT(L)*RLATINC
RLON(J) = RLON(I-2)+FLOAT(L)*RLONINC
TYPE(J) = 'D'
DTYPE(J) = 1.0
SRRAD(J) = -99.
flag(j) = 'I' ! pal- all should be labelled 'I' not 'S' or 'D'
END DO
I = K
INSERT = 0
ENDIF
C
IF (I.GT.100) STOP '100'
IF (TYPE(I).NE.'Z') GOTO 100
WRITE(1, '(A1, 1X, A30)') type(i), string ! pal
C
NT = I
C
C2345678911234567892123456789312345678941234567895123456789612345678971X34567890
C
C -----------------------------------------------------------
C Done reading input file.
C Compute track distance for all turn points and print tables
C -----------------------------------------------------------
C
800 CONTINUE
TTYP = 'TRACK DISTANCE TABLE'
NT = I
WRITE(LUFO,901) STMNAME,FNAME,IAC,TAKEOFF,TTYP
WRITE(1, 901) stmname, fname, iac, takeoff, ttyp ! pal
WRITE(LUFO,902)
WRITE(LUFO,903)
WRITE(LUFO,904)
TTYP = 'DROP LOCATIONS'
WRITE(LUT,901) STMNAME,FNAME,IAC,TAKEOFF,TTYP
WRITE(LUT,907)
WRITE(LUT,908)
WRITE(LUT,909)
C WRITE(LUT,'(/)')
C
LTURN = -1
IC = 0
LDROP = 0 ! jpd changed from “1” to “0” to set IP as waypoint #1: 6-10-2016
TOTAL = 0.
subtotal = 0.0 ! pal keeps track of legs of inserted drops.
TIME = 0.
i = 0
dleg52 = 0.0
150 i = i + 1
subtotal = total
IF (TYPE(I).EQ.'X' .OR. TYPE(I).EQ.'H') GOTO 150
IF (type(i).EQ.'I') THEN ! insert storm relative points count read
insert = rlat(i)
inserted = insert
alt = rlon(i)
GOTO 150
ENDIF
IL = IC ! Current index
IC = I ! Last index
IF (IL .EQ. 0) IL = IC
LTURN = LTURN+1
if(type(i).eq.'S')then
temptime=time
C I have no idea why this is being done in a loop of 5 but it matters
C for the results to be the same as before??? pal
Do ijkl=1,5
c calculate storm location at time
stormlat=slat+temptime*stormv/60.
stormlon=slon+temptime*stormu/(60.*cos(deg2rad*stormlat))
c
c calculate aircraft location in relation to storm
temprlat=stormlat+rlat(i)/60.
temprlon=-(stormlon+rlon(i)/(60.*cos(deg2rad*temprlat)))
dleg=gcdistance(temprlat,temprlon,rlat(il),rlon(il))
temptime=time+dleg/speed(i)
ENDDO ! ijkl 1->5 loop
rlat(ic)=temprlat
rlon(ic)=temprlon
dleg=gcdistance(rlat(ic),rlon(ic),rlat(il),rlon(il))
total=total+dleg
time=time+dleg/speed(i)+0.0167
subtotal = subtotal + dleg
IF (insert.NE.0) THEN ! pal insert storm relative points here
dlegout = dleg / (insert + 1)
time = time - dleg/speed(i)
subtotal = subtotal - dleg
newnt = nt + insert - 1
dtype(i) = 1.0
k = i + insert - 1
DO j = newnt, k, -1 ! pal move points to leave space for inserts
l = j - insert + 1
rlat(j) = rlat(l)
rlon(j) = rlon(l)
type(j) = type(l)
flag(j) = flag(l)
dtype(j) = dtype(l)
srrad(j) = srrad(l)
srazm(j) = srazm(l)
speed(j) = speed(l)
ENDDO
rlatinc = (rlat(k) - rlat(i-2))/FLOAT(insert + 1)
rloninc = (rlon(k) - rlon(i-2))/FLOAT(insert + 1)
temptime = time
stormlat=slat+temptime*stormv/60.
stormlon=slon+temptime*stormu/(60.*cos(deg2rad*stormlat))
DO l = 1, insert
j = i - 2 + l
rlat(j) = rlat(i - 2) + FLOAT(l) * rlatinc
rlon(j) = rlon(i - 2) + FLOAT(l) * rloninc
xlat = rlat(j) ! pal comments out to test Aug 3
xlon = -rlon(j) ! pal comments out to test Aug 3
temprlat=stormlat+rlat(j)/60.
temprlon=-(stormlon+rlon(j)/(60.*cos(deg2rad*temprlat)))
dlegtime=gcdistance(temprlat,temprlon,rlat(j-1),rlon(j-1))
temptime=time+dlegtime/speed(j - 1) ! pal change i to j - 1
type(j) = 'D'
dtype(j) = 1.0
srrad(j) = -99.
flag(j) = 'I' ! pal- all should be labelled 'I' not 'S' or 'D'
time = time + dlegout / speed(j) ! pal
subtotal = subtotal + dlegout ! pal ? total = total + dleg ???
CALL DGMN(rlat(j), lad, lam)
CALL DGMN(rlon(j), lod, lom)
CALL DGMN(time, ith, itm)
ldrop = ldrop + 1
if((lturn.eq.1 .OR. ldrop.eq.1) .AND. ipset) then ! jpd changed from “2” to “1” to set IP as waypoint #1: 6-10-2016
iph=ith
ipm=itm
ipset=.false.
endif
WRITE(LUP, 501) rlat(j), rlon(j) ! output to points file
IF (.NOT. globalhawk)
+ WRITE(lufo, 161) lturn, flag(j), lad, lam, lod, lom,
+ dlegout, subtotal, ith, itm
WRITE(lut, 171) ldrop, flag(j), lad, lam, lod, lom,
+ ith, itm
c lturn = lturn + 1 ! pal commented out to not count SR inserts as WPs
ENDDO ! pal inserts
indexk = 21 ! jason testing 10 aug 2016
dleg52 = 0
total = subtotal + dlegout ! pal
subtotal=0 ! pal inserts to test Aug 3
time = time + dlegout / speed(j) ! pal just added
dlegout = 0 ! pal added for SR insert testing 10 aug 2016
i = k
ic = ic+insert-1 ! pal changes on 12 aug 2016
insert = 0
nt = newnt
ipos(ns) = nt
ENDIF ! pal storm relative insertions
elseif(type(i).ne.'I'.and.type(i).ne.'D')then
DLEG = GCDISTANCE(RLAT(IC),RLON(IC),RLAT(IL),RLON(IL))
TOTAL = TOTAL+DLEG
time=time+dleg/speed(i)+0.0167
subtotal = subtotal + dleg
IF ((type(i).EQ.'Z').AND.(insert.NE.0)) THEN ! jpd start
dlegout = dleg / (insert + 1)
time = time - dleg/speed(i)
subtotal = subtotal - dleg
newnt = nt + insert - 1
dtype(i) = 1.0
k = i + insert - 1
DO j = newnt, k, -1 ! pal move points to leave space for inserts
l = j - insert + 1
rlat(j) = rlat(l)
rlon(j) = rlon(l)
type(j) = type(l)
flag(j) = flag(l)
dtype(j) = dtype(l)
srrad(j) = srrad(l)
srazm(j) = srazm(l)
speed(j) = speed(l)
ENDDO
rlatinc = (rlat(k) - rlat(i-2))/FLOAT(insert + 1)
rloninc = (rlon(k) - rlon(i-2))/FLOAT(insert + 1)
temptime = time
stormlat=slat+temptime*stormv/60.
stormlon=slon+temptime*stormu/(60.*cos(deg2rad*stormlat))
DO l = 1, insert
j = i - 2 + l
rlat(j) = rlat(i - 2) + FLOAT(l) * rlatinc
rlon(j) = rlon(i - 2) + FLOAT(l) * rloninc
xlat = rlat(j) ! pal comments out to test Aug 3
xlon = -rlon(j) ! pal comments out to test Aug 3
temprlat=stormlat+rlat(j)/60.
temprlon=-(stormlon+rlon(j)/(60.*cos(deg2rad*temprlat)))
dlegtime=gcdistance(temprlat,temprlon,rlat(j-1),rlon(j-1))
temptime=time+dlegtime/speed(j - 1) ! pal change i to j - 1
type(j) = 'D'
dtype(j) = 1.0
srrad(j) = -99.
flag(j) = 'I' ! pal- all should be labelled 'I' not 'S' or 'D'
time = time + dlegout / speed(j) ! pal
subtotal = subtotal + dlegout ! pal ? total = total + dleg ???
CALL DGMN(rlat(j), lad, lam)
CALL DGMN(rlon(j), lod, lom)
CALL DGMN(time, ith, itm)
ldrop = ldrop + 1
if((lturn.eq.1 .OR. ldrop.eq.1) .AND. ipset) then ! jpd changed from “2” to “1” to set IP as waypoint #1: 6-10-2016
iph=ith
ipm=itm
ipset=.false.
endif
write(6,*)' 1, i, type(i)=',i,type(i)
write(6,501) rlat(j), rlon(j)
WRITE(LUP, 501, err=9013) rlat(j), rlon(j) ! output to points file
IF (.NOT. globalhawk)
+ WRITE(lufo, 161) lturn, flag(j), lad, lam, lod, lom,
+ dlegout, subtotal, ith, itm
WRITE(lut, 171) ldrop, flag(j), lad, lam, lod, lom,
+ ith, itm
lturn = lturn + 1
ENDDO ! pal inserts
dleg52 = 0 ! pal added for testing 10 aug 2016
total = subtotal + dlegout ! pal
time = time + dlegout / speed(j) ! pal just added
i = k
insert = 0
nt = newnt
ipos(ns) = nt
ENDIF ! pal storm relative insertions
else
IF (iac.EQ.52 .OR. iac.EQ.57 .OR. iac.EQ.51 .OR. iac.EQ.50 .OR.
+ iac.EQ.49 .OR. iac.EQ.43 .OR. iac.EQ.42) THEN
lturn = lturn - 1 ! pal sets to exclude interpolated points as WPs
ENDIF
DLEG = GCDISTANCE(RLAT(IC),RLON(IC),RLAT(IL),RLON(IL))
dleg52 = dleg52+dleg
TOTAL = TOTAL+DLEG
subtotal = subtotal + dleg
time=time+dleg/speed(i)
endif
IF (iac.eq.52) THEN ! jpd modified to add 30-min to the GH track after take-off (GH climb-out maneuvers)
IF ((type(i).eq.'A')) THEN
climb=.true.
endif
IF ((type(i).eq.'Z')) THEN ! jpd modified to add 30-min to the GH track just before landing (GH decent maneuvers)
time=time+0.5
dleg=dleg+(335*0.5)
total= total+(335*0.5)
endif
endif
CALL DGMN(RLAT(I),LAD,LAM)
CALL DGMN(RLON(I),LOD,LOM)
CALL DGMN(TIME,ITH,ITM)
IX = 0
DO 155 L = 1,NS
IF (IPOS(L).EQ.I) IX = L
155 CONTINUE
C write(6,*)' 2, i, type(i)=',i,'/',type(i),'/'
write(6,501) rlat(i), rlon(i)
if(type(i).ne.'T')write(LUP,501,err=9013)rlat(i),rlon(i)
if(type(i).eq.'T')write(LUP,500,err=9013)rlat(i),rlon(i),TEE
if((lturn.eq.1 .OR. ldrop.eq.1) .AND. ipset) then ! jpd changed from “2” to “1” to set IP as waypoint #1
iph=ith
ipm=itm
ipset=.false.
endif
IF (.NOT.((TYPE(I).EQ.'D').AND.globalhawk)) THEN ! pal
dlegout = subtotal
IF (iac.EQ.52 .OR. iac.EQ.57 .OR. iac.EQ.51 .OR. iac.EQ.50 .OR.
+ iac.EQ.49 .OR. iac.EQ.43 .OR. iac.EQ.42) THEN ! pal sets to exclude interpolated points as WPs
dleg=dleg+dleg52 ! pal comment out Aug 3
dleg52=0 ! pal comment out Aug 3
ENDIF
IF ((LTURN.EQ.1).AND.(IAC.EQ.52)) THEN ! jpd adds to account for climb out dx to track for WP 1
dleg=dleg+(335*0.5)
total= total+(335*0.5)
ENDIF
IF (IX.NE.0) THEN
WRITE(LUFO,160) LTURN,FLAG(I),NAME(IX),DLEG,TOTAL,ITH,ITM
ELSE
IF (SRRAD(I).GE.0.) THEN
WRITE(LUFO,162) LTURN,FLAG(I),LAD,LAM,LOD,LOM,
* INT(SRRAD(I)),INT(SRAZM(I)),DLEG, TOTAL,ITH,ITM
ELSE
IF (globalhawk) THEN
dleg = dleg*(inserted+1) ! pal adds to track inserted legs
inserted = 0
ENDIF
WRITE(LUFO,161) LTURN,FLAG(I),LAD,LAM,LOD,LOM,DLEG,
* TOTAL,ITH,ITM
ENDIF
ENDIF
subtotal = 0.0
ENDIF ! pal
IF (iac.eq.52 .AND. climb) THEN ! jpd modified to add 30-min to the GH track after take-off (GH climb-out maneuvers)
time=time+0.5
climb=.false.
ENDIF
IF(type(i).eq.' '.or.type(i).eq.'D'.or.type(i).eq.'E'
1 .OR.type(i).eq.'S'.or.type(i).eq.'I')then
LDROP = LDROP+1
if((lturn.eq.1 .OR. ldrop.eq.1) .AND. ipset) then ! jpd changed from “2” to “1” to set IP as waypoint #1
iph=ith
ipm=itm
ipset=.false.
endif
IF (SRRAD(I).GE.0.) THEN
isrrad=srrad(i)
israzm=srazm(i)
write(lut,172)LDROP,flag(i),lad,lam,lod,lom,
* isrrad,israzm,ith,itm
ELSE
WRITE(LUT,171) LDROP,FLAG(I),LAD,LAM,LOD,LOM,ITH,ITM
ENDIF
ENDIF
IF (i.LT.nt) GOTO 150 ! pal getting out early?
WRITE(LUFO,904)
C
C Now print table for drop locations
C ----------------------------------
WRITE(LUT,910)
c
c Now print MTS information in drops and turns files
WRITE(LUFO,8011)STMNAME,FNAME,IAC,STRINGA,TAKEOFF,STRINGZ,
1 IPH,IPM,ITH,ITM
8011 FORMAT(//,1X,72("*"),/,
1 ' MISSION PLAN: ',a20,/,
2 ' Prepared by the Hurricane Research Division File: ',A,/,
3 ' Aircraft: N',i2,'RF',/,
4 ' Proposed takeoff: ',A8,' ',A8,/,
5 ' Proposed recovery: ',A8,/,
6 ' Time to IP: ',I2,':'I2,/,
7 ' Mission Duration: ',I2,':'I2,/,
8 1X,72("*"))
C
C All done, return
C ----------------
CLOSE(LUFI)
CLOSE(LUFO)
CLOSE(LUT)
RETURN
C
900 WRITE(LUT,*) ' OPEN OR READ OR CITY ERROR IN SUBROUTINE TRACK'
STOP '00'
9010 STOP '10'
9011 STOP '11'
9012 STOP '12'
9013 STOP '13'
9014 STOP '14'
END
C
C2345678911234567892123456789312345678941234567895123456789612345678971X34567890
SUBROUTINE DGMN(DDEG,IDEG,MIN)
IDEG = ABS(INT(DDEG))
MIN = NINT((ABS(DDEG)-IDEG)*60.)
IF (MIN.EQ.60) THEN
MIN = 0
IDEG = IDEG+1.
ENDIF
IF (DDEG.LT.0.) IDEG = -IDEG
RETURN
END
C --------------------------------------------------------
C2345678911234567892123456789312345678941234567895123456789612345678971X34567890
C SONDELIB
C
C Collection of subroutines relating to soundings.
C This files has three main sections:
C
C 1) Routines relating to Ooyama's spline filtering.
C 2) Mathematical or meteorological routines
C 3) Routines for message decoding
C
C Recent revision history:
C
C 12/17/99: Modified dropsonde TEMP DROP to HSA format
C conversion routine to allow for decoding of:
C 1) surface significant wind data following
C the "21212" indicator
C 2) extrapolated level data following both
C the "51515" indicator and doubtful
C temperature or height groups (SEF)
C
C -----------------------------------------------------------------
SUBROUTINE STMREL(DAYMN,DAYOB,GMTOB,XD,YD,NFD,DAYSTM,GMTSTM,
* XSTM,YSTM,DAY0,GMT0)
C -----------------------------------------------------------------
C
C
DIMENSION DAYSTM(NFD),GMTSTM(NFD),XSTM(NFD),YSTM(NFD)
DIMENSION DTFIX(500)
LOGICAL MATCH
C
MATCH=.FALSE.
NFIX = NFD
C
C
C Find storm position at reference time
C -------------------------------------
C
DO 110 L=1,NFIX
IF (DAY0.EQ.DAYSTM(L).AND.GMT0.EQ.GMTSTM(L)) THEN
XSTM0=XSTM(L)
YSTM0=YSTM(L)
MATCH=.TRUE.
GOTO 120
ENDIF
110 CONTINUE
120 IF (.NOT.MATCH) THEN
WRITE(6,'("*** BAD REFERENCE TIME IN STMREL ***")')
STOP
ENDIF
C
C
200 CALL XTRTIME(DAYMN,000.0,IYMN,IMMN,IDMN,HRMN)
DO 210 N=1,NFIX
CALL XTRTIME(DAYSTM(N),GMTSTM(N),IYR,IMO,IDA,HR)
CALL DIFTIME(IYMN,IMMN,IDMN,HRMN,IYR,IMO,IDA,HR,DTFIX(N))
210 CONTINUE
C
C
CALL XTRTIME(DAYOB,GMTOB,IYR,IMO,IDA,HR)
CALL DIFTIME(IYMN,IMMN,IDMN,HRMN,IYR,IMO,IDA,HR,DTOB)
NFIX1=NFIX-1
C
DO 300 N=1,NFIX1
NF=N
IF (DTOB.GE.DTFIX(N) .AND. DTOB.LE.DTFIX(N+1)) GOTO 310
300 CONTINUE
C
WRITE(6,301) DAYOB,GMTOB
301 FORMAT(' **** CANNOT INTERPOLATE FIXES FOR ',I6,1X,I4,' ****',/,
* ' **** PROGRAM ABORTING ****',//)
STOP
C
C
310 DT=DTFIX(NF+1)-DTFIX(NF)
IF (ABS(DT) .LT. 1.E-4) GOTO 910
RAT = (DTOB-DTFIX(NF))/(DTFIX(NF+1)-DTFIX(NF))
XSTOB = XSTM(NF)+(XSTM(NF+1)-XSTM(NF))*RAT
YSTOB = YSTM(NF)+(YSTM(NF+1)-YSTM(NF))*RAT
XD = XD - XSTOB + XSTM0
YD = YD - YSTOB + YSTM0
RETURN
C
C
C Errors
C ------
C
910 WRITE(6,911) NF,DTFIX(NF),DTFIX(NF+1)
911 FORMAT("**** FIX TIMES ARE EQUAL IN STMREL***",I5,2F15.5)
STOP
END
C
C
C
C --------------------------------------------
SUBROUTINE XTRTIME(DATE,GMT,IYR,IMO,IDA,HR)
C --------------------------------------------
C
IYR=INT(DATE/10000.)
IMO=INT((DATE-FLOAT(IYR)*10000.)/100.)
IDA=INT(DATE-FLOAT(IYR)*10000.-IMO*100.)
HR=FLOAT(NINT(GMT/100.-0.3))
HR=HR+(GMT-HR*100.)/60.
RETURN
END
C
C
C
C --------------------------------------------------------
SUBROUTINE DIFTIME(IYZ,IMZ,IDZ,HRZ,IYX,IMX,IDX,HRX,DHR)
C --------------------------------------------------------
C
DIMENSION MODA(12)
DATA MODA/31,28,31,30,31,30,31,31,30,31,30,31/
C
DHR=0.0
IDZZ=IDZ
IMZZ=IMZ
HRZZ=HRZ
C
IF(IYZ.EQ.IYX) GOTO 100
DHR=24.-HRZZ+FLOAT((MODA(IMZZ)-IDZZ)*24+MAX0(IYX-(IYZ+1),0)*8760)
IMZZ=MOD(IMZZ+1,12)
IDZZ=1
HRZZ=0.0
C
IF (IMZZ.EQ.1) GOTO 100
DO I=IMZZ,12
DHR=DHR+FLOAT(MODA(I)*24)
END DO
IMZZ=1
C
100 IF (IMZZ.EQ.IMX) GOTO 200
DHR=DHR+FLOAT((MODA(IMZZ)-IDZZ)*24)+24.-HRZZ
IMZZ1=IMZZ+1
C
IF (IMZZ1 .GE. IMX) GOTO 120
IMX1=IMX-1
DO I=IMZZ1,IMX1
DHR=DHR+FLOAT(MODA(I)*24)
END DO
C
120 IMZZ=IMZZ1
IDZZ=1
HRZZ=0.0
C
200 DHR=DHR+FLOAT((IDX-IDZZ-1)*24)+24.-HRZZ+HRX
RETURN
END
C
C
C
C --------------------------------------------------
SUBROUTINE DAYCMPR(FLID,DATE,TODAY,TOMORROW)
C --------------------------------------------------
C
C
DIMENSION IMONTH(12)
LOGICAL TODAY,TOMORROW
DATA IMONTH/31,28,31,30,31,30,31,31,30,31,30,31/
C
TODAY = .FALSE.
TOMORROW = .FALSE.
C
C SEPERATE DATES INTO YEAR,MONTH,DAY
C ----------------------------------
C
IYR = INT(FLID/10000.)
IMN = INT(FLID/100.) - (IYR*100.)
IDY = FLID - (IYR*10000.) - (IMN*100.)
JYR = INT(DATE/10000.)
JMN = INT(DATE/100.) - (JYR*100.)
JDY = DATE - (JYR*10000.) - (JMN*100.)
IF (MOD(IYR,4).EQ.0) IMONTH(2) = 29
C
C FIND IF SAME DAY OR NEXT
C ------------------------
C
IF (FLID.EQ.DATE) TODAY = .TRUE.
IF (FLID+1.EQ.DATE) TOMORROW = .TRUE.
C
C CHECK FOR MONTHLY OR YEARLY FLIP OVERS
C --------------------------------------
C
IF (JDY.EQ.1.AND.IDY.EQ.IMONTH(IMN)) THEN
IF (JMN.EQ.IMN+1) TOMORROW = .TRUE.
IF (JMN.EQ.1.AND.IMN.EQ.12) THEN
IF (JYR.EQ.IYR+1) TOMORROW = .TRUE.
ENDIF
ENDIF
RETURN
END
C
C
C
C --------------------------------------------------------
SUBROUTINE LOPASS(GIN,GOUT,NMAX,FRAC,NTRM)
C Complete symmetric filter with multiplicative adjustment
C --------------------------------------------------------
C
C
PARAMETER(MTERMS=100)
DIMENSION GIN(NMAX),GOUT(NMAX),WT(MTERMS)
DATA PI/3.1415926535/
IPRT=1
NTRM1=NTRM+1
NMAX1=NMAX-NTRM
OMCUT=PI*FRAC
WTO=FRAC
C
C Endpoints
C ---------
C
GOUT(1)=GIN(1)
GOUT(NMAX)=GIN(NMAX)
C
C
DO 40 L=2,NMAX-1
SUM=0.0
MTRM=NTRM
IF(L.LE.NTRM) MTRM=L-1
IF(L.GE.NMAX+1-MTRM) MTRM=NMAX-L !FIX 2/17/88
C
C Calculate Weights
C -----------------
C
WTO = FRAC
WFSUM = 0.0
DO 20 N=1,MTRM
FAC=FLOAT(N)*2.*PI/(2.*MTRM+1)
WT(N)=SIN(FLOAT(N)*OMCUT)/(PI*FLOAT(N))*SIN(FAC)/FAC
WFSUM=WFSUM+2.0*WT(N)
20 CONTINUE
C
WFSUM=WFSUM+WTO
WTO=WTO/WFSUM
C
DO N=1,MTRM
WT(N)=WT(N)/WFSUM
END DO
DO N=1,MTRM
SUM=SUM+(GIN(L-N)+GIN(L+N))*WT(N)
END DO
GOUT(L)=SUM+GIN(L)*WTO
40 CONTINUE
RETURN
END
C
C
C
C --------------------------------------------
SUBROUTINE GAP(X,NT,IBGN,IEND,NGAPS,BAD)
C --------------------------------------------
C
PARAMETER (MXGPS = 100)
C
DIMENSION X(NT),IBGN(MXGPS),IEND(MXGPS)
LOGICAL LAST
C
COMMON /PARAM/ LUT,LUFI,LUFX,LUFW,LUFP,LUFO,LUPR,
* NPLTFORM,NSNDTYPE,FALLRATE,DATARATE
C
IGAP=0
LAST=.FALSE.
NGAPS=0
C
DO 5 L=1,MXGPS
IBGN(L)=0
IEND(L)=0
5 CONTINUE
C
DO 10 L=1,NT
IF (X(L).GT.BAD) THEN
IF (LAST) GO TO 10
IGAP=IGAP+1
IBGN(IGAP)=L
LAST=.TRUE.
GO TO 10
ELSE
IF(.NOT.LAST) GO TO 10
IEND(IGAP)=L-1
LAST=.FALSE.
GO TO 10
ENDIF
10 CONTINUE
C
IF(X(NT).GT.BAD) IEND(IGAP)=NT
NGAPS=IGAP-1
IF (NGAPS.LT.0) NGAPS=0
C
IF (NGAPS.GT.MXGPS) THEN
WRITE(LUT,'(/,
* " *** FATAL ERROR: TOO MANY GAPS IN SOUNDING ***")')
STOP
ENDIF
C
RETURN
END
C
C
C
FUNCTION GCDISTANCE(YY,XX,BB,AA)
DOUBLE PRECISION X,Y,A,B
PI = ACOS(-1.0)
REARTHKM = 6378.163
REARTHNM = REARTHKM*60./111.12
IF (YY.EQ.BB .AND. XX.EQ.AA) THEN
GCDISTANCE = 0.
RETURN
ENDIF
Y=YY*2.0*PI/360.
X=XX*2.0*PI/360.
A=AA*2.0*PI/360.
B=BB*2.0*PI/360.
ANGLE=DACOS(DCOS(A-X)*DCOS(Y)*DCOS(B)+DSIN(Y)*DSIN(B))
GCDISTANCE=ANGLE*REARTHNM
RETURN
END
C
C
C
C ------------------------------------------------
SUBROUTINE UPPERCASE(CH)
C
C Converts to upper case.
C ------------------------------------------------
C
CHARACTER*1 CH
C
I = ICHAR(CH)