ISCE_INSAR/components/stdproc/orbit/orbitLib/src/latlon.F

85 lines
2.4 KiB
Fortran

!c****************************************************************
subroutine latlon(elp,r_v,r_llh,i_type)
!c****************************************************************
!c**
!c** FILE NAME: latlon.f
!c**
!c** DATE WRITTEN:7/22/93
!c**
!c** PROGRAMMER:Scott Hensley
!c**
!c** FUNCTIONAL DESCRIPTION:This program converts a vector to
!c** lat,lon and height above the reference ellipsoid or given a
!c** lat,lon and height produces a geocentric vector.
!c**
!c** ROUTINES CALLED:none
!c**
!c** NOTES: none
!c**
!c** UPDATE LOG:
!c**
!c****************************************************************
implicit none
!c INPUT VARIABLES:
integer i_type !1=lat,lon to vector,2= vector to lat,lon
type :: ellipsoid
real*8 r_a
real*8 r_e2
end type ellipsoid
type(ellipsoid) :: elp
real*8 r_v(3) !geocentric vector (meters)
real*8 r_llh(3) !latitude (deg -90 to 90),longitude (deg -180 to 180),height
!c OUTPUT VARIABLES: see input
!c LOCAL VARIABLES:
integer i_ft
real*8 pi,r_dtor,r_re,r_q2,r_q3,r_b,r_q
real*8 r_p,r_tant,r_theta,r_a,r_e2
!c DATA STATEMENTS:
data pi /3.141592653589793238d0/
data r_dtor /1.74532925199d-2/
!C FUNCTION STATEMENTS:
!c PROCESSING STEPS:
r_a = elp%r_a
r_e2 = elp%r_e2
if(i_type .eq. 1)then !convert lat,lon to vector
r_re = r_a/sqrt(1.d0 - r_e2*sin(r_llh(1))**2)
r_v(1) = (r_re + r_llh(3))*cos(r_llh(1))*cos(r_llh(2))
r_v(2) = (r_re + r_llh(3))*cos(r_llh(1))*sin(r_llh(2))
r_v(3) = (r_re*(1.d0-r_e2) + r_llh(3))*sin(r_llh(1))
elseif(i_type .eq. 2)then !convert vector to lat,lon
r_q2 = 1.d0/(1.d0 - r_e2)
r_q = sqrt(r_q2)
r_q3 = r_q2 - 1.d0
r_b = r_a*sqrt(1.d0 - r_e2)
r_llh(2) = atan2(r_v(2),r_v(1))
r_p = sqrt(r_v(1)**2 + r_v(2)**2)
r_tant = (r_v(3)/r_p)*r_q
r_theta = atan(r_tant)
r_tant = (r_v(3) + r_q3*r_b*sin(r_theta)**3)/(r_p - r_e2*r_a*cos(r_theta)**3)
r_llh(1) = atan(r_tant)
r_re = r_a/sqrt(1.d0 - r_e2*sin(r_llh(1))**2)
r_llh(3) = r_p/cos(r_llh(1)) - r_re
endif
end