CL_fr_topoN2ter — Topocentric north to terrestrial frame vector transformation
[pos_ter[,vel_ter[,jacob]] = CL_fr_topoN2ter(orig[,pos_topoN[,vel_topoN[,er[,obl]]]])
Velocity and jacobian are optionally computed.
NOTE: position and velocity are not necessary to compute jacobian. In this case, zero vectors are given for pos_ter and vel_ter.
Warning : The origin of a topocentric North frame is not the center of the planet : it is the given point of longitude and latitude
x: a unit vector towards norh
y: a unit vector (local paralel tangent) towards west
z: a unit vector in direction of the local vertical
[LON;LAT;H] topocentric frame origin elliptical (geodetic) coordinates [rad],[m] (3x1 : same origin for all positions or 3xN : one origin for each position)
(optional) [X;Y;Z] position coordinates in topocentric North frame [m] (3xN)
(optional) [Vx;Vy;Vz] velocity coordinates in topocentric North frame [m/s] (3xN)
(optional) ellipsoid equatorial radius (default is %CL_eqRad) [m]
(optional) ellipsoid oblateness (default is %apla)
[X;Y;Z] position coordinates in earth reference frame [m] (3xN)
(optional) [Vx;Vy;Vz] velocity coordinates in earth reference frame [m/s] (3xN)
(optional) transformation jacobian d(x,y,z,vx,vy,vz)_ter/d(x,y,z,vx,vy,vz)_topoN (6x6x size(orig))