Part II. Coordinates and frames

Table of Contents

CL_co_car2ell — Cartesien to elliptical coordinates
CL_co_car2sph — Cartesien to spherical coordinates
CL_co_ell2car — Elliptical to cartesien coordinates
CL_co_sph2car — Spherical to cartesien coordinates
CL_dat_cal2cjd — Calendar date to CNES Julian Day
CL_dat_cal2jd — Calendar date to Julian Date
CL_dat_cjd2cal — CNES Julian date to calendar date
CL_dat_cjd2jd — CNES Julian date to Julian date
CL_dat_cjd2mjd — CNES Julian date to Modified Julian date
CL_dat_jd2cal — Julian Date to calendar date
CL_dat_jd2cjd — Julian date to CNES Julian date
CL_dat_mjd2cjd — Modified Julian Date to CNES Julian date
CL_dat_tai2utc — TAI to UTC conversion
CL_dat_utc2tai — UTC to TAI conversion
CL_fr_G502J2000 — Gamma50 (Veis) to EME2000 (J2000) frame vector transformation
CL_fr_G502J2000Mat — Gamma50 (Veis) to EME2000 (J2000) matrix
CL_fr_G502ter — Gamma50 (Veis) to terrestrial frame vector transformation
CL_fr_G502terMat — Gamma50 (Veis) to terrestrial matrix
CL_fr_H0n2J2000Mat — H0-n to EME2000 matrix
CL_fr_J20002G50 — EME2000 (J2000) to Gamma50 (Veis) frame vector transformation
CL_fr_J20002ter — EME2000 (J2000) to terrestrial frame vector transformation
CL_fr_inertial2qsw — Inertial to local orbital frame (q,s,w) vector transformation
CL_fr_inertial2tnw — Inertial to local orbital frame (t,n,w) vector transformation
CL_fr_lvlhMat — Local orbital frame (LVLH) definition in an inertial frame
CL_fr_qsw2inertial — Local orbital (q,s,w) to inertial frame vector transformation
CL_fr_qswMat — Local orbital frame (q,s,w) definition in an inertial frame
CL_fr_teme2J2000Mat — TEME to J2000 matrix
CL_fr_ter2G50 — Gamma50 (Veis) to G50restrial frame vector transformation
CL_fr_ter2J2000 — Terrestrial to EME2000 (J2000) frame vector transformation
CL_fr_ter2J2000Mat — Terrestrial to EME2000 (J2000) matrix
CL_fr_ter2topoN — Terrestrial to topocentric north frame vector transformation
CL_fr_tnw2inertial — Local orbital (t,n,w) to inertial frame vector transformation
CL_fr_tnwMat — Local orbital frame (t,n,w) definition in an inertial frame
CL_fr_topoN2ter — Topocentric north to terrestrial frame vector transformation
CL_fr_topoNMat — Local topocentric north frame
CL_oe_car2cir — Cartesien to circular adapted orbital elements
CL_oe_car2cirEqua — Cartesien to circular equatorial adapted orbital elements
CL_oe_car2kep — Cartesien to keplerian orbital elements
CL_oe_cir2car — Circular adapted to cartesien orbital elements
CL_oe_cirEqua2car — Circular equatorial adapted to cartesien orbital elements
CL_oe_cirEqua2kep — Circular equatorial adapted to keplerian orbital elements
CL_oe_kep2car — Keplerian to cartesian orbital elements
CL_oe_kep2cirEqua — Keplerian to circular equatorial adapted orbital elements
CL_rot_angles2matrix — Rotation angles matrix
CL_rot_angularVelocity — Rotation angles to velocity and acceleration vectors
CL_rot_axAng2quat — Rotation axis and angle to quaternion
CL_rot_defQuat — Quaternion definition from its real or imaginary components
CL_rot_eul2quat — Euler '123' angles to quaternion
CL_rot_matrix2quat — Matrix to quaternion
CL_rot_quat2eul — Quaternion to Euler '123' angles
CL_rot_quat2matrix — Quaternion to matrix
CL_rot_quatSlerp — Spherical linear interpolation between 2 quaternions
CL_rot_rotVect — Rotation(defined by a quaternion) of a vector