DEPRECATED

• CL_3b_manifolds — Manifolds (divergent and convergent) from Halo and Lissajous - DEPRECATED
• CL_colMult — Multiplication of column vectors by coefficients - DEPRECATED
• CL_colNorm — Norm of column vectors - DEPRECATED
• CL_cw_ballisticPropa — Ballistic propagation of a chaser relatively to a target - DEPRECATED
• CL_cw_contPropa — Continuous thrust trajectory - DEPRECATED
• CL_cw_diffDrag — Differential acceleration drag - DEPRECATED
• CL_cw_impulPropa — Propagation of a chaser relatively to a target, with impulsives maneuvers - DEPRECATED
• CL_cw_twoImpulse — Two-impulse transfer - DEPRECATED
• CL_dat_cal2jd — Calendar date to Julian day - DEPRECATED
• CL_dat_cjd2jd — Modified (1950.0) Julian day to Julian day - DEPRECATED
• CL_dat_cjd2mjd — Modified (1950.0) Julian day to modified Julian day - DEPRECATED
• CL_dat_jd2cal — Julian day to calendar date - DEPRECATED
• CL_dat_jd2cjd — Julian day to modified (1950.0) Julian day - DEPRECATED
• CL_dat_mjd2cjd — Modified Julian day to modified (1950.0) Julian day - DEPRECATED
• CL_dat_tai2utc — TAI to UTC conversion - DEPRECATED
• CL_dat_tcb2tdb — TCB to TDB conversion - DEPRECATED
• CL_dat_tdb2tcb — TDB to TCB conversion - DEPRECATED
• CL_dat_utc2tai — UTC to TAI conversion - DEPRECATED
• CL_dsp_covCoord — Conversion of type of orbital elements in a covariance matrix - DEPRECATED
• CL_dsp_kepCovPropa — Covariance propagation - DEPRECATED
• CL_ev_visibility — Geometrical visibility start and end times - DEPRECATED
• CL_ev_visibilityEph — Geometrical visibility calculation - DEPRECATED
• CL_ev_visibilityExtr — Geometrical visibility calculation - DEPRECATED
• CL_ex_eckHech — Eckstein-Hechler propagation model - DEPRECATED
• CL_ex_eckHechInfos — Informations about Eckstein-Hechler orbit propagation analytical model - DEPRECATED
• CL_ex_lyddane — Orbit propagation using Lyddane model (mean elements = secular) - DEPRECATED
• CL_ex_lyddaneInfos — Informations about Lyddane orbit propagation analytical model - DEPRECATED
• CL_ex_lyddaneLp — Orbit propagation using Lyddane model (mean elements = secular + long periods) - DEPRECATED
• CL_ex_lyddaneMan — Lyddane orbit propagation analytical model with maneuvers - DEPRECATED
• CL_ex_meanEckHech — Eckstein-Hechler propagation model - mean elements - DEPRECATED
• CL_ex_meanElem — Mean orbital elements (all analytical models) - DEPRECATED
• CL_ex_meanLyddane — Lyddane propagation model - mean elements (mean = secular) - DEPRECATED
• CL_ex_meanLyddaneLp — Lyddane propagation model - mean elements (mean = secular + LP) - DEPRECATED
• CL_fr_G502J2000 — Gamma50 (Veis) to EME2000 (J2000) vector transformation - DEPRECATED
• CL_fr_G502J2000Mat — Gamma50 (Veis) to EME2000 (J2000) transformation matrix - DEPRECATED
• CL_fr_G502ter — Gamma50 (Veis) to terrestrial frame vector transformation - DEPRECATED
• CL_fr_G502terMat — Gamma50 (Veis) to terrestrial frame transformation matrix - DEPRECATED
• CL_fr_H0n2J2000Mat — H0-n to EME2000 (J2000) transformation matrix - DEPRECATED
• CL_fr_J20002G50 — EME2000 (J2000) to Gamma50 (Veis) vector transformation - DEPRECATED
• CL_fr_J20002ter — EME2000 (J2000) to terrestrial frame vector transformation - DEPRECATED
• CL_fr_ter2G50 — Terrestrial frame to Gamma50 (Veis) vector transformation - DEPRECATED
• CL_fr_ter2J2000 — Terrestrial frame to EME2000 (J2000) vector transformation - DEPRECATED
• CL_fr_ter2J2000Mat — Terrestrial frame to EME2000 (J2000) transformation matrix - DEPRECATED
• CL_fr_ter2topoN — Terrestrial frame to topocentric North frame vector transformation - DEPRECATED
• CL_fr_topoN2ter — Topocentric North frame to terrestrial frame vector transformation - DEPRECATED
• CL_gm_equatorialOverlap — Ratio between sensor footprint and gap between ground tracks - DEPRECATED
• CL_gm_equatorialSwath — Sensor view angle for an overlap ratio of 1 at equator - DEPRECATED
• CL_gm_lat2locTime — Satellite's local time at given latitude - DEPRECATED
• CL_gm_locSolTime — Local solar time - DEPRECATED
• CL_gm_sphericDist — Angle (angular distance) between 2 directions - DEPRECATED
• CL_gm_stationElevation — Elevation of any object as seen from ground stations - DEPRECATED
• CL_kp_M2Ecir — Kepler's equation for circular or equinoctial orbital elements - DEPRECATED
• CL_man_applyDv — Effect of maneuver on orbital elements - DEPRECATED
• CL_man_apsidesLine — Delta V required to change the line of apsides - DEPRECATED
• CL_man_biElliptic — Bi-elliptic transfer - DEPRECATED
• CL_man_hohmann — Hohmann transfer - DEPRECATED
• CL_man_hohmannG — Generalized Hohmann transfer - DEPRECATED
• CL_man_incRaanCirc — Inclination and RAAN maneuver for circular orbits - DEPRECATED
• CL_man_inclination — Inclination maneuver (elliptical orbits) - DEPRECATED
• CL_man_sma — Change of semi-major axis (elliptical orbits) - DEPRECATED
• CL_matSort — Matrix sorting by row or column - DEPRECATED
• CL_mod_equinoxesEquation — Equation of the equinoxes (IERS 1996) - DEPRECATED
• CL_mod_expDensity — Exponential density model - DEPRECATED
• CL_mod_expDensityDrag — Atmospheric drag using exponential density model - DEPRECATED
• CL_mod_meanObliquity — Mean obliquity (IERS 1996) - DEPRECATED
• CL_mod_moonSunG50 — Moon and Sun positions in Gamma50 (Veis) reference frame - DEPRECATED
• CL_mod_nutationAngles — Nutation angles (Wahr IAU 1980) - DEPRECATED
• CL_mod_nutationArg — Fundamental arguments for nutation - DEPRECATED
• CL_mod_nutationMatrix — Nutation matrix and rotation vectors (IERS 1996) - DEPRECATED
• CL_mod_planetsG50ecl — Planet positions in Gamma50 ecliptic reference frame - DEPRECATED
• CL_mod_polarMotionMatrix — Polar motion matrix - DEPRECATED
• CL_mod_precessionAngles — Precession angles (Lieske 1976) - DEPRECATED
• CL_mod_precessionMatrix — Precession matrix and rotation vectors (IERS 1996) - DEPRECATED
• CL_mod_sidTime — Greenwich mean sidereal time (IERS 1996) - DEPRECATED
• CL_mod_sidTimeG50 — sidereal time in Gamma50 (Veis) frame - DEPRECATED
• CL_oe_car2cirEqua — Cartesian to circular equatorial adapted orbital elements - DEPRECATED
• CL_oe_cirEqua2car — Circular equatorial adapted to cartesian orbital elements - DEPRECATED
• CL_oe_cirEqua2kep — Circular equatorial adapted to keplerian orbital elements - DEPRECATED
• CL_oe_kep2cirEqua — Keplerian to circular equatorial adapted orbital elements - DEPRECATED
• CL_op_locTimeG50 — Conversion between longitude, right ascension and local time - DEPRECATED
• CL_rot_angularVelocity — Rotation angles to angular velocity and acceleration vectors - DEPRECATED
• CL_rot_eul2quat — Euler '123' angles to quaternion - DEPRECATED
• CL_rot_quat2eul — Quaternion to Euler '123' angles - DEPRECATED