Trajectory and maneuvers

• CL_ex_getInfo — Information about a propagation model
• CL_ex_kepler — Keplerian orbit propagation
• CL_ex_mean2osc — Mean to osculating orbital elements (all analytical models)
• CL_ex_osc2mean — Osculating to mean orbital elements (all analytical models)
• CL_ex_propagate — Orbit propagation (all analytical models)
• CL_ex_propagateMan — Orbit propagation with maneuvers (all analytical models)
• CL_ex_secularJ2 — Orbit propagation using "secular J2" model
• CL_man_applyDvKep — Effect of maneuver on orbital elements
• CL_man_consumption — Mass consumed as function of delta-V
• CL_man_dvApsidesLine — Delta V required to change the line of apsides
• CL_man_dvBiElliptic — Bi-elliptic transfer
• CL_man_dvHohmann — Hohmann transfer
• CL_man_dvHohmannG — Generalized Hohmann transfer
• CL_man_dvInc — Inclination maneuver (elliptical orbits)
• CL_man_dvIncRaanCirc — Inclination and RAAN maneuver for circular orbits
• CL_man_dvIncSma — Inclination + semi-major axis maneuver (elliptical orbits)
• CL_man_dvSma — Change of semi-major axis (elliptical orbits)
• CL_man_dvSmaEccv — Change of semi major axis and excentricity vector (eccentric orbits)
• CL_man_dvSmaT — Change of semi-major axis by a tangential maneuver (elliptical orbits)
• CL_man_lambert — Lambert's problem
• CL_man_lambert2 — Lambert's problem
• CL_man_thrustDuration — Thrust duration as function of mass consumed
• CL_stela_convert — Mean/osculating conversion using STELA
• CL_stela_deriv — Orbital elements time derivatives using STELA
• CL_stela_extrap — Orbit propagation using STELA
• CL_stela_getConst — Physical constants used by STELA
• CL_stela_params — Model parameters for STELA
• CL_tle_evalAvgElem — Evaluates TLE mean orbital elements at epoch
• CL_tle_format — Two-line string generation from TLE structure
• CL_tle_genEphem — Ephemeris generation from TLEs (SGP4/SDP4 propagation)
• CL_tle_getBalCoef — Ballistic coefficient from bstar
• CL_tle_getConst — Physical constants used in TLE propagation
• CL_tle_getElem — TLE epoch and associated mean orbital elements (no propagation)
• CL_tle_load — Loads TLEs from files
• CL_tle_new — Creation of TLE structure
• CL_tle_parse — TLE structure from two-line string
• CL_tle_set — Change values in a TLE structure
• CL_tle_setElem — Sets TLE orbital state
• CL_tle_update — Update TLE orbital state