Part VIII. Trajectory and maneuvers

Table of Contents

CL_dsp_covCoord — Change coordinates of covariance matrix
CL_dsp_kepCovPropa — Covariance propagation (Keplerian)
CL_ex_eckHech — Eckstein Hechler orbit extrapolation analytic model
CL_ex_kepler — Keplerian orbit extrapolation
CL_ex_lyddane — Lydanne orbit extrapolation analytic model
CL_ex_lyddaneMan — Lydanne orbit extrapolation analytic model with maneuvers
CL_ex_meanEckHech — Mean parameters of the Eckstein Hechler orbit extrapolation analytic model
CL_ex_meanLyddane — Mean parameters of the Lydanne orbit extrapolation model
CL_ex_secularJ2 — Secular J2 effects orbit propagation
CL_man_applyDv — Modification of osculating orbital elements after a maneuver defined in QSW frame.
CL_man_apsidesLine — Delta V for a maneuver to modify line of apsides
CL_man_biElliptic — Total delta V for a bi-elliptic Hohmann transfer
CL_man_consumption — Mass consumed, delta V, isp or initial mass
CL_man_hohmann — Delta V for a hohmann transfer
CL_man_hohmannG — Delta V for a generalized Hohmann transfer maneuver
CL_man_incRaanCirc — Inclination and RAAN maneuver for circular orbits
CL_man_inclination — Delta V for an inclination maneuver
CL_man_lambert — Lambert's problem
CL_man_sma — Delta V for an orbit shape modification (semi major axis)
CL_man_thrustDuration — Thrust duration, mass consumed, thrust value or propellant specific impulse