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