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>> Trajectory and maneuvers
Trajectory and maneuvers
CL_dsp_covCoord
—
Conversion of type of orbital elements in a covariance matrix
CL_dsp_kepCovPropa
—
Keplerian covariance propagation
CL_ex_eckHech
—
Eckstein Hechler orbit propagation analytical model
CL_ex_kepler
—
Keplerian orbit propagation
CL_ex_lyddane
—
Lyddane orbit propagation analytical model
CL_ex_lyddaneMan
—
Lyddane orbit propagation analytical model with maneuvers
CL_ex_meanEckHech
—
Eckstein Hechler orbit propagation analytical model (mean elements)
CL_ex_meanLyddane
—
Lyddane orbit propagation analytical model (mean elements)
CL_ex_secularJ2
—
Secular J2 orbit propagation
CL_man_applyDv
—
Effect of maneuver on orbital elements
CL_man_apsidesLine
—
Delta V required to change the line of apsides
CL_man_biElliptic
—
Delta V for a bi-elliptic transfer
CL_man_consumption
—
Mass consumed as function of delta-V
CL_man_hohmann
—
Delta V for a Hohmann transfer
CL_man_hohmannG
—
Delta V for a generalized Hohmann transfer
CL_man_incRaanCirc
—
Inclination and RAAN maneuver for circular orbits
CL_man_inclination
—
Delta V required to change the inclination
CL_man_lambert
—
Lambert's problem
CL_man_sma
—
Delta V required to change the semi-major axis
CL_man_thrustDuration
—
Thrust duration as function of mass consumed
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