poliastro2.core.actions.thrust.change_ecc_quasioptimal

poliastro2.core.actions.thrust.change_ecc_quasioptimal(orb_0, ecc_f, f)

Guidance law from the model. Thrust is aligned with an inertially fixed direction perpendicular to the semimajor axis of the orbit.

Parameters:

• orb_0 (Orbit) – Initial orbit, containing all the information.

• ecc_f (float) – Final eccentricity.

• f (float) – Magnitude of constant acceleration