`poliastro.twobody.thrust`¶

Submodules¶

`change_a_inc`
`change_argp`(k, a, ecc, argp_0, argp_f, f)	Guidance law from the model.
`change_ecc_inc`(ss_0, ecc_f, inc_f, f)	Simultaneous eccentricity and inclination changes. Guidance law from the model. Thrust is aligned with an inertially fixed direction perpendicular to the semimajor axis of the orbit.
`change_ecc_quasioptimal`(ss_0, ecc_f, f)	Guidance law from the model.