poliastro.core.thrust

Submodules

Summary

Functions

change_a_inc(k, a_0, a_f, inc_0, inc_f, f)

Change semimajor axis and inclination.

change_argp(k, a, ecc, argp_0, argp_f, f)

Guidance law from the model.

change_ecc_inc

Simultaneous eccentricity and inclination changes.

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