poliastro.core.thrust.change_inc_ecc

Module Contents

Functions

beta(ecc_0, ecc_f, inc_0, inc_f, argp)

delta_V(V_0, ecc_0, ecc_f, beta_)

Compute required increment of velocity.

extra_quantities(k, a, ecc_0, ecc_f, inc_0, inc_f, argp, f)

Extra quantities given by the model.

poliastro.core.thrust.change_inc_ecc.beta(ecc_0, ecc_f, inc_0, inc_f, argp)
poliastro.core.thrust.change_inc_ecc.delta_V(V_0, ecc_0, ecc_f, beta_)

Compute required increment of velocity.

poliastro.core.thrust.change_inc_ecc.extra_quantities(k, a, ecc_0, ecc_f, inc_0, inc_f, argp, f)

Extra quantities given by the model.