poliastro2.math.thrust.change_ecc_quasioptimal

Functions

delta_V(V_0, ecc_0, ecc_f)	Compute required increment of velocity.
extra_quantities(k, a, ecc_0, ecc_f, f)	Extra quantities given by the model.

poliastro2.math.thrust.change_ecc_quasioptimal.delta_V(V_0, ecc_0, ecc_f)

Compute required increment of velocity.

poliastro2.math.thrust.change_ecc_quasioptimal.extra_quantities(k, a, ecc_0, ecc_f, f)

Extra quantities given by the model.