poliastro.core.thrust.change_a_inc

Module Contents

Functions

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

Extra quantities given by the Edelbaum (a, i) model.

beta(t, *, V_0, f, beta_0)

Compute yaw angle (β) as a function of time and the problem parameters.

beta_0(V_0, V_f, inc_0, inc_f)

Compute initial yaw angle (β) as a function of the problem parameters.

compute_parameters(k, a_0, a_f, inc_0, inc_f)

Compute parameters of the model.

delta_V(V_0, beta_0, inc_0, inc_f)

Compute required increment of velocity.

poliastro.core.thrust.change_a_inc.extra_quantities(k, a_0, a_f, inc_0, inc_f, f)

Extra quantities given by the Edelbaum (a, i) model.

poliastro.core.thrust.change_a_inc.beta(t, *, V_0, f, beta_0)

Compute yaw angle (β) as a function of time and the problem parameters.

poliastro.core.thrust.change_a_inc.beta_0(V_0, V_f, inc_0, inc_f)

Compute initial yaw angle (β) as a function of the problem parameters.

poliastro.core.thrust.change_a_inc.compute_parameters(k, a_0, a_f, inc_0, inc_f)

Compute parameters of the model.

poliastro.core.thrust.change_a_inc.delta_V(V_0, beta_0, inc_0, inc_f)

Compute required increment of velocity.