poliastro.core.thrust.change_argp
¶
Module Contents¶
Functions¶
|
Compute required increment of velocity. |
|
Extra quantities given by the model. |
|
Guidance law from the model. |
- poliastro.core.thrust.change_argp.delta_V(V, ecc, argp_0, argp_f, f, A)¶
Compute required increment of velocity.
- poliastro.core.thrust.change_argp.extra_quantities(k, a, ecc, argp_0, argp_f, f, A=0.0)¶
Extra quantities given by the model.
- poliastro.core.thrust.change_argp.change_argp(k, a, ecc, argp_0, argp_f, f)¶
Guidance law from the model. Thrust is aligned with an inertially fixed direction perpendicular to the semimajor axis of the orbit.
- Parameters
- Returns
a_d (function)
delta_V (numpy.ndarray)
t_f (float)