poliastro.core.thrust.change_ecc_inc
¶
Simultaneous eccentricity and inclination changes.
References
Pollard, J. E. “Simplified Analysis of Low-Thrust Orbital Maneuvers”, 2000.
Module Contents¶
Functions¶
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Compute required increment of velocity. |
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Compute required increment of velocity. |
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- poliastro.core.thrust.change_ecc_inc.beta(ecc_0, ecc_f, inc_0, inc_f, argp)¶
- poliastro.core.thrust.change_ecc_inc.delta_V(V_0, ecc_0, ecc_f, beta_)¶
Compute required increment of velocity.
- poliastro.core.thrust.change_ecc_inc.delta_t(delta_v, f)¶
Compute required increment of velocity.
- poliastro.core.thrust.change_ecc_inc.change_ecc_inc(k, a, ecc_0, ecc_f, inc_0, inc_f, argp, r, v, f)¶