poliastro.threebody.flybys
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Module Contents¶
Functions¶
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Computes outbound velocity after a flyby. |
- poliastro.threebody.flybys.compute_flyby(v_spacecraft, v_body, k, r_p, theta=0 * u.deg)¶
Computes outbound velocity after a flyby.
- Parameters
v_spacecraft (Quantity) – Velocity of the spacecraft, relative to the attractor of the body.
v_body (Quantity) – Velocity of the body, relative to its attractor.
k (Quantity) – Standard gravitational parameter of the body.
r_p (Quantity) – Radius of periapsis, measured from the center of the body.
theta (Quantity, optional) – Aim angle of the B vector, default to 0.
- Returns
v_spacecraft_out (~astropy.units.Quantity) – Outbound velocity of the spacecraft.
delta (~astropy.units.Quantity) – Turn angle.