ssapy_toolkit.Orbital_Mechanics.transfer_coplanar_continuous

ssapy_toolkit.Orbital_Mechanics.transfer_coplanar_continuous(r1, v1, r2, v2=None, a_thrust=1, mu=398600441800000.0, t0=None, max_time=7200.0, tol=1.0, plot=False)[source]

Continuous‐thrust, coplanar transfer: thrust always lies in the initial orbital plane (normal = r1×v1), steering to rendezvous r2 (and optionally v2).

All units SI: r (m), v (m/s), a_thrust (m/s²), t (s), mu (m³/s²).