Gary A. McCue
Abstract
Spacecraft rendezvous trajectory between two elliptical orbits is determined by optimization of the two impulse orbital transfer
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Spacecraft rendezvous trajectory between two elliptical orbits is determined by optimization of the two impulse orbital transfer
Key concepts: Orbital maneuver, Elliptic orbit, Rendezvous, Impulse (physics), Spacecraft, Trajectory optimization, Physics, Orbital mechanics