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Rendezvous Between Two Spacecrafts With Coplanar Elliptic Orbits Using The Horizontal Impulse
Author(s): 
Pages: 1-12
Year: Issue:  3
Journal: Aerospace Control

Keyword:  RendezvousSpacecraftElliptis orbitImpulse;
Abstract: In this paper, We investigate the problem of rendezvous between two spacecraftswith Coplanar elliptic orbits using three horizontal impulses. The necessary conditions for ren-dezvous are derived, and the procedures for solving the magnitudes and times of three horizon-tal impulses are given.
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