AIAA-2002-4844 Optimal Two-Impulse Rendezvous Between Two Circular Orbits Using Multiple-Revolution Lambert's Solutions
Conference, Guidance, navigation and control ; 2002 ; Monterey, CA
2002-01-01
11 pages
Conference paper
English
guidance , navigation , control , AIAA
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Optimal Two-Impulse Cotangent Rendezvous Between Coplanar Elliptical Orbits
Online Contents | 2013
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