Rendezvous Problem for Nearly Circular Orbits
Author:
Affiliation:
1. Martin Company, Denver, Colo.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference7 articles.
1. Terminal Guidance System for Satellite Rendezvous
2. London, H. S. "Second approximation to the solution of rendezvous equations/' AIAA J. 1, 1691-1693 (1963).
3. ELLIPTIC ELEMENTS IN TERMS OF SMALL INCREMENTS OF POSITION AND VELOCITY COMPONENTS
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