Relative motion of two particles in elliptic orbits
Author:
Affiliation:
1. NASA Goddard Space Flight Center, Greenbelt, Md.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6007
Reference8 articles.
1. Terminal Guidance System for Satellite Rendezvous
2. SECOND APPROXIMATION TO THE SOLUTION OF THE RENDEZVOUS EQUATIONS
3. ELLIPTIC ELEMENTS IN TERMS OF SMALL INCREMENTS OF POSITION AND VELOCITY COMPONENTS
4. Rendezvous Problem for Nearly Circular Orbits
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