Relative Motion Control for Autonomous Rendezvous Based on Classical Orbital Element Differences
Author:
Affiliation:
1. Beihang University, Beijing 100083, People’s Republic of China
2. University of Nottingham, Nottingham, NG7 2RD England, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.28250
Reference37 articles.
1. Guidance and Relative Navigation for Autonomous Rendezvous in a Circular Orbit
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