Optimal maneuvering strategy of spacecraft evasion based on angles-only measurement and observability analysis
Author:
Affiliation:
1. College of Liberal Arts and Sciences, National University of Defense Technology,Changsha,China,410073
Funder
National Key R&D Program of China
National Natural Science Foundation of China
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
General Earth and Planetary Sciences,General Environmental Science
Link
http://xplorestaging.ieee.org/ielx7/5971804/10066212/10018350.pdf?arnumber=10018350
Reference29 articles.
1. Numerical Solution of the Three-Dimensional Orbital Pursuit-Evasion Game
2. Analysis of optimal impulse for in-plane collision avoidance maneuver;su;Systems Engineering and Electronics,2018
3. An escape strategy in orbital pursuit-evasion games with incomplete information
4. Nonlinear Control for Spacecraft Pursuit-Evasion Game Using the State-Dependent Riccati Equation Method
5. Collision probability based optimal collision avoidance maneuver in rendezvous and docking;wang;Journal of Astronautics,2008
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