Optimization Of Spacecraft Pursuit-Evasion Game Trajectories In The Euler-Hill Reference Frame-Reference-Cited by-同舟云学术

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Optimization Of Spacecraft Pursuit-Evasion Game Trajectories In The Euler-Hill Reference Frame

Published:2014-08-01 Issue: Volume: Page:
ISSN:
Container-title:AIAA/AAS Astrodynamics Specialist Conference
language:
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Author:

Jagat Ashish¹,Sinclair Andrew J.¹

Affiliation:

1. Auburn University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-4131

Reference19 articles.

1. 1Isaacs,R.,DifferentialGames,JohnWiley&Sons,NewYork,1965.

2. 2Basar,T.andOlsder,G.J.,DynamicNoncooperativeGameTheory,AcademicPress,London,1982.

3. 3EngwerdaJ.,LQDynamicOptimizationandDifferentialGames,JohnWiley&Sons,England,2005.

4. Systematic and effective design of nonlinear feedback controllers via the state-dependent Riccati equation (SDRE) method

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