A Decentralized Attitude Control for Spacecraft Formation Flying Via the State-Dependent Riccati Equation Technique (AAS 07-403)
Astrodynamics 2007: proceedings of the AAS/AIAA Astrodynamics Specialist Conference ; 2007 ; Mackinac Island, MI
2008-01-01
20 pages
Includes bibliographical references and index. Proceedings of the AAS/AIAA Astrodynamics Conference.Part 3 of 3
Conference paper
English
Astrodynamics , AAS , AIAA
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Optimized State-Dependent Riccati Equation Method for Spacecraft Attitude Estimation and Control
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