Optimized State-Dependent Riccati Equation Method for Spacecraft Attitude Estimation and Control
AIAA guidance, navigation, and control conference ; 2012 ; Minneapolis, MN
2012-01-01
21 pages
Includes bibliographical references and index
Conference paper
English
Guidance , Control , AIAA , Navigation
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Optimized State-Dependent Riccati Equation Method for Spacecraft Attitude Estimation and Control
British Library Conference Proceedings | 2012
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