Optimized State-Dependent Riccati Equation Method for Spacecraft Attitude Estimation and Control
AIAA guidance, navigation, and control conference ; 2012 ; Minneapolis, MN
01.01.2012
21 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
Guidance , Navigation , Control , AIAA
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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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