Using the State-Dependent Riccati Equation and Kalman Filter Techniques to Design a Satellite Attitude Control Simulator (IAA-AAS-DyCoSS1-07-09 - AAS 12-351)
Conference, Dynamics and Control of Space Systems; proceedings of the 1st International Academy of Astronautics Conference ; 2012 ; Porto, Portugal
2012-01-01
14 pages
Includes bibliographical references and indexes; ALSO HELD ON CD-ROM
Conference paper
English
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