IEEE - Institute of Electrical and Electronics Engineers, Inc. - Linear feedback spacecraft stabilization using the method of invariant ellipsoids

2009 41st Southeastern Symposium on System Theory (SSST)

Author(s): Gonzalez-Garcia, S. ; Polyakov, A. ; Poznyak, A.
Publisher: IEEE - Institute of Electrical and Electronics Engineers, Inc.
Publication Date: 1 March 2009
Conference Location: Tullahoma, USA
Conference Date: 15 March 2009
Page(s): 195 - 198
ISBN (CD): 978-1-4244-3325-4
ISBN (Paper): 978-1-4244-3324-7
ISSN (Paper): 0094-2898
DOI: 10.1109/SSST.2009.4806834
Regular:

This paper addresses the robust attitude control for an uncertain flexible spacecraft with disturbances bounded by ellipsoids. An observed-state feedback is designed using the so-called invariant... View More

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