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Finite-Time Output Feedback Attitude Tracking Control for Rigid Spacecraft

โœ Scribed by Zou, An-Min


Book ID
126092189
Publisher
IEEE
Year
2014
Tongue
English
Weight
523 KB
Volume
22
Category
Article
ISSN
1063-6536

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๐Ÿ“œ SIMILAR VOLUMES


Output feedback control for attitude tra
โœ Fabrizio Caccavale; Luigi Villani ๐Ÿ“‚ Article ๐Ÿ“… 1999 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 148 KB

In this paper the problem of attitude tracking control for a rigid spacecraft is addressed. It is assumed that only attitude measurements are available, and thus spacecraft's angular velocity has to be properly estimated. Two alternative schemes are proposed in which the unit quaternion is adopted t