Optimal Variable-Structure Control Tracking of Spacecraft Maneuvers
- 1 May 2000
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 23 (3), 564-566
- https://doi.org/10.2514/2.4568
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
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- Variable-structure control of spacecraft attitude maneuversJournal of Guidance, Control, and Dynamics, 1988
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- Quaternion feedback for spacecraft large angle maneuversJournal of Guidance, Control, and Dynamics, 1985