Attitude tracking control of flexible spacecraft with large amplitude slosh
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Computational Mechanics
Link
http://link.springer.com/article/10.1007/s10409-017-0700-9/fulltext.html
Reference21 articles.
1. Reyhanoglu, M.: Maneuvering control problems for a spacecraft with unactuated fuel slosh dynamics. IEEE Control Syst. 1, 695–699 (2003). doi: 10.1109/CCA.2003.1223522
2. Kang, J.Y., Lee, S.: Attitude acquisition of a satellite with a partially filled liquid tank. J. Guid. Control Dyn. 31, 790–793 (2008). doi: 10.2514/1.31865
3. Yue, B.Z.: Chaotic attitude and reorientation maneuver for completely liquid-filled spacecraft with flexible appendage. Acta Mech. Sin. 25, 271–277 (2009). doi: 10.1007/s10409-008-0213-7
4. Yue, B.Z.: Study on the chaotic dynamics in attitude maneuver of liquid-filled flexible spacecraft. AIAA J. 49, 2090–2099 (2012). doi: 10.2514/1.J050144
5. Yang, D.D., Yue, B.Z., Wu, W.J., et al.: Attitude maneuver of liquid-filled spacecraft with a flexible appendage by momentum wheel. Acta Mech. Sin. 28, 543–550 (2012). doi: 10.1007/s10409-012-0060-4
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