Rigid-flexible coupling dynamic modeling and vibration control for flexible spacecraft based on its global analytical modes
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Engineering,General Materials Science
Link
http://link.springer.com/content/pdf/10.1007/s11431-017-9219-1.pdf
Reference25 articles.
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3. Bang H, Ha C K, Kim J H. Flexible spacecraft attitude maneuver by application of sliding mode control. Acta Astronaut, 2005, 57: 841–850
4. Hu Q, Ma G. Variable structure control and active vibration suppression of flexible spacecraft during attitude maneuver. Aerosp Sci Tech, 2005, 9: 307–317
5. Yang J B, Jiang L J, Chen D C. Dynamic modelling and control of a rotating Euler-Bernoulli beam. J Sound Vib, 2004, 274: 863–875
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