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Optimal Slewing of a Flexible Spacecraft

✍ Scribed by A. E. Zakrzhevskii


Book ID
111586606
Publisher
Springer US
Year
2003
Tongue
English
Weight
115 KB
Volume
39
Category
Article
ISSN
1573-8582

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A new computational approach to modelling and control of a flexible beam is proposed. The structural modelling and the control design problems are formulated in a unified mathematical framework that allows simultaneous structural and control design iterations that result in an optimal overall system