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- W2358001815 abstract "Based on Hamilton's principle and Mindlin's theory of elastic thick plates,the hub-plate dynamic model of flexible spacecraft with flexible attachments is established,and the problems of a central rigid body approach to a rotating cantilever thick plate and its variable structure control are researched. By applying Hamiltonian formulism and elastic wave propagation theory,the vibration modes of the rotating Mindlin plate are presented. Based on the theory of sliding mode variable structure control( SMVSC),the controller of the system is designed to make the system reach asymptotic stability. The desired motion of the system can be obtained by using the theory of SMVSC,and the additional vibration of the flexible plate can be suppressed effectively. At last,the results are analyzed and discussed by numerical simulations. The method and calculation results in this paper are expected to be applied to the dynamics control of spacecraft with flexible attachments." @default.
- W2358001815 created "2016-06-24" @default.
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- W2358001815 date "2015-01-01" @default.
- W2358001815 modified "2023-09-23" @default.
- W2358001815 title "Vibration of a Rotating Spacecraft with Flexible Attachments and Its Variable Structure Control" @default.
- W2358001815 hasPublicationYear "2015" @default.
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