| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1712950 | Journal of Systems Engineering and Electronics | 2008 | 8 Pages |
Abstract
This article is concerned with the modeling and control problems of the flexible spacecraft. First, the state observer is designed to estimate the vibration mode on the basis of free vibration models. Then, an optimal guaranteed cost controller is proposed to stabilize system attitude and damp the vibration of the flexible beam at the same time. Numerical simulation examples show the feasibility and validity of the proposed method.
Related Topics
Physical Sciences and Engineering
Engineering
Control and Systems Engineering
Authors
Wang Qingchao, Cai Peng,