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Variable Structure Control for Large Angle Maneuvering of Flexible Spacecraft
Author(s): 
Pages: 48-52
Year: Issue:  3
Journal: AEROSPACE CONTROL

Keyword:  挠性航天器变结构控制弹性稳态器振动抑制;
Abstract: 考虑刚性主体上带有挠性梁的航天器,在建立挠性系统动力学模型的基础上,采用等速趋近率的滑模变结构控制策略进行大角度机动控制,并通过最优控制理论设计弹性稳态器,抑制由于刚体运动而激发的弹性振动,实现了旋转机动的同时,有效抑制弹性振动.
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