| 引用本文: | 吴爱国,董瑞琦,张颖.转动惯量存在不确定性的挠性航天器滑模姿态控制[J].控制理论与应用,2018,35(10):1422~1429.[点击复制] |
| WU Ai-guo,DONG Rui-qi,ZHANG Ying.Sliding mode attitude control for flexible spacecraft with inertia uncertainty[J].Control Theory and Technology,2018,35(10):1422~1429.[点击复制] |
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| 转动惯量存在不确定性的挠性航天器滑模姿态控制 |
| Sliding mode attitude control for flexible spacecraft with inertia uncertainty |
| 摘要点击 3228 全文点击 1516 投稿时间：2017-11-23 修订日期：2018-09-13 |
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| DOI编号 10.7641/CTA.2018.70861 |
| 2018,35(10):1422-1429 |
| 中文关键词 挠性航天器 转动惯量不确定性 姿态镇定 滑模控制 |
| 英文关键词 flexible spacecraft parameter uncertainty attitude stabilization sliding mode control |
| 基金项目 国家自然科学基金重大项目(61690210, 61690212), 深圳市学科布局项目(JCYJ20170413112722597), 国家自然科学基金项目(61603111), 深圳市基础 研究项目(JCYJ20170307150227897), 广东省自 然科学基金项目(2017A030313340) , 国家自然科学基金优秀青年科学基金项目(61822305). |
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| 中文摘要 |
| 在转动惯量存在不确定性时, 采用滑动模态控制方法对挠性航天器设计了姿态镇定控制律. 由于挠性模态是不可量测的, 首先设计了一个部分状态观测器对挠性模态进行估计. 进而结合滑模控制方法, 提出了基于观测器的滑模姿态控制律. 采用Lyapunov 方法证明了在存在转动惯量不确定性时, 所设计的滑模姿态控制律能使闭环航天器姿态系统稳定. 最后, 通过数值仿真例子验证了所提出方法的有效性. |
| 英文摘要 |
| In this paper, the sliding mode control technique is adopted to design attitude stabilization controllers for flexible spacecraft with inertia uncertainty. First, a partial state observer is designed to estimate the flexible modal variables since the flexible variables are unmeasurable. By using the sliding mode control technique, a
sliding mode control law based on observers is proposed for flexible spacecraft with inertia uncertainty.
The Lyapunov technique is utilized to show that the proposed sliding mode control law can stabilize the attitude system of the flexible spacecraft with the inertia uncertainty. Finally, a numerical example is employed to verify the effectiveness of
the presented control law. |
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