| 引用本文: | 马广富,于彦波,李波,胡庆雷.基于积分滑模的航天器有限时间姿态容错控制[J].控制理论与应用,2017,34(8):1028~1034.[点击复制] |
| Ma Guang-fu,Yu Yan-bo,Li Bo,Hu Qing-lei.Integral-type sliding mode finite-time fault tolerant control for[J].Control Theory and Technology,2017,34(8):1028~1034.[点击复制] |
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| 基于积分滑模的航天器有限时间姿态容错控制 |
| Integral-type sliding mode finite-time fault tolerant control for |
| 摘要点击 3203 全文点击 1852 投稿时间：2016-10-26 修订日期：2017-04-24 |
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| DOI编号 10.7641/CTA.2017.60805 |
| 2017,34(8):1028-1034 |
| 中文关键词 积分滑模 航天器 有限时间 姿态控制 容错控制 |
| 英文关键词 integral-type sliding mode spacecraft finite-time attitude control fault tolerant control |
| 基金项目 国家自然科学基金项目(61522301, 61633003, 61540045), 上海市科学技术委员会项目(17595810300, 14170501500, 14DZ2280200)资助. |
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| 中文摘要 |
| 针对存在执行机构故障和外部干扰的刚体航天器姿态稳定系统, 本文提出了基于积分滑模的容错控制策
略, 实现了姿态有限时间稳定. 首先, 利用齐次系统相关理论, 设计了一类饱和有界的基础控制律, 保证了不存在执
行机构故障和干扰情况下的姿态有限时间稳定. 在此基础上, 利用积分滑模和自适应技术设计了一种有限时间姿
态鲁棒容错控制方案, 对执行机构故障和干扰进行有效的补偿; 该方案能够快速地实现姿态高精度稳定, 并抑制系
统抖振现象. 最后, 将本文提出的姿态容错控制方案进行数值仿真与对比, 验证了方案的有效性与优越性. |
| 英文摘要 |
| This paper addresses the problem of integral-type sliding mode robust fault tolerant control for spacecraft , in
the presence of actuator failures and external disturbances simultaneously, achieving the finite-time attitude stabilization.
As a stepping stone, a simple saturated nominal controller is firstly designed using homogeneous system theory, to ensure
finite-time attitude stabilization of spacecraft without failures and disturbances. Then, utilizing integral-type sliding mode
and adaptive techniques, a novel finite-time robust fault tolerant control strategy is developed to compensate for actuators
failures and external disturbances. And also, the chattering problem has been restrained via a gain adjusting law. Finally,
numerical simulation results are presented to illustrate and highlight the fine performance benefits obtained using the
proposed scheme, especially for the faster and higher-precise attitude stabilization. |
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