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考虑系统不确定性的高超声速飞行器容错控制

彭程 王新民 谢蓉 穆凌霞

彭程, 王新民, 谢蓉, 等 . 考虑系统不确定性的高超声速飞行器容错控制[J]. 北京航空航天大学学报, 2016, 42(7): 1414-1421. doi: 10.13700/j.bh.1001-5965.2015.0462
引用本文: 彭程, 王新民, 谢蓉, 等 . 考虑系统不确定性的高超声速飞行器容错控制[J]. 北京航空航天大学学报, 2016, 42(7): 1414-1421. doi: 10.13700/j.bh.1001-5965.2015.0462
PENG Cheng, WANG Xinmin, XIE Rong, et al. Fault-tolerant control for hypersonic vehicle with system uncertainty[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(7): 1414-1421. doi: 10.13700/j.bh.1001-5965.2015.0462(in Chinese)
Citation: PENG Cheng, WANG Xinmin, XIE Rong, et al. Fault-tolerant control for hypersonic vehicle with system uncertainty[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(7): 1414-1421. doi: 10.13700/j.bh.1001-5965.2015.0462(in Chinese)

考虑系统不确定性的高超声速飞行器容错控制

doi: 10.13700/j.bh.1001-5965.2015.0462
基金项目: 陕西省自然科学基金(2014JQ8342)
详细信息
    作者简介:

    彭程 男,博士研究生。主要研究方向:容错飞行控制。Tel.: 029-88431356 E-mail: wanli1818@163.com;王新民 男,硕士,教授,博士生导师。主要研究方向:飞行控制。Tel.: 029-88431356 E-mail: wxmin@nwpu.edu.cn;谢蓉 女,博士,副教授。主要研究方向:飞行控制与控制理论。E-mail: xierong@nwpu.edu.cn;穆凌霞 女,博士研究生。主要研究方向:高超声速控制。E-mail: mulx@nwpu.edu.cn

    通讯作者:

    王新民,Tel.: 029-88431356 E-mail: wxmin@nwpu.edu.cn

  • 中图分类号: TP13

Fault-tolerant control for hypersonic vehicle with system uncertainty

  • 摘要: 针对一类含有执行器失效故障和范数有界不确定性的系统,提出了一种鲁棒容错跟踪控制设计方法。该方法利用有界实引理,给出了保证闭环系统稳定且满足鲁棒性能要求的线性矩阵不等式(LMI)的表达式;为了削弱控制器的保守性,使用不同的Lyapunov变量对应不同的系统状态;由此带来的非凸优化问题,发展了一种迭代线性矩阵不等式算法。考虑到该迭代算法的收敛性取决于初值的选择,经过推导给出了一种求解合适初值的算法。将该算法应用于高超声速飞行器X-33跟踪控制器的设计,仿真结果表明本文算法是可行和有效的。

     

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出版历程
  • 收稿日期:  2015-07-09
  • 网络出版日期:  2016-07-20

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