留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

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。

     

  • [1] JI Y,ZHOU H L,ZONG Q.Adaptive active fault-tolerant control of generic hypersonic flight vehicles[J].Journal of Systems and Control Engineering,2015,229(2):130-138.
    [2] ZHANG P,LIU H H T,LI X B,et al.Fault tolerance of cooperative interception using multiple flight vehicles[J].Journal of the Franklin Institute,2013,350(9):2373-2395.
    [3] 傅强.航空发动机被动容错控制系统鲁棒性设计[J].测控技术,2013,32(5):32-34.FU Q. Robustness design of passive fault tolerant control system for aero engine[J].Measurement & Control Technology, 2013,32(5):32-34(in Chinese).
    [4] 张爱华,胡庆雷,霍星,等.过驱动航天器飞轮故障重构与姿态容错控制[J].宇航学报,2013,34(3):369-376.ZHANG A H,HU Q L,HUO X,et al.Fault reconstruction and fault tolerant attitude control for over-activated spacecraft under reaction wheel failure[J].Journal of Astronautics,2013, 34(3):369-376(in Chinese).
    [5] CHEN F Y,WANG Z,TAO G,et al. Robust adaptive fault-tolerant control for hypersonic flight vehicles with multiple faults[J].Journal of Aerospace Engineering,2015,28(4):04014111.
    [6] HE J J,QI R Y,JIANG B.Adaptive fault-tolerant control design for hypersonic flight vehicles based on feedback linearization[C]//33rd Chinese Control Conference.Piscataway,NJ: IEEE Press,2014:3197-3202.
    [7] YANG G H,ZHANG S Y,LAM J,et al.Reliable control using redundant controllers[J].IEEE Transactions on Automatic Control,1998,43(11):1588-1593.
    [8] PANZA S,LOVERA M.Rotor state feedback in helicopter flight control: Robustness and fault tolerance[C]//2014 IEEE Conference on Control Applications.Piscataway,NJ:IEEE Press,2014:451-456.
    [9] 陈雪芹,耿云海,张迎春,等.基于LMI的鲁棒容错控制及其在卫星姿态控制中的应用[J].控制理论与应用,2008,25(1):95-99.CHEN X Q,GENG Y H,ZHANG Y C,et al.Robust fault-tolerant control based on LMI approach and application in satellite attitude control system[J].Control Theory & Applications,2008,25(1):95-99(in Chinese).
    [10] 陈明,童朝南.不确定系统鲁棒容错控制的LMI设计方法[J].控制与决策,2009,24(4):526-531.CHEN M,TONG C N.LMI approach to robust fault-tolerant H-infinity control for uncertain systems[J].Control and Decision,2009,24(4): 526-531(in Chinese).
    [11] 杨冬梅,孙俊娜.不确定时滞线性离散系统的鲁棒容错控制[J].东北大学学报(自然科学版),2012,33(2):161-164.YANG D M,SUN J N.Robust fault tolerant control for uncertain linear discrete systems with time-delay[J].Journal of Northeastern University(Natural Science),2012,33(2):161-164(in Chinese).
    [12] YE S J,ZHANG Y M,WANG X M,et al.An improved LMI approach for static output feedback fault-tolerant control with application to flight tracking control[C]//4th IEEE Conference on Industrial Electronics and Applications.Piscataway,NJ:IEEE Press,2009:35-40.
    [13] 欧阳高翔,倪茂林,孙承启.视故障为结构不确定项的鲁棒可靠跟踪控制器设计[J].控制理论与应用,2009,26(1): 80-84.OUYANG G X,NI M L,SUN C Q.Robust reliable tracking controller design when the fault is viewed as a structural uncertainty[J].Control Theory & Applications,2009,26(1):80-84 (in Chinese).
    [14] ZHANG Q J,YE S J,LI Y,et al.An enhanced LMI approach for mixed H2/H flight tracking control[J].Chinese Journal of Aeronautics,2011,24(3):324-328.
    [15] 王明昊,刘刚,杨述华.高超声速飞行器的多胞LPV系统控制器设计[J].空间控制技术与应用,2013,39(1):15-22.WANG M H,LIU G,YANG S H.Polytopic-LPV-system-based control design for hypersonic vehicle[J].Aerospace Control and Application,2013,39(1):15-22(in Chinese).
    [16] XIE L.Output feedback H control of systems with parameter uncertainty[J].International Journal of Control,1996,63(4): 741-750.
    [17] 俞立,陈国定,杨马英.不确定系统具有圆盘区域极点约束的鲁棒控制[J].自动化学报,2000,26(l):116-120.YU L,CHEN G D,YANG M Y.Robust control of uncertain linear system with disk pole constraints[J].Acta Automatica Sinica,2000,26(l):116-120(in Chinese).
    [18] HAN X D,LIU J G,XIE D X,et al.Robust H guaranteed cost satisfactory fault-tolerant control for discrete-time systems with quadratic D stabilizability[J].Journal of Systems Engineering and Electronics,2010,21(3):496-502.
    [19] HE Y,WANG Q G.An improved ILMI method for static output feedback control with application to multivariable PID control[J].IEEE Transactions on Automatic Control,2006,51(10): 1678-1683.
    [20] CAO Y Y,LAM J,SUN Y X.Static output feedback stabilization: An ILMI approach[J].Automatica,1998,34(12):1641-1645.
    [21] HOLLIS B R,THOMPSON R A,MURPHY K J,et al.X-33 aerodynamic computations and comparisons with wind-tunnel data[J].Journal of Spacecraft and Rockets,2001,38(5):684-691.
  • 加载中
计量
  • 文章访问数:  659
  • HTML全文浏览量:  2
  • PDF下载量:  598
  • 被引次数: 0
出版历程
  • 收稿日期:  2015-07-09
  • 刊出日期:  2016-07-20

目录

    /

    返回文章
    返回
    常见问答