基于干扰观测器的高超音速飞行器鲁棒反步控制
DOI:
CSTR:
作者:
作者单位:

西北工业大学自动化学院

作者简介:

王首斌

通讯作者:

中图分类号:

V448.2

基金项目:

西北工业大学新教师基金项目(11GH0322).


Robust backstepping control based on disturbance observer for#br# hypersonic vehicle
Author:
Affiliation:

School of Automation, Northwestern Polytechnical University

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    针对高超音速飞行器严格反馈不确定非线性MIMO系统, 提出一种基于干扰观测器的鲁棒反步控制方法.
    该方法采用超扭曲算法设计干扰观测器以估计系统复合干扰, 观测误差有限时间收敛. 设计非线性反步控制律, 引入
    鲁棒项使得系统满足干扰到性能输出的??2 增益不超过设定的正实数, 满足耗散不等式, 使闭环系统跟踪误差一致最
    终有界稳定. 仿真结果表明, 所设计的控制律可以有效抑制系统复合干扰的影响, 设计方法可行.

    Abstract:

    To solve the control problem of a general hypersonic vehicle which is a strict-feedback nonlinear uncertain MIMO
    system, a robust backstepping control strategy based on the disturbance observer is proposed. The super-twisting algorithm
    is used to estimate and compensate for disturbances. The finite time convergence is guaranteed. A nonlinear backstepping
    control law is designed. Robust items are designed to make the whole control system has the ??2 gain which is less than or
    equal to the prescribed positive const. Theoretical analysis is done to validate that the system can satisfy dissipative inequality
    and is uniformly ultimately bounded. The simulation results show that the developed method is effective and deals with the
    problem of uncertain factors preferably.

    参考文献
    相似文献
    引证文献
引用本文

王首斌 王新民 谢蓉 姚从潮.基于干扰观测器的高超音速飞行器鲁棒反步控制[J].控制与决策,2013,28(10):1507-1512

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:2012-05-10
  • 最后修改日期:2012-09-26
  • 录用日期:
  • 在线发布日期: 2013-10-20
  • 出版日期:
文章二维码