Journal of Systems Engineering and Electronics ›› 2013, Vol. 35 ›› Issue (6): 1268-1274.doi: 10.3969/j.issn.1001-506X.2013.06.23

• 制导、导航与控制 • 上一篇    下一篇

无人直升机局部H最优LPV 速度控制器设计

贺跃帮1,裴海龙1,周洪波2   

  1. 1. 华南理工大学自主系统与网络控制教育部重点实验室,广东 广州 510640;
    2. 湖南理工学院机械工程学院,湖南 岳阳 414006
  • 收稿日期:2012-02-28 修回日期:2013-02-07 出版日期:2013-06-15 发布日期:2013-04-09

Local Hoptimal LPV velocity controller design for unmanned helicopter

HE Yue-bang 1,PEI Hai-long 1,ZHOU Hong-bo2   

  1. 1. Key Laboratory of Autonomous Systems and Networked Control, Ministry of Education, South China
    University of Technology, Guangzhou 510640, China; 2. School of Mechanical Engineering, Hunan
    Institute of Science and Technology, Yueyang, 414006, China
  • Received:2012-02-28 Revised:2013-02-07 Online:2013-06-15 Published:2013-04-09

摘要:

针对无人直升机的大范围鲁棒控制问题, 提出局部H最优线性变参数(liner parameter varying, LPV)速度(local Hoptimal LPV velocity, LHOV)控制方法。首先将无人直升机系统简化成含有干扰的LPV 系统,接着针对各个固定飞行模式独立设计H静态输出反馈(Hstatic output feedback, HSOF)控制器,然后采用插补控制技术,针对每一种飞行模式下的线性系统设计一个只含有不可控部分和不可观部分的插补控制器,进而将所有模式下的控制器融合成一个LHOV控制器,从而既保证模式之间鲁棒转换,又使得系统进入任意一个模式后能达到H性能最优。最后,仿真结果表明,采用此方法设计的控制器能够获得大范围良好的稳定性和鲁棒性。

Abstract:

Considering the large rang robust control problem of an unmanned helicopter, a local H optimal linear parameter varying (LPV) velocity (LHOV) controller is designed. Firstly the nonlinear system of the helicopter is simplified as an LPV system with disturbances, then a Hstatic output feedback (HSOF) controller for every fixed flight mode independently is designed. The interpolation control technique is used to design an interpolated controller for every local controller. The interpolated controllers only include uncontrollable modes and unobservable modes, so the optimal H performance can be ensured when the helicopter flights in this mode. Finally, an LHOV controller is composed of these local controllers, and simulation results illustrate its good large rang stability and robustness.