代冀阳, 高强, 吴印华. 基于Krylov子空间的直升机降阶控制器设计[J]. 南昌航空大学学报(自然科学版), 2008, 22(3): 57-61.
引用本文: 代冀阳, 高强, 吴印华. 基于Krylov子空间的直升机降阶控制器设计[J]. 南昌航空大学学报(自然科学版), 2008, 22(3): 57-61.
DAI Ji-yang, GAO Qiang, WU Yin-hua. Design of controller reduction of helicopters based on Krylov subspace[J]. Journal of nanchang hangkong university(Natural science edition), 2008, 22(3): 57-61.
Citation: DAI Ji-yang, GAO Qiang, WU Yin-hua. Design of controller reduction of helicopters based on Krylov subspace[J]. Journal of nanchang hangkong university(Natural science edition), 2008, 22(3): 57-61.

基于Krylov子空间的直升机降阶控制器设计

Design of controller reduction of helicopters based on Krylov subspace

  • 摘要: 目前直升机控制器的阶数往往较高,在保证闭环性能的情况下,如何尽可能地降低控制器阶数是亟待解决的问题.本文将一种基于Krylov子空间的控制器降阶方法应用于直升机模型的控制器,不仅设计出的降阶控制器能够完全符合闭环系统要求;而且该方法不需要解Lyapunov方程和使用工具箱,大大地减小了计算量.仿真结果也表明了此方法的有效性和实用性.

     

    Abstract: The order of helicopter controller is usually high.How to reduce the order of controller as much as possible and preserve the performance of closed-loop system is a problem which needs solving.In this paper,a Krylov subspace method is applied to H controller reduction of UH-60A helicopter.It is shown that the proposed method can not only match the desired closed-loop system responses,but also does not need solving any Lyapunov equations and using computational tools,greatly reducing computation work.The simulation results also show the effectiveness of the method.

     

/

返回文章
返回