Journal of Propulsion Technology ›› 2000, Vol. 21 ›› Issue (6): 28-31.

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Mixed H2/H output feedback control of aeroengine based on LMI

  

  1. The 31st Research Inst ,Beijing 100074,China;Data Processing Center,Northwestern Polytechnical Univ ,Xi′an 710072,China
  • Published:2021-08-15

基于LMI的航空发动机混合H2/H输出反馈控制

谢光华,曾庆福   

  1. 航天机电集团公司31所!北京100074;西北工业大学数据处理中心!陕西西安710072
  • 基金资助:
    航空科学基金资助项目! (96C5 30 40 )

Abstract: According to the shortage of H ∞ controllers in time-domain performance, mixed H 2/H ∞ control problem was investigated For a species of systems with structured perturbations, the sufficient and necessary condition that there were mixed H 2/H ∞ controllers and the method to design a controller were presented The simulation results for a certain double spool turbojet aero-engine reveals that the robust control with no static error for both rotational velocity of low-pressure rotor and temperature at low-pressure turbine outlet in the same time can be realized And the dynamic performance character of closed loop system is also improved evidently

Key words: Aircraft engine;Control system;Feedback control;Matrix algorihm

摘要: 针对H∞ 控制器在时域性能方面的不足 ,研究了混合H2 /H∞ 控制问题 ,给出了一类结构摄动系统混合H2 /H∞ 控制器存在的充要条件和控制器的设计方法。对某双转子涡喷发动机的仿真结果表明 ,可以对低压转子转速和低压涡轮后温度同时实现无静差鲁棒控制 ,并使闭环系统的动态性能品质获得明显改善

关键词: 航空发动机;控制系统;反馈控制;矩阵算法