引用本文:
【打印本页】   【HTML】 【下载PDF全文】   查看/发表评论  【EndNote】   【RefMan】   【BibTex】
←前一篇|后一篇→ 过刊浏览    高级检索
本文已被:浏览 1257次   下载 593 本文二维码信息
码上扫一扫!
分享到: 微信 更多
基于LMI的航空发动机混合H2/H输出反馈控制
谢光华1, 曾庆福2
1.航天机电集团公司31所!北京100074;2.西北工业大学数据处理中心!陕西西安710072
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
DOI:
分类号:
基金项目:航空科学基金资助项目! (96C5 30 40 )
Mixed H2/H output feedback control of aeroengine based on LMI
Xie Guang-hua1, Zeng Qing-fu2
1.The 31st Research Inst ,Beijing 100074,China;2.Data Processing Center,Northwestern Polytechnical Univ ,Xi′an 710072,China
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