首页 | 本学科首页   官方微博 | 高级检索  
     检索      

一种多变量频域动态伪对角化法及航空发动机解耦控制器设计
引用本文:彭凯,樊丁,郭雅楠,卜振鹏,焦春波,薜原.一种多变量频域动态伪对角化法及航空发动机解耦控制器设计[J].航空动力学报,2016,31(9):2276-2282.
作者姓名:彭凯  樊丁  郭雅楠  卜振鹏  焦春波  薜原
作者单位:1. 西北工业大学 动力与能源学院, 西安 710072;
基金项目:国家自然科学基金(51506176)
摘    要:针对多变量频域Nyquist类设计法中的Hawkins伪对角化法,给出了一种改进的动态伪对角化方法来提高系统的对角优势度以改善系统的解耦性与鲁棒性并进行了相关分析.最后将这种动态伪对角化方法用于某型航空发动机稳态控制器的设计,仿真结果表明:相较于标准Hawkins法,改进的动态伪对角化所给出的补偿系统具有较好的动静态解耦性与鲁棒性. 

关 键 词:多变量    频域    伪对角化    鲁棒性    航空发动机
收稿时间:2014/12/7 0:00:00

A multivariable frequency-domain dynamic pseudodiagonalization method and design of aero-engine decoupling controller
PENG Kai,FAN Ding,GUO Ya-nan,BU Zhen-peng,JIAO Chun-bo and XUE Yuan.A multivariable frequency-domain dynamic pseudodiagonalization method and design of aero-engine decoupling controller[J].Journal of Aerospace Power,2016,31(9):2276-2282.
Authors:PENG Kai  FAN Ding  GUO Ya-nan  BU Zhen-peng  JIAO Chun-bo and XUE Yuan
Institution:1. School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072;2. Collaborative Innovation Center for Advanced Aero-Engine, Beijing 100191, China;3. Unit 92728 of People's Liberation Army of China, Shanghai 200436, China;4. Military Resident Representative Bureau of Rocket Force in Jinzhou, Jinzhou Liaoning 121000, China;5. Operating Branch of Xi'an Metro Company Limited, Xi'an 710018, China
Abstract:For Hawkins''s pseudodiagonalization method in multivariable Nyquist-class frequency domain design, an improved dynamic pseudodiagonalization method was presented to enhance the diagonal dominance of the system in order to improve the decoupling and robustness of the system together with relevant analysis. Finally, the dynamic pseudodiagonalization method was used to design an aero-engine steady controller. The simulation results show that the compensated system given by improved dynamic pseudodiagonalization method has good dynamic and static decoupling and robustness compared with standard Hawkins''s method.
Keywords:multivariable  frequency domain  pseudodiagonalization  robustness  aero-engine
本文献已被 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号