LPV

作品数：208被引量：651H指数：13
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相关领域：自动化与计算机技术更多>>
相关作者：郑总准杨凌宇董朝阳吴建武李爱国更多>>
相关机构：江南大学哈尔滨工业大学南京航空航天大学北京航空航天大学更多>>
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相关基金：国家自然科学基金中国航空科学基金中央高校基本科研业务费专项资金国家教育部博士点基金更多>>
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Direct thrust control for multivariable turbofan approach被引量：4
《Chinese Journal of Aeronautics》2022年第6期125-136,共12页Yiyang ZHU Jinquan HUANG Muxuan PAN Wenxiang ZHOU 
supported by the National Science and Technology Major Project, China (No. 2017-V-0004-0054)
A novel turbofan Direct Thrust Control(DTC)architecture based on Linear ParameterVarying(LPV)approach for a two-spool turbofan engine thrust control is proposed in this paper.Instead of transforming thrust command to ...
关键词：Turbofan engine Direct thrust control Linear Parameter Varying(LPV)approach Particle Swarm Optimization(PSO) Robust LPV H∞filter 
LPV modeling and controller design for body freedom flutter suppression subject to actuator saturation被引量：1
《Chinese Journal of Aeronautics》2020年第10期2679-2693,共15页Wei TANG Yu WANG Jiawei GU Zhiwei SUN 
the National Natural Science Foundation of China(No.61573289);Space Science and Technology Fund,and Natural Science Basic Research Plan in Shaanxi Province of China(No.2019JM042);Fundamental Research Funds for the Central Universities of China(No.3102019ZDHKY11)。
In recent years,the Active Flutter Suppression(AFS)employing Linear ParameterVarying(LPV)framework has become a hot spot in the research field.Nevertheless,the flutter suppression technique is facing two severe challe...
关键词：Anti-windup compensation Flutter suppression Linear parameter-varying interpolation Model order reduction SATURATION 
Robust LPV modeling and control of aircraft flying through wind disturbance被引量：11
《Chinese Journal of Aeronautics》2019年第7期1588-1602,共15页Zhenxing GAO Jun FU 
co-supported by the National Natural Science Foundation of China(Nos.U1533120 and U1733122);the Fundamental Research Funds for the Central Universities of China(No.NS2015066)
This article deals with the disturbance attenuation control of aircraft flying through wind shear via Linear Parameter Varying(LPV) modeling and control method. A Flight Dynamics Model(FDM) with wind shear effects con...
关键词：Function SUBSTITUTION Linear parameter varying LPV CONTROL ROBUST CONTROL Wind shear 
A systematic method of smooth switching LPV controllers design for a morphing aircraft被引量：19
《Chinese Journal of Aeronautics》2015年第6期1640-1649,共10页Jiang Weilai Dong Chaoyang Wang Qing 
supported by the National Natural Science Foundation of China(Nos.61273083 and 61374012)
This paper is concerned with a systematic method of smooth switching linear parameter- varying （LPV） controllers design for a morphing aircraft with a variable wing sweep angle. The morphing aircraft is modeled as a...
关键词：Morphing aircraft Parameter set division：Robust control Smooth switching Switched linear parameter-varying system 
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