MULTIVARIABLE

作品数：107被引量：242H指数：7
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相关作者：陈之兵张新建郑怀林陈维南童丽更多>>
相关机构：深圳大学国防科学技术大学东南大学艾默生电气中国投资有限公司更多>>
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相关基金：国家自然科学基金中国博士后科学基金国家重点基础研究发展计划北京市自然科学基金更多>>
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Design method of multivariable PI controller for turboprop engine based on equivalent transfer function
《Chinese Journal of Aeronautics》2024年第9期237-260,共24页Shancheng LI Yong WANG Haibo ZHANG 
support by the National Natural Science Foundation of China (No.52202474);China Postdoctoral Science Foundation (No.2023M731655);Major Projects of National Science and Technology,China (No.J2019-I-0020-0019);Advanced Aviation Power Innovation Workstation Project,China (No.HKCX2022-01-026-03);Basic Research Business Fees for Central Universities,China (No.NT2023004);Nanjing University of Aeronautics and Astronautics Forward-looking Layout Research Project,China (No.1002-ILA22037-1A22).
Traditional centralized Proportional Integral(PI)controller design methods based on Equivalent Transfer Functions(ETFs)have poor decoupling effect in turboprop engines.In this paper,a centralized PI design method base...
关键词：Multivariable control sys-tems Equivalent transfer function Disturbance compensation control Control parameter design Turboprop engine control 
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 
A novel model-based multivariable framework for aircraft gas turbine engine limit protection control被引量：3
《Chinese Journal of Aeronautics》2021年第12期57-72,共16页Shuwei PANG Soheil JAFARI Theoklis NIKOLAIDIS Qiuhong LI 
supported by China Scholarship Council(No.201906830081)。
Control technologies are innovated to satisfy increasingly complicated control demands of gas turbine engines.In terms of limit protection control,a novel model-based multivariable limit protection control method,whic...
关键词：Amplitude conversion Command reconstruction Gas turbine engine Limit protection control Multivariable control Onboard prediction 
MULTIVARIABLE MODEL REFERENCE ADAPTIVE CONTROL FOR A TURBOFAN ENGINE被引量：6
《Chinese Journal of Aeronautics》1996年第4期300-304,共5页Fan Jun Huang Jinquan Sun Jianguo Feng Zhengping(Dep. Of Power Engineering, Nanjing University of Aeronauticsand Astronautics, Nanjing,China, 210026) 
A decentralized model reference adaptive control (MRAC) scheme is proposed and applied to design a multivariable control system of a dual-spool turbofan engine.Simulation studies show good static and dynamic performan...
关键词：turbofan engines model reference adaptive control flight envelopes multivariable control 
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