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基于改进滑模趋近律的航空发动机控制器设计
引用本文:刘帅,王金环,白杰,戴士杰.基于改进滑模趋近律的航空发动机控制器设计[J].科学技术与工程,2019,19(34).
作者姓名:刘帅  王金环  白杰  戴士杰
作者单位:河北工业大学 机械工程学院,河北工业大学 理学院,河北工业大学 机械工程学院;中国民航大学 天津市民用航空器适航与维修重点实验室;中国民航大学 天津市民用航空器适航与维修重点实验室,河北工业大学 机械工程学院
摘    要:将多幂次滑模趋近律用于航空发动机控制,设计了基于滑模控制方法的航空发动机追踪控制器。针对多幂次滑模趋近律在航空发动机追踪控制中出现的高频振荡问题,提出了一种改进的多幂次滑模趋近律。基于改进多幂次滑模趋近律的追踪控制仿真表明,改进的多幂次滑模趋近律适用于航空发动机追踪控制,该方法不仅具备了多幂次滑模趋近方法响应速度快、鲁棒性好的优点,而且消除了控制中的高频振荡现象。

关 键 词:航空发动机  滑模控制  趋近律  多幂次
收稿时间:2019/5/21 0:00:00
修稿时间:2019/6/30 0:00:00

The Controller Design for Aero-Engine Based on Improved Reaching Law of Sliding Mode Control
LIU Shuai,Wang JinHuan,BAI Jie and Dai ShiJie.The Controller Design for Aero-Engine Based on Improved Reaching Law of Sliding Mode Control[J].Science Technology and Engineering,2019,19(34).
Authors:LIU Shuai  Wang JinHuan  BAI Jie and Dai ShiJie
Institution:School of Mechanical Engineering,Hebei University of Technology,China School of Sciences,Hebei University of Technology,School of Mechanical Engineering,Hebei University of Technology;Tianjin Key Laboratory for Civil Airworthiness and Maintenance,Civil Aviation University of China,School of Mechanical Engineering,Hebei University of Technology
Abstract:An improved sliding mode control algorithm is applied to aeroengine control, for which the controller is designed that based on sliding mode control. An improved multi power reaching law of sliding mode control is proposed in this paper, which aims at reducing high frequency oscillation phenomenon appeared in multi power tracking control process of aero engine. The proposed reaching law is used in simulation of aero engine control system, whose results show that the proposed reaching law is applicable for tracking control of aero engine. Not only does the proposed reaching law has these advantages that are fast response speed and strong robustness but also it can eliminate high frequency oscillation phenomenon.
Keywords:Aero-Engine  Sliding Mode  Control  Reaching  Law  Multi  Power
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