Multivariable steady state control of aeroengine based on backstepping method

Xin Yue Ma, Lin Feng Gou, Chen Yang Zhao, Ying Wang

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

Aeroengine control system is based on engine model design, to ensure that the engine can operate stably, safely and reliably under various working conditions and working conditions. Stability control is the basic performance requirement of engine control system. In this paper, based on the existing linear state variable model and linear variable parameter model (LPV) of a turbofan engine, aiming at the characteristics of backstepping method, the nonlinear affine model of aeroengine is established, and the backstepping control law is designed by using backstepping method to realize the steady-state control of aeroengine. The simulation results show that in the process of engine steady-state control, the control law can ensure that the controlled variables can quickly restore to the original stable state under disturbance conditions. The research shows that the steady-state control method of engine established in this paper has certain engineering practical value.

源语言英语
主期刊名2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
出版商Institute of Electrical and Electronics Engineers Inc.
42-46
页数5
ISBN(电子版)9781728155357
DOI
出版状态已出版 - 7月 2019
活动10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019 - Brussels, 比利时
期限: 22 7月 201925 7月 2019

出版系列

姓名2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019

会议

会议10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
国家/地区比利时
Brussels
时期22/07/1925/07/19

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