Fast Response Control of Turbofan Engines Using a Finite Time Approach

摘要：

　　Increasing requirements from flight control demand fast regulation of engine control systems.This has motivated research on advanced control of turbofan engines.One of the attempts is to employ nonlinear design techniques in consideration of the inherent nonlinearity of the engine dynamics.In this note,a finite-time based control approach is proposed for fast response control of turbofan engines.Results on control design are obtained that stabilizes the closed-loop system in a finite time.The proposed design is then validated though a numerical example.The study also shows that the proposed controller possesses good robustness to fuel flow pulsation and aero-dynamical coupling disturbances.

关键词： Set-point control turbofan engine control finite-time control

作者: WANG Jiqiang DIMIROVSKI Georgi YUE Hong

作者单位: Jiangsu Province Key Laboratory of Aerospace Power Systems,Nanjing University of Aeronautics & Astro Dogus University of Istanbul,Istanbul 34722,Turkey Industrial Control Centre,University of Strathclyde,Glasgow G1 1XW,UK

会议类型: 国际会议

会议名称: The 33th Chinese Control Conference第33届中国控制会议

会议地点: 南京

会议语种:英文

页码: 3632-3636

在线出版日期: 2014-07-28（万方平台首次上网日期，不代表论文的发表时间）