location: Current position: Home >> Scientific Research >> Paper Publications

H∞ control for tracking targets of aero-engines

Hits:

Indexed by:会议论文

Date of Publication:2016-07-27

Included Journals:EI、Scopus

Volume:2016-August

Page Number:5879-5884

Abstract:An H∞controller design technique for tracking targets is proposed based on a switched model of an aero-engine. Firstly, a switched LPV model is constructed using gain-scheduling parameters, which owns the advantages of nonlinearity and real time observation. Secondly, a sufficient theoretical criterion is provided to guarantee the H∞performance in the format of linear matrix inequalities (LMIs), where the switched controllers can be easily constructed by utilizing LMIs Toolbox in Matlab. Finally, simulation results are given to show the validity of the proposed design method. © 2016 TCCT.

Pre One:Experimental comparisons of hypothesis test and moving average based combustion phase controllers

Next One:Finite convergence of value iteration algorithm for discounted infinite horizon optimal control of stochastic logical systems