文章基本信息

标题：AERO-ENGINE VARIABLE STRUCTURE GLOBAL FAST TERMINAL SLIDING MODE CONTROL METHOD
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作者：LI YONG ; FAN DING
期刊名称：Journal of Theoretical and Applied Information Technology
印刷版ISSN：1992-8645
电子版ISSN：1817-3195
出版年度：2013
卷号：51
期号：2
出版社：Journal of Theoretical and Applied
摘要：One new kind of aero-engine control method based on the variable structure global fast terminal sliding mode control is proposed for the varying uncertainty nonlinear system of aero-engine. The aero-engine global fast terminal sliding mode variable structure controller has been designed by the in-depth study of VSTSMC theory.The simulation results show that the designed controller has good control effect and strong suppression of external interference, so that the controlled system has strong robustness in the entire control stage.
关键词：Global Fast Terminal Sliding Mode; Aero-engine; Variable Structure Control