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  • 标题:Nonlinear control study on aircraft engine using a generalized minimum variance approach
  • 本地全文:下载
  • 作者:Bing Yu ; Yang Gao ; Jiqiang Wang
  • 期刊名称:Advances in Mechanical Engineering
  • 印刷版ISSN:1687-8140
  • 电子版ISSN:1687-8140
  • 出版年度:2016
  • 卷号:8
  • 期号:9
  • DOI:10.1177/1687814016667383
  • 语种:English
  • 出版社:Sage Publications Ltd.
  • 摘要:With the requirements of the advanced propulsion systems for aircraft control performance increasing, it has attracted the attention to design more efficient controller that is based on the nonlinear model over the flight envelope directly. A nonlinear aircraft engine control method based on generalized minimum variance approach is studied. A nonlinear autoregressive with extra input aircraft engine model for a certain turbofan engine is built and is chosen as the control plant in this study. Then, a controller is designed for the identification model based on the nonlinear generalized minimum variance theory. And simulation results manifest the controller to satisfy the requirements of the tracking with the transient process and the regulation with the steady process.
  • 关键词:Aircraft engine; nonlinear generalized minimum variance; nonanalytical mathematical model
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