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Self-tuning control of landing gear load

  • Beihang University

科研成果: 期刊稿件文章同行评审

摘要

A controller is designed by establishing the nonlinear model and the ARMAX model of system for the self-tuning of landing gear. The self-tuning control is realized in combination with parameter identification. The simulation results show that the control scheme can improve the absorber capability of landing gear.

源语言英语
页(从-至)237-241
页数5
期刊Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
25
3
出版状态已出版 - 5月 2004

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