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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2004, Vol. 25 ›› Issue (3): 237-241.

• 论文 • Previous Articles     Next Articles

Self-tuning Control of Landing Gear Load

JIA Yu-hong, LIU Ying   

  1. Department of Flight Vehicle Design and Applied Mechanics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
  • Received:2003-05-09 Revised:2003-07-01 Online:2004-06-25 Published:2004-06-25

Abstract: The controller is designed by establishing the non-linear 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 effectively improve the absorber capability of landing gear.

Key words: landing gear, taxing load, non-linear model, parameter identification, self-tuning control