起落架载荷的自校正控制

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

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Self-tuning Control of Landing Gear Load

JIA Yu-hong, LIU Ying

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

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

JIA Yu-hong;LIU Ying. Self-tuning Control of Landing Gear Load[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2004, 25(3): 237-241.

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Self-tuning Control of Landing Gear Load

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