Adaptive control for semi-active landing gear

Yuhong Jia; Jianjun Wang

Adaptive control for semi-active landing gear

Yuhong Jia^*
, Jianjun Wang

^*Corresponding author for this work

School of Aeronautic Science and Engineering

Beihang University

Research output: Contribution to journal › Article › peer-review

3 Scopus citations

Abstract

Combining optimal control and self-tuning control theory, the adaptive control strategy for semi-active landing gear is proposed. The mathematical model describing the absorber system in the airplane landing gear is established and the semi-active controller is designed and used in the system based on analyzing the influence of the parameters on the system performance. The simulation results demonstrate that the control scheme can improve airplane taxing performance and operation stability performance.

Original language	English
Pages (from-to)	55-58+87
Journal	Zhendong yu Chongji/Journal of Vibration and Shock
Volume	25
Issue number	2
State	Published - Apr 2006

Keywords

Landing gear
Parameter identification
Semi-active control
Simulation

Cite this

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title = "Adaptive control for semi-active landing gear",

abstract = "Combining optimal control and self-tuning control theory, the adaptive control strategy for semi-active landing gear is proposed. The mathematical model describing the absorber system in the airplane landing gear is established and the semi-active controller is designed and used in the system based on analyzing the influence of the parameters on the system performance. The simulation results demonstrate that the control scheme can improve airplane taxing performance and operation stability performance.",

keywords = "Landing gear, Parameter identification, Semi-active control, Simulation",

author = "Yuhong Jia and Jianjun Wang",

year = "2006",

month = apr,

language = "英语",

volume = "25",

pages = "55--58+87",

journal = "Zhendong yu Chongji/Journal of Vibration and Shock",

issn = "1000-3835",

publisher = "Chinese Vibration Engineering Society",

number = "2",

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TY - JOUR

T1 - Adaptive control for semi-active landing gear

AU - Jia, Yuhong

AU - Wang, Jianjun

PY - 2006/4

Y1 - 2006/4

N2 - Combining optimal control and self-tuning control theory, the adaptive control strategy for semi-active landing gear is proposed. The mathematical model describing the absorber system in the airplane landing gear is established and the semi-active controller is designed and used in the system based on analyzing the influence of the parameters on the system performance. The simulation results demonstrate that the control scheme can improve airplane taxing performance and operation stability performance.

AB - Combining optimal control and self-tuning control theory, the adaptive control strategy for semi-active landing gear is proposed. The mathematical model describing the absorber system in the airplane landing gear is established and the semi-active controller is designed and used in the system based on analyzing the influence of the parameters on the system performance. The simulation results demonstrate that the control scheme can improve airplane taxing performance and operation stability performance.

KW - Landing gear

KW - Parameter identification

KW - Semi-active control

KW - Simulation

UR - https://www.scopus.com/pages/publications/33745638788

M3 - 文章

AN - SCOPUS:33745638788

SN - 1000-3835

VL - 25

SP - 55-58+87

JO - Zhendong yu Chongji/Journal of Vibration and Shock

JF - Zhendong yu Chongji/Journal of Vibration and Shock

IS - 2

ER -

Adaptive control for semi-active landing gear

Abstract

Keywords

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