Improvement of taxiing performance for civil airliner by active control

Yuhong Jia; Ying Liu

Improvement of taxiing performance for civil airliner by active control

Yuhong Jia^*
, Ying Liu

^*此作品的通讯作者

航空科学与工程学院

Beihang University

科研成果: 期刊稿件 › 文章 › 同行评审

2 引用（Scopus）

摘要

Based on two performance indexes including vertical acceleration and vertical displacement of the body of civil airliner, by the nonlinear model of self-tuning of landing gear and the ARAMX model of system, using the design of controller for the multistep recursive predictor and the identification of the model parameters and system structure, the self-tuning control of landing gear was implemented. The simulation results show that the control scheme can improve the performance of taxiing for civil airliner.

源语言	英语
页（从-至）	1017-1021
页数	5
期刊	Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
卷	29
期	11
出版状态	已出版 - 11月 2003

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引用此

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title = "Improvement of taxiing performance for civil airliner by active control",

abstract = "Based on two performance indexes including vertical acceleration and vertical displacement of the body of civil airliner, by the nonlinear model of self-tuning of landing gear and the ARAMX model of system, using the design of controller for the multistep recursive predictor and the identification of the model parameters and system structure, the self-tuning control of landing gear was implemented. The simulation results show that the control scheme can improve the performance of taxiing for civil airliner.",

keywords = "Landing gear, Nonlinear model, Parameter identification, Self-tuning control",

author = "Yuhong Jia and Ying Liu",

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T1 - Improvement of taxiing performance for civil airliner by active control

AU - Jia, Yuhong

AU - Liu, Ying

PY - 2003/11

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N2 - Based on two performance indexes including vertical acceleration and vertical displacement of the body of civil airliner, by the nonlinear model of self-tuning of landing gear and the ARAMX model of system, using the design of controller for the multistep recursive predictor and the identification of the model parameters and system structure, the self-tuning control of landing gear was implemented. The simulation results show that the control scheme can improve the performance of taxiing for civil airliner.

AB - Based on two performance indexes including vertical acceleration and vertical displacement of the body of civil airliner, by the nonlinear model of self-tuning of landing gear and the ARAMX model of system, using the design of controller for the multistep recursive predictor and the identification of the model parameters and system structure, the self-tuning control of landing gear was implemented. The simulation results show that the control scheme can improve the performance of taxiing for civil airliner.

KW - Landing gear

KW - Nonlinear model

KW - Parameter identification

KW - Self-tuning control

UR - https://www.scopus.com/pages/publications/1542712601

M3 - 文章

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JO - Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics

JF - Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics

IS - 11

ER -

Improvement of taxiing performance for civil airliner by active control

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