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�������պ����ѧѧ�� 2003, Vol. 29 Issue (11) :1017-1021    DOI:
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�����, ��ӥ*
�������պ����ѧ ���տ�ѧ�빤��ѧԺ, ���� 100083
Improvement of taxing performance for civil airliner by active control
Jia Yuhong, Liu Ying*
School of Aeronautics Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

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Abstract�� Based on two performance indexes of vertical acceleration and vertical displacement of body, by the non-linear model of self-tuning of landing gear and the ARAMX model of system, using the design of controller of the multi-step 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 effectively improve the performance of taxing for civil airliner.
Keywords�� landing gears   non-linear model   parameter identification   self-tuning control     
Received 2003-07-01;
About author: �����(1966-),Ů,�ӱ�������,������,Jiayuhong@buaa.edu.cn.
�����, ��ӥ.������������������ÿͻ��Ļ�������[J]  �������պ����ѧѧ��, 2003,V29(11): 1017-1021
Jia Yuhong, Liu Ying.Improvement of taxing performance for civil airliner by active control[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2003,V29(11): 1017-1021
http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2003/V29/I11/1017
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