[an error occurred while processing this directive]
���¿��ټ��� �߼�����
   ��ҳ  �ڿ�����  ��ί��  Ͷ��ָ��  �ڿ�����  ��������  �� �� ��  ��ϵ����
�������պ����ѧѧ�� 2003, Vol. 29 Issue (12) :1119-1122    DOI:
���� ����Ŀ¼ | ����Ŀ¼ | ������� | �߼����� << | >>
�ɶ��ɻ�����о���, �ɶ� 610041
LQ optimal simulation for aircraft anti-skid brake control system
Huang You*
Chengdu Aircraft Design and Research Institute, Chengdu 610041, China

Download: PDF (481KB)   HTML 1KB   Export: BibTeX or EndNote (RIS)      Supporting Info
ժҪ �����ִ������������Զ�����(LQ)���ſ������۶Էɻ��Զ�����ɲ������ABSϵͳ����������ķ����о�,������Matlab���ſ��ƹ����估Simulink��ɲ������ϵͳ�����˷���,��������ۺϿ����˷ɻ����塢������̥��·��״����ɲ������װ�õ�����,��״̬�ռ���ʽ�����˷ɻ�ɲ�����ܵĶ���ѧģ��,ͨ�������ƶ�ѹ�������ƻ��ֵĻ�����,ʹ��ﵽ����ֵ,������ŷ�������,����������������ģ��,������Ƴ��ɻ�����ɲ��ϵͳ����³��������.
Email Alert
�ؼ����� LQ���ſ���   ���Զ�����   ɲ��ϵͳ   ״̬�ռ䷽��   ����     
Abstract�� Linear-Quadratic optimal control technique, Matlab optimal toolbox and Simulink were applied for aircraft anti-skid brake control system, according to aircraft body,tyre,ground and brake device. The dynamic model was given by modern state-space method, optimal state-feedback gain was calculated and the robust controller of aircraft anti-skid brake system was designed.
Keywords�� Linear-Quadratic optimal control technique   aircraft anti-skid   brake system   state-space method   simulation     
Received 2003-06-20;
About author: �� ��(1963-),��,���ϳ�ɳ��,�о�Ա, huangyou63@163.com.
����.�ɻ�����ɲ������ϵͳLQ���ſ��Ʒ���[J]  �������պ����ѧѧ��, 2003,V29(12): 1119-1122
Huang You.LQ optimal simulation for aircraft anti-skid brake control system[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2003,V29(12): 1119-1122
http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2003/V29/I12/1119
Copyright 2010 by �������պ����ѧѧ��