[an error occurred while processing this directive]
   
 
���¿��ټ��� �߼�����
   ��ҳ  �ڿ�����  ��ί��  Ͷ��ָ��  �ڿ�����  ��������  �� �� ��  ��ϵ����
�������պ����ѧѧ�� 2007, Vol. 33 Issue (05) :572-576    DOI:
���� ����Ŀ¼ | ����Ŀ¼ | ������� | �߼����� << | >>
���п����е�һ���������ſ��Ʒ��䷽��
������, �߽�Դ, �깦�*
�������պ����ѧ �Զ�����ѧ���������ѧԺ, ���� 100083
New optimal control allocation method for flight control system
Yang Lingyu, Gao Jinyuan, Shen Gongzhang*
School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

ժҪ
�����
�������
Download: PDF (401KB)   HTML 1KB   Export: BibTeX or EndNote (RIS)      Supporting Info
ժҪ �����һ���������������Ŀ��Ʒ�������,�����һ��ȫ�µ����ſ��Ʒ����㷨——��������.�÷������Ż�Ŀ�갴�շ��п��Ƶ�����ֳɿ���Ŀ�������Ŀ������,�Ի��׵���ʽ�Զ�������������,��������������Ŀ��������Ż�ָ���������,�������Ż�����ת��������������Խ��.ͨ���뼸�ֳ��ÿ��Ʒ��䷽���ıȽϼ����������п���ϵͳ�ķ�����֤,����������������׼ȷʵ������Ŀ���ͬʱ��ø��õ�����Ŀ�������,���ɵĿ���ϵͳ�ܰ�����Ҫ��׼ȷ�����ٵظ���ָ���ź�,������Ч�����Ʒɻ�������ͨ��֮���Ӱ��.
Service
�ѱ����Ƽ�������
�����ҵ����
�������ù�����
Email Alert
RSS
�����������
�ؼ����� ���п���ϵͳ   ���ſ��Ʒ���   ����     
Abstract�� Control allocation method was investigated with the background of aircraft with multiple control effectors. A new optimal control allocation method, bases sequence control allocation, was put forward. The optimal objectives were divided into control objective and mission objective, and the control objective should be fulfilled firstly. The actuators were recombined, and the efficiency vectors of the actuators were treated as the bases of multidimensional space. All of the bases were sequenced according to the control object and the mission objective. Then the optimization of redundancy system was transformed to a sequencing problem. Comparison with other allocation method and control system simulation results show the bases sequence method can achieve the objective accurately and optimally, and can be computed in real-time. The response of the control system is rapid and accurate, and shows good decouple performance among axes.
Keywords�� flight control system   optimal control allocation   redundancy     
Received 2006-06-13;
Fund:

����973������Ŀ(5132004)

About author: ������(1979-),��,���ּ�������,��ʿ��,yly@asee.buaa.edu.cn.
���ñ���:   
������, �߽�Դ, �깦�.���п����е�һ���������ſ��Ʒ��䷽��[J]  �������պ����ѧѧ��, 2007,V33(05): 572-576
Yang Lingyu, Gao Jinyuan, Shen Gongzhang.New optimal control allocation method for flight control system[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2007,V33(05): 572-576
���ӱ���:  
http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2007/V33/I05/572
Copyright 2010 by �������պ����ѧѧ��