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�������պ����ѧѧ�� 2003, Vol. 29 Issue (12) :1133-1135    DOI:
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����1, ������2, ���3*
1. ������ҵ��ѧ �ɻ�ϵ, ���� 710072;
2. �վ��Ϻ�������������, �Ϻ� 200233;
3. ������ҵ��ѧ �Զ�����ϵ, ���� 710072
Dynamic reverse and fuzzy integrated control of unmanned helicopters
Shen Yi1, Yu Xiaomin2, Li Aijun3*
1. Dept. of Aircraft Engineering, Northwestern Polytechnical University, Xi'an 710072, China;
2. Military Representatives Office of Air Force, Shanghai 200233, China;
3. Dept. of Automatic Control, Northwestern Polytechnical University, Xi'an 710072, China

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Abstract�� To nonlinear system, the approximate reverse of the system was extracted using its approximate linearized model and the fuzzy control was employed to restrain the effect the error produces on the system so as to guarantee the terminal performance of the system, thus constituting a plan of dynamic reverse and fuzzy integrated control. This method was applied to the attitude control of unmanned helicopters and it can, in accordance with the simulation results, remove uncertain effects unmanned helicopters bring about, being provided with better robustness.
Keywords�� fuzzy control theory   attitude control   dynamic reverse   unmanned helicopter     
Received 2003-06-20;
About author: �� ��(1960-),��,��������,��ʿ��, yemonaduo@sohu.com.
����, ������, ���.����ֱ�����Ķ�̬��ģ�����ɿ���[J]  �������պ����ѧѧ��, 2003,V29(12): 1133-1135
Shen Yi, Yu Xiaomin, Li Aijun.Dynamic reverse and fuzzy integrated control of unmanned helicopters[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2003,V29(12): 1133-1135
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