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�������պ����ѧѧ�� 2003, Vol. 29 Issue (12) :1130-1132    DOI:
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Helicopter pitch fly-by-wire control law design based on fuzzy control
Huang Ying*
Flight Automatic Control Research Institute, Xi'an 710065, China

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Abstract�� Because of the nonlinear properties of the helicopters, such as multivariable, strong couple, the conventional control methods can hardly provide the perfect manipulability for advanced helicopter. Fuzzy control is an effect control method, which deals with the control problems through the way similar to human problems solving, so it can control some uncertain systems by imitating the fuzzy concepts of human thoughts. Fuzzy control method was applied to designing the pitch ACAH control law of hovering for a helicopter. The effectiveness of the proposed method was provided by simulation.
Keywords�� helicopters   fuzzy control theory   fly-by-wire     
Received 2003-06-20;
About author: �� ݺ(1974-),Ů,���ջ�����,����ʦ, yhuang@facri.com.
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��ݺ.����ģ�����Ƶ�ֱ��������紫���������[J]  �������պ����ѧѧ��, 2003,V29(12): 1130-1132
Huang Ying.Helicopter pitch fly-by-wire control law design based on fuzzy control[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2003,V29(12): 1130-1132
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