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�������պ����ѧѧ�� 2003, Vol. 29 Issue (12) :1059-1063    DOI:
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Design of longitudinal automatic landing control law of transport aircraft with μ synthesis
Wang Hui, Li Shaoyan, Chen Zongji*
School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

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Abstract�� The process and characteristic of landing of transport aircraft was analyzed. The synthesis method based on structured singular value was adopted to design the automatic landing control system to accurately follow the slide path of landing. The robust performance of the landing system was analyzed. The simulation results showed that the designed control law satisfied the requirements of automatic landing of transport aircraft when there are uncertainties of transport aircraft model, measurement noises and gust disturbances.
Keywords�� automatic landing   robust control   flight control   &mu   synthesis   robust performance analysis     
Received 2003-06-20;


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Wang Hui, Li Shaoyan, Chen Zongji.Design of longitudinal automatic landing control law of transport aircraft with μ synthesis[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2003,V29(12): 1059-1063
http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2003/V29/I12/1059
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