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�������պ����ѧѧ�� 2003, Vol. 29 Issue (11) :998-1000    DOI:
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Servo-elasticity test of an aircraft with the flight control system
Zhang Junjie, Yang Chao*
School of Aeronautics Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

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Abstract�� To discover the servo-elasticity stability nature of an aircraft equipped with a flight control system, some active-control-system/structural dynamics interaction tests on it have been performed. The test principle and test method was described. Some typical test results have been presented and compared with the calculated results. The test method is reasonable.
Keywords�� servo systems   test   stability     
Received 2003-07-05;
About author: �¿���(1961-),��,�㽭������,��ְ��ʿ��,�߼�����ʦ, yangchao@buaa.edu.cn.
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�¿���, �.���з��п���ϵͳ�ɻ����ŷ����������о�[J]  �������պ����ѧѧ��, 2003,V29(11): 998-1000
Zhang Junjie, Yang Chao.Servo-elasticity test of an aircraft with the flight control system[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2003,V29(11): 998-1000
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