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�������պ����ѧѧ�� 2003, Vol. 29 Issue (12) :1101-1104    DOI:
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���, ������, ��ռ��, �߲�*
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Design and analysis of novel airborne integrated electro-hydrostatic actuator
Li Jun, Fu Yongling, Wang Zhanlin, Gao Bo*
School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

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Abstract�� To meet the development of aircraft actuating systems in the future, a novel airborne electro-hydrostatic actuator (EHA) which is integrated for power-by-wire (PBW) is designed. The paper describes the principle of work and features of EHA, models its components and the system, and simulates it with Matlab/Simulink. The EHA closed-loop system's simulation obtained the perfect dynamic performances; verify the correctness of the design with its control strategy. It will be used as a part of airborne PBW actuating system.
Keywords�� non-linear control systems   model building   simulation   Power-By-Wire (PBW)   aircraft actuating system   Electro-Hydrostatic Actuator (EHA)   performance analysis     
Received 2003-07-01;


About author: �� ��(1973-),��,����������,��ʿ��, journer@263.net.
���, ������, ��ռ��, �߲�.һ�����ͻ���һ�廯��Һ����������������[J]  �������պ����ѧѧ��, 2003,V29(12): 1101-1104
Li Jun, Fu Yongling, Wang Zhanlin, Gao Bo.Design and analysis of novel airborne integrated electro-hydrostatic actuator[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2003,V29(12): 1101-1104
http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2003/V29/I12/1101
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