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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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ժҪ ��Խ������ɻ���������ϵͳ�ķ�չ,�����һ�����ڹ��ʵ紫������һ�廯�綯��Һѹ������(EHA) ,������ԭ����ص�,���۸�������ϵͳ�Ľ�ģ����,����Matlab/Simulink������з���,�����������Ƶ�EHA�������õĶ�̬���ܺʹ���������,�ﵽ�����õ�����ָ��,����Ϊδ���ɻ����ص�����ϵͳ�ķ���֮һ,�Թ��ʵ紫��Һ����ϵͳ�����ƾ���ʵ��ָ������.
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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;
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�ߵ�ѧУ��ʿ��ѧ��ר����л���������Ŀ(20020006006)

About author: �� ��(1973-),��,����������,��ʿ��, journer@263.net.
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���, ������, ��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
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