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一种新型机载一体化电液作动器的设计与分析
Design and analysis of novel airborne integrated electro-hydrostatic actuator
【摘要】 针对近年来飞机机载作动系统的发展 ,设计了一种用于功率电传的新型一体化电动静液压作动器 (EHA) ,分析其原理和特点 ,讨论各部件和系统的建模方法 ,采用Matlab Simulink对其进行仿真 ,结果表明所设计的EHA具有良好的动态性能和带负载能力 ,达到了良好的性能指标 ,可作为未来飞机机载电作动系统的方案之一 ,对功率电传电液作动系统的研制具有实际指导意义 .
【Abstract】 To meet the development of aircraft actuating systems in the future, a novel air borne electro-hydrostatic actuator (EHA) which is integrated for power-by-wir e ( 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. Th e EHA closed-loop system’s simulation obtained the perfect dynamic performances ; verify the correctness of the design with its control strategy. It will be use d as a part of airborne PBW actuating system.
【Key words】 non-linear control systems; model building; simulati on; Power-By-Wire (PBW); aircraft actuating system; Electro-Hydrostatic Actu ator (EHA); performance analysis;
- 【文献出处】 北京航空航天大学学报 ,Journal of Beijing University of Aeronautics and Astronautics , 编辑部邮箱 ,2003年12期
- 【分类号】V243
- 【被引频次】55
- 【下载频次】1190