摘要
基于控制理论建立了飞机操纵系统中液压助力器的数学模型,运用Simulink对模型进行了动态仿真,分析了液压助力器的动态特性,这将对液压助力器的设计、制造和使用有一定的参考价值。
The model of hydraulic booster for mechanical control system of airplane was founded according to hydraulic transmission and control theories. The dynamic simulation of the model was carried out by Simulink and the dynamic characteristic of the hydraulic booster was analyzed.
出处
《机床与液压》
北大核心
2007年第9期222-223,共2页
Machine Tool & Hydraulics
