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,分析了液压助力器的动态特性并对其在整个操纵系统的建模中的降阶简化做了简要分析,并运用Simulink进行仿真,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.Modeling of reduced-order in the control system was analyzed.The dynamic simulation of the model was carried out by Simulink and the dynamic characteristic of the hydraulic booster was analyzed.
出处
《价值工程》
2012年第14期27-28,共2页
Value Engineering
