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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。
Based on the control theory, the mathematical model of the hydraulic booster in the aircraft control system is established. The dynamic characteristics of the hydraulic booster are analyzed and its reduction in the overall modeling of the control system is analyzed briefly. Simulink is used to simulate the hydraulic booster. This will be hydraulic booster design, manufacture and use of a certain reference value.