摘要
该文为某型飞机起落架舱门气动力地面模拟实验设计了一套加载控制系统,针对被加载对象运动干扰产生的多余力,设计了前馈干扰补偿器,有效地减小了多余力,在AMESim中对舱门加载控制系统模型进行了仿真,并对结果进行了分析。
This paper design a set of load control system of a certain type of aircraft landing gear door aerodynamic ground simulation test. To effectively reduce the additional force generated by the movement interference of the landing gear door, this paper design a feedforward disturbance compensator, simulate the model in AMESim, analyzed the results.
出处
《液压气动与密封》
2013年第2期30-32,共3页
Hydraulics Pneumatics & Seals
关键词
加载
多余力
前馈补偿器
AMESIM
load control
additional force
feedforward compensator
AMESim
