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Design and Analysis of Aircraft Landing Gear Door Load Control System
Pages: 30-32
Year: Issue:  2
Journal: Hydraulics Pneumatics & Seals

Keyword:  加载多余力前馈补偿器AMESim;
Abstract: 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.
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