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Modeling and Simulation of Hydraulic System in the Launch Equipment of UAV Based on AMESIM
Author(s): 
Pages: 16-18
Year: Issue:  9
Journal: Hydraulics Pneumatics & Seals

Keyword:  AMESIM插装阀;
Abstract: 无人机起飞弹射液压系统要求高压、高速、反应时间快,国内进行的相关研究比较少.本文分析了无人机起飞弹射液压系统的工作原理,对插装阀的结构进行了描述,运用AMESIM软件对液压系统进行建模与仿真.仿真结果表明该系统性能良好,能够在短时间内将无人机加速到规定的速度值,同时,该仿真结果也为液压系统的调试提供了参考依据.
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