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无人机气动弹射系统弹射性能的仿真研究 被引量:6

Simulation Research on Launch Performance of UAV Pneumatic Launch System
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摘要 以贮气罐作为动力源、滑轮组作为增速机构的无人机气动弹射系统为研究对象,介绍了系统弹射过程的工作原理,基于键合图法推导出了系统的数学模型,并利用MATLAB软件建立了系统的仿真模型.通过对系统的不同设计参数进行仿真研究,得到了这些参数对系统弹射性能的影响规律,合理匹配这些参数,既可以优化系统的弹射性能,也为系统的研发与改进提供了理论的指导. This paper introduces the working principle of an Unmanned Aerial Vehicle (UAV) pneumatic launch system, which takes an air tank as power supply and a pulley block as growth mechanism. The mathe- matical model of the system is deduced by using the bond graph method. And the simulation model is estab- lished by using MATLAB. Through adjusting the design parameters of the system, the influence of these pa- rameters on the launch performance is obtained. The haunch performance can be optimized by reasonable matc- hing of these parameters, which provides the theoretical guidance for this system.
出处 《郑州大学学报(工学版)》 CAS 北大核心 2013年第5期56-58,共3页 Journal of Zhengzhou University(Engineering Science)
关键词 气动弹射系统 键合图 数学模型 仿真模型 弹射性能 pneumatic launch system bond graph mathematical model simulation model launch performance
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