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无人机水下发射试验系统弹射性能的仿真研究
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Simulation Research on Ejection Performance of UAV Underwater Launch Test System
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    摘要:

    为研究无人机水下发射的可行性及其弹射过程动力学性能,对系统主要参数进行影响规律和灵敏度分析。通过研究机械结构和传动系统的耦合特性,建立基于AMESim和ADAMS的水下发射试验系统动力学联合仿真模型,在发射角10°~90°范围内对3种类型无人机进行仿真,得到发射速度随发射角和储气瓶压力的变化规律;利用局部灵敏度分析方法,对储气瓶压力、储气瓶容积、气缸有效面积和行程4个关键参数进行了影响发射速度和加速时间的规律分析。结果表明:在相同压力下,随着发射角的增大和无人机模型质量的减小,其脱离发射架的速度逐渐增大;影响发射速度灵敏度最大的参数为储气瓶压力,随着压力的增大,速度增大的幅度逐渐减小;影响加速过程时间灵敏度最大的参数为储气瓶压力和气缸有效面积。

    Abstract:

    In order to study the feasibility of underwater launch of UAV and its dynamics performance of ejection process,the influence law and sensitivity analysis of the main parameters of the system were carried out.By studying the coupling characteristics of the mechanical structure and transmission system,a dynamics joint simulation model of the underwater launch test system based on AMESim and ADAMS was established,and the simulation was carried out for three types of UAVs in the range of launch angle 10° to 90° to obtain the variation law of the launch speed with launch angle and gas cylinder pressure;using the local sensitivity analysis method,the four key parameters of cylinder pressure,cylinder volume,effective area and stroke were analyzed to influence the launch speed and acceleration time.The results show that under the same pressure,as the launch angle increases and the mass of the drone model decreases,the speed of its detachment from the launch platform gradually increases;the parameter that affects the launch speed sensitivity most is the cylinder pressure,and as the pressure increases,the amplitude of the speed increase gradually decreases;the parameters that affect the acceleration process time sensitivity most are the cylinder pressure and the effective area of the cylinder.

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引用本文

陈尚成.无人机水下发射试验系统弹射性能的仿真研究[J].机床与液压,2023,51(16):172-177.
CHEN Shangcheng. Simulation Research on Ejection Performance of UAV Underwater Launch Test System[J]. Machine Tool & Hydraulics,2023,51(16):172-177

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  • 在线发布日期: 2023-09-13
  • 出版日期: 2023-08-28