无人机探空仪自由抛射试验研究

Chen Yao, Xia Lianghua, G. Ran, Yan Linming, Chen Rui, Z. Yanping
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引用次数: 0

摘要

对高空长航时(HALE)无人机模型进行了探空仪自由抛射试验研究。根据动力相似原理设计了探空仪模型及其弹射机构。通过分析高速摄像机记录的探空仪轨迹和姿态,研究了不同条件对探空仪抛射的影响。实验结果表明,探空仪与无人机没有发生碰撞。飞行高度、马赫数和攻角对探空仪抛射的影响较小,而侧滑角对探空仪抛射的影响较大。
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Experimental Research of Sonde Free Jettison from UAV
Experimental research of sonde free jettison from a high altitude long endurance (HALE) unmanned air vehicle (UAV) model was carried out. The sonde model and its ejection mechanism were designed according to the principle of dynamic similarity. Influences of different conditions to the sonde jettison were studied by analyzing the sonde trajectory and attitude recorded by high speed cameras. Results show that the sonde doesn't collide with the UAV in the experiments. And the flight altitude, Mach number and angle of attack have little influences on the sonde jettison, but the angle of side-slip show great influence.
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