江汉大学学报(自然科学版) ›› 2019, Vol. 47 ›› Issue (5): 430-435.doi: 10.16389/j.cnki.cn42-1737/n.2019.05.007

• 自动化及控制系统 • 上一篇    下一篇

太阳能无人机空中起飞设计

雷安旭,冯博文,董琛,胡锦欣   

  1. 江汉大学 物理与信息工程学院,湖北 武汉 430056
  • 发布日期:2019-10-08
  • 作者简介:雷安旭(1987—),男,实验师,硕士,研究方向:航空器、无人机的飞行控制和电工电子实验教学。

Design of Aerial Take-off of Solar Unmanned Aerial Vehicle

LEI Anxu,FENG Bowen,DONG Chen,HU Jinxin   

  1. School of Physics and Information Engineering,Jianghan University,Wuhan 430056,Hubei,China
  • Published:2019-10-08

摘要: 通常情况下,太阳能无人机从地面起飞需要消耗大量能量,必须携带质量较大的电池组,很大程度上降低了无人机的续航能力。基于此设计了无人机空中起飞系统,该系统由地面控制台、升空动力模块、传感器模块、空中定位及位置保持模块、起飞弹射系统和空中滑跑辅助系统组成。通过理论推导构建物理模型,对比了空中起飞和地面起飞的能量消耗,从而得出无人机空中起飞的方案。

关键词: 太阳能无人机, 空中起飞跑道, 浮空器, 能量消耗

Abstract: Usually,ground take-off of solar unmanned aerial vehicle(UAV)will consume plenty of energy,so it has to carry batteries of higher mass,which greatly reduces the UAV′ s endurance capability. Based on this ,the author designed a new aerial take-off system of UAV ,the system consisted of ground console,lift-off power module,sensor module,spatial positioning and position holding module,take-off ejection system and aerial taxiing assistant system. The physical model was built through theoretical deduction,the energy consumptions of aerial take-off and ground take-off were compared by simulation calculation,thus the superior scheme of UAV aerial take-off was obtained.

Key words: solar unmanned aerial vehicle, aerial take-off runway, aerostat, energy consumption

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