Journal of Jianghan University (Natural Science Edition) ›› 2019, Vol. 47 ›› Issue (5): 430-435.doi: 10.16389/j.cnki.cn42-1737/n.2019.05.007
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LEI Anxu,FENG Bowen,DONG Chen,HU Jinxin
Published:
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
CLC Number:
V279
LEI Anxu,FENG Bowen,DONG Chen,HU Jinxin. Design of Aerial Take-off of Solar Unmanned Aerial Vehicle[J]. Journal of Jianghan University (Natural Science Edition), 2019, 47(5): 430-435.
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URL: https://qks.jhun.edu.cn/jhdx_zk/EN/10.16389/j.cnki.cn42-1737/n.2019.05.007
https://qks.jhun.edu.cn/jhdx_zk/EN/Y2019/V47/I5/430