高空长航时太阳能无人机总体设计要点分析
收稿日期: 2016-04-21
修回日期: 2016-08-26
网络出版日期: 2016-09-01
基金资助
中航工业技术创新基金
Essentials of configuration design of HALE solar-powered UAVs
Received date: 2016-04-21
Revised date: 2016-08-26
Online published: 2016-09-01
Supported by
Technology lnnovation Foundation of AVIC
张健 , 张德虎 . 高空长航时太阳能无人机总体设计要点分析[J]. 航空学报, 2016 , 37(S1) : 1 -7 . DOI: 10.7527/S1000-6893.2016.0244
There are significant differences between high altitude long endurance (HALE) solar-powered unmanned aerial vehicles (UAVs) and conventional propulsion aircrafts. The configuration method for HALE solar-powered UAV has its own peculiarity, and some critical technical details must be paid attention to during schematic design. The mechanism of the general design method based on weight balance and energy balance for the HALE solar-powered UAV is analyzed. Some important factors are summed up including the power needed for level flight, the styles of configuration of HALE solar-powered UAV, the optimization of flight profile, operating environment influence, etc. The conclusions may be referred to in the configuration design and scheme optimization of solar-powered UAV.
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