多旋翼无人机飞行续航力测量

Petr Žárský, J. Hub
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引用次数: 1

摘要

本文描述了目前商用多旋翼机的飞行耐力测量。续航力是该机最全面的参数之一,它受海拔高度、天气条件、飞行特性、载荷和能量容量等诸多因素的影响。根据在捷克共和国地区和阿富汗巴格拉姆空军基地对具有代表性的尤涅克台风H型六旋翼机进行的测量结果,对影响因素的理论说明进行了实际飞行试验。这些测量可以作为将来测量多旋翼飞机飞行性能的基础,这些飞机即将进入捷克陆军作战部队。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Flight Endurance Measurement of a Multicopter UAS
This article describes the flight endurance measurements of current commercially available multicopter. Endurance, as one of the most comprehensive parameter of this machine, is influenced by a number of factors as altitude, weather conditions, character of the flight, load and energy capacity. The theoretical description of influencing factors is complemented by practical flight tests, based on measurements on the representative Yuneec Typhoon H hexacopter carried out both in the Czech Republic region and at the Bagram Air Field (BAF) in Afghanistan. These measurements can be the basis for the future measurement of flight performances of multicopters, which are about to be introduced into the Czech Army operation service.
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