Research on Improving Take-Off Characteristics of Fly Wing with a New Constitution

Song Mo; Jun Huang; Xue Chai; Quan Zhao

doi:10.4028/www.scientific.net/AMR.462.265

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HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 462Research on Improving Take-Off Characteristics of...

Research on Improving Take-Off Characteristics of Fly Wing with a New Constitution

Abstract:

The take-off control of UAV with fly wing layout is limited by its relatively lower pitch moment. This paper gained the state parameters of a few groups of taking off model by means of numerical simulation. The influence of different models on take-off distance, take-off angle of attack (AOA), take-off safe speed and c.g. location was then analyzed. Based on the analysis, a new fly wing constitution was designed and the corresponding take-off control scheme was suggested as well. Finally, the flight test results shows that this fly wing constitution can gain better take-off control characteristics.

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Periodical:

Advanced Materials Research (Volume 462)

Pages:

265-270

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.462.265

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Online since:

February 2012

Authors:

Song Mo, Jun Huang, Xue Chai, Quan Zhao

Keywords:

Angle of Attack (AOA), Flight Test, Fly Wing, Take-Off

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