@inproceedings{3544f3370ca9487aa5e54a8c80cee356,
title = "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.",
keywords = "Angle of attack (AOA), Flight test, Fly wing, Take-off",
author = "Mo Song and Huang Jun and Chai Xue and Zhao Quan",
year = "2012",
doi = "10.4028/www.scientific.net/AMR.462.265",
language = "英语",
isbn = "9783037853610",
series = "Advanced Materials Research",
pages = "265--270",
booktitle = "Material Science and Engineering Technology",
note = "2011 International Conference on Material Science and Engineering Technology, ICMSET 2011 ; Conference date: 11-11-2011 Through 13-11-2011",
}