@inproceedings{9e679d150e6f426f8205761abb16f066,
title = "Development of the AMT in yawing control of flying wing UAVs",
abstract = "This paper focus the property and application on an innovative yawing control effector for unmanned aerial vehicles (UAV) named all moving wing tips (AMT). The prospective application area of AMT is flying wing and other kind of stealth fighters. In terms of performance, it has a linearly drag output through a deflection from 20° to 60°, which is friendly to control methodology, and the yawing control efficiency is at a same order of magnitude with the traditional rudder. The AMT has a good prospect of application on future UAVs.",
keywords = "UAV, all moving wing tip, flying wing, yawing control",
author = "Dawei Bie and Wenbiao Gan and Tielin Ma and Qinling Zhang and Xiaoou Zhang",
note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 2017 IEEE International Conference on Unmanned Systems, ICUS 2017 ; Conference date: 27-10-2017 Through 29-10-2017",
year = "2017",
month = jul,
day = "2",
doi = "10.1109/ICUS.2017.8278378",
language = "英语",
series = "Proceedings of 2017 IEEE International Conference on Unmanned Systems, ICUS 2017",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "404--406",
editor = "Xin Xu",
booktitle = "Proceedings of 2017 IEEE International Conference on Unmanned Systems, ICUS 2017",
address = "美国",
}