@inproceedings{4a2a58c734b4443c8eaf31a668c188c5,
title = "Analysis of technical characteristics of fixed-wing VTOL UAV",
abstract = "Fixed-Wing VTOL UAV has advantages of having less demand for landing space, high agility and high cruising speed compared with traditional air vehicle. It is one of the hotspots of aircraft's development. This paper described the development status of Fixed-Wing VTOL UAV and analyzed the technical characteristics of different types of Fixed-Wing VTOL UAV, prospected their development trends and put forward a feasible design plan of hybrid quadrotor UAV.",
keywords = "hybrid quadrotor, tail-sitter, tilt-rotor, UAV, VTOL",
author = "Ma Tielin and Yang Chuanguang and Gan Wenbiao and Xue Zihan and Zhang Qinling and Zhang Xiaoou",
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.2017.8278357",
language = "英语",
series = "Proceedings of 2017 IEEE International Conference on Unmanned Systems, ICUS 2017",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "293--297",
editor = "Xin Xu",
booktitle = "Proceedings of 2017 IEEE International Conference on Unmanned Systems, ICUS 2017",
address = "美国",
}