@inproceedings{c6d26c25353b426baffaa7cea57165e6,
title = "Design of a lift-propulsion VTOL UAV system",
abstract = "In this paper, a general design method for lift-propulsion vertical take-off and landing unmanned aerial vehicle (VTOL UAV) is proposed. The power matching based conceptual parameter estimation and aerodynamic shape design are carried out. The attitude control law is designed. The hovering and level flight test of the prototype are carried out. Confirming the validity of the overall design method and the attitude control law design.",
keywords = "Conceptual design method炻attitude control rate, Lift-propulsion, VTOL UAV",
author = "Xin Zhao and Zhou Zhou and Xiaoping Zhu",
note = "Publisher Copyright: {\textcopyright} 2018 IEEE.; 15th IEEE International Conference on Mechatronics and Automation, ICMA 2018 ; Conference date: 05-08-2018 Through 08-08-2018",
year = "2018",
month = oct,
day = "5",
doi = "10.1109/ICMA.2018.8484448",
language = "英语",
series = "Proceedings of 2018 IEEE International Conference on Mechatronics and Automation, ICMA 2018",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "1908--1913",
booktitle = "Proceedings of 2018 IEEE International Conference on Mechatronics and Automation, ICMA 2018",
}