@inproceedings{bc946795dda446ad9bf056ad10048b16,
title = "Hover Control of New type ducted aircraft",
abstract = "In this paper, a new type of foldable winged unmanned aerial vehicle is designed, and the structure of the aircraft is analyzed. The dynamic model is established and an improved sliding mode control algorithm is used to control the attitude of the aircraft. In addition, a centroid position control method using attitude compensation is designed for the coupling characteristics of this aircraft. The simulation proves that the attitude and position of the new aircraft can be effectively controlled.",
keywords = "ducted aircraft, hover control, sliding mode control",
author = "Peijun Liu and Hongbin Deng and Shikun Wang and Kewei Li and Yiran Wei",
note = "Publisher Copyright: {\textcopyright} 2019 IEEE.; 2019 IEEE International Conference on Unmanned Systems, ICUS 2019 ; Conference date: 17-10-2019 Through 19-10-2019",
year = "2019",
month = oct,
doi = "10.1109/ICUS48101.2019.8995931",
language = "English",
series = "Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "109--113",
booktitle = "Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019",
address = "United States",
}