@inproceedings{bbf8c98657c54c83b4379efa86ba483a,
title = "Hybrid position-attitude control of DF-UAV based on generalized flight dynamics",
abstract = "For a ducted fan unmanned aerial vehicle (DF-UAV), the aerodynamic forces comprising the aerodynamic lift and drag as well as their induced angular moments are the real physical inputs dominating the flight state. These forces originate from the motions of the duct, propeller and control surfaces. Therefore, this study considered an integrated modeling of DF-UAV and proposed a layered design method for the hybrid position-attitude controller based on the reference feedback and dynamic decoupling.",
keywords = "Ducted fan, Dynamic decoupling, Flight dynamics, Layered design, Reference feedback",
author = "Hongzhe Jin and Yi Zheng and Qingming Hou and Jie Zhao",
note = "Publisher Copyright: {\textcopyright} 2013 IEEE.; 2013 International Conference on Mechatronic Sciences, Electric Engineering and Computer, MEC 2013 ; Conference date: 20-12-2013 Through 22-12-2013",
year = "2013",
doi = "10.1109/MEC.2013.6885082",
language = "英语",
series = "Proceedings - 2013 International Conference on Mechatronic Sciences, Electric Engineering and Computer, MEC 2013",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "277--281",
booktitle = "Proceedings - 2013 International Conference on Mechatronic Sciences, Electric Engineering and Computer, MEC 2013",
address = "美国",
}