@inproceedings{4c56e139a4a74c3d8a230121c66795c2,
title = "Mode-transition control law design for aircraft with ability of VTOL and high-speed cruise flight",
abstract = "The considered aircraft can provide an economical combination of vertical takeoff and landing (VTOL) capability with efficient high-speed cruise flight. The sliding mode control laws are proposed in this paper for flight path tracking and attitude control to achieve the mode transition. Besides, a control allocation algorithm based on the sliding mode control law is designed. The design overcomes the defect of the original mode-transition algorithm which is sensitive to the noise. By using this design, the aircraft can achieve the mode-transition and path tracking under measurement noise which is reasonable. The efficiency of this mode-transition control law is verified by simulations.",
keywords = "High-speed cruise flight, Mode-transition, Noise-reduction, Sliding mode control, VTOL",
author = "Chenxi Zhang and Penghui Fan and Xinhua Wang and Kaiyuan Cai",
year = "2010",
language = "英语",
isbn = "9787894631046",
series = "Proceedings of the 29th Chinese Control Conference, CCC'10",
pages = "3284--3289",
booktitle = "Proceedings of the 29th Chinese Control Conference, CCC'10",
note = "29th Chinese Control Conference, CCC'10 ; Conference date: 29-07-2010 Through 31-07-2010",
}