DocumentCode
2255425
Title
A vortex-ring-state-avoiding descending control strategy for multi-rotor UAVs
Author
Chenglong, Li ; Zhou, Fang ; Jiafang, Wang ; Xiang, Zhang
Author_Institution
School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027
fYear
2015
fDate
28-30 July 2015
Firstpage
4465
Lastpage
4471
Abstract
The vortex ring state (VRS) is a dangerous phenomenon that may typically arise in rotorcraft descent process. In VRS, the rotor will lose lift and get into a wobbling state. As a kind of rotorcraft, multi-rotor UAV(Unmanned Aerial Vehicle) also encounters the same problems in descending flight. So in this paper, we propose a VRS-avoiding control strategy for multi-rotor UAVs. The real phenomenon of multi-rotor in vortex ring state is described through experiments. Based on test data, a VRS alarm and recovery strategy is proposed for vertical landing. To meet the demand of rapid descending, a spiraling down control strategy is devised to make the multi-rotor avoid entering into the VRS based on Gao and Xin´s criterion. Using the developed simple model, this control strategy has been proved effective in hardware-in-loop simulation test, where larger than 4 m/s stable descending is realized.
Keywords
Aerodynamics; Aerospace control; Blades; Helicopters; Mathematical model; Rotors; Multi-rotor UAV; rapid descending control; vortex ring state;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2015 34th Chinese
Conference_Location
Hangzhou, China
Type
conf
DOI
10.1109/ChiCC.2015.7260330
Filename
7260330
Link To Document