DocumentCode :
1707101
Title :
Performance analysis of a small-scale unmanned helicopter under large wind disturbance
Author :
Zeng WenWu ; Zhu XiaoRui ; Li Yanjie ; Li Lei
Author_Institution :
State Key Lab. of Robot. & Syst. (HIT), Harbin, China
fYear :
2013
Firstpage :
1877
Lastpage :
1882
Abstract :
Large wind disturbance is harmful to the autonomous helicopters, especially to the small ones because of their low inertia and high cross-coupling effects among the multiple inputs. This paper has analyzed how the large wind disturbance would affect the performance of the small-scale unmanned autonomous helicopter (UAH) under the condition of hovering and forward flight. A group of polynomial functions were identified first according to the experiment data from the wind tunnel tests to estimate the variation of the total forces and moments caused by different large wind disturbances. Then, the wind resistance abilities of UAH are discussed based on further analysis of the wind tunnel experiment data. This paper has provided support to the controller design in order to attenuate large horizontal wind disturbances.
Keywords :
aerospace control; autonomous aerial vehicles; helicopters; polynomials; wind tunnels; UAH; autonomous helicopters; controller design; cross coupling effects; forward flight; hovering; large wind disturbance; performance analysis; polynomial functions; small scale unmanned autonomous helicopter; wind resistance; wind tunnel tests; Electronic mail; Force; Helicopters; Laboratories; Performance analysis; Robots; Wind speed; Unmanned Autonomous Helicopter (UAH); Wind Disturbance; Wind Tunnel Experiment;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2013 32nd Chinese
Conference_Location :
Xi´an
Type :
conf
Filename :
6639733
Link To Document :
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