DocumentCode :
1587457
Title :
Environmental adaptive yaw control autonomous unmannedhelicopter and bifurcation of maneuvering in turning
Author :
Nakanishi, Hiroaki ; Kanata, Sayaka ; Sawaragi, Tetsuo
Author_Institution :
Yoshida Honmachi, Kyoto Univ., Kyoto, Japan
fYear :
2010
Firstpage :
1
Lastpage :
6
Abstract :
Adaptation to the environmental changes, such as wind, has very important role to improve the reliability of an autonomous unmanned helicopter. In this paper, we propose an adaptive yaw (heading) control for an autonomous helicopter. The control structure is based on a hierarchal scheme utilizing an inner yaw feedback control loop plus an outer feedback loop, which estimates the direction of the airspeed using roll angle and roll angular rate. Stable coupling in yaw and roll motion is induced by the proposed controller to improve the stabitity of the helicopter´ flight. Turning utilizing the proposed adaptive control system is discussed in particular. Results of flight experiments showed bifurcation of the helicopter´s maneuvering in turning occurs depending on the airspeed.
Keywords :
helicopters; mobile robots; remotely operated vehicles; state feedback; autonomous helicopter control; autonomous unmanned helicopter; control structure; environmental adaptive yaw control autonomous unmanned helicopter; feedback control loop; helicopter flight; maneuvering bifurcation; roll angle; roll angular rate; Autonomous Unmanned Helicoptera; Bifurcation of Maneuvering; Environmental Adaptive Flight Control; Turing; Yaw control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
World Automation Congress (WAC), 2010
Conference_Location :
Kobe
ISSN :
2154-4824
Print_ISBN :
978-1-4244-9673-0
Electronic_ISBN :
2154-4824
Type :
conf
Filename :
5665345
Link To Document :
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