DocumentCode
2694617
Title
Robust control of an uncertain underactuated airship with asymptotic rejection against wind disturbance
Author
Yamada, Manabu ; Adachi, Hiroki ; Funahashi, Yasuyuki
Author_Institution
Res. Center for Nano Device & Syst., Nagoya Inst. of Technol., Nagoya, Japan
fYear
2010
fDate
8-10 Sept. 2010
Firstpage
1844
Lastpage
1849
Abstract
This paper considers the problem of controlling both the planar position and the orientation of an underactuated airship with a reduced number of actuators in the presence of a unknown persistent wind disturbance. The airship is a nonholonomic system described by a set of nonlinear equations and the dynamics are subjected to bounded uncertainties. A smooth and time-varying coordinate transformation is proposed to reduce the disturbance rejection problem of the airship to that of a simple linear time-invariant system. A new adaptive robust feedback controller provides global stabilization and asymptotical rejection against the unknown wind disturbance under the plant uncertainties. The proposed design method is simple and straightforward. Some flight simulations using a real blimp are performed to validate the effectiveness of the proposed controller.
Keywords
actuators; adaptive control; aerospace simulation; airships; asymptotic stability; control system synthesis; feedback; linear systems; nonlinear equations; robust control; time-varying systems; uncertain systems; wind; actuators; adaptive robust feedback controller; asymptotic rejection; asymptotical rejection; blimp; flight simulations; global stabilization; linear time-invariant system; nonholonomic system; nonlinear equations; orientation control; planar position control; robust control; time-varying coordinate transformation; uncertain underactuated airship; wind disturbance; Design methodology; Propellers; Robustness; Time varying systems; Trajectory; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications (CCA), 2010 IEEE International Conference on
Conference_Location
Yokohama
Print_ISBN
978-1-4244-5362-7
Electronic_ISBN
978-1-4244-5363-4
Type
conf
DOI
10.1109/CCA.2010.5611226
Filename
5611226
Link To Document