DocumentCode
2846503
Title
On the linear control of the quad-rotor system
Author
Sira-Ramirez, Hebertt
Author_Institution
Dept. de Ing. Electr., Cinvestav-IPN, Mexico City, Mexico
fYear
2011
fDate
June 29 2011-July 1 2011
Firstpage
3178
Lastpage
3183
Abstract
In this article, a robust linear output feedback control scheme is proposed for the efficient regulation, and trajectory tracking tasks, in the nonlinear, multivariable, quad-rotor system model. The proposed linear feedback scheme is based on the use of a classical linear feedback controllers and suitably extended, high gain, linear Generalized Proportional Integral (GPI) observers; aiding the linear feedback controllers in two important tasks: 1) accurate estimation of the input-output system model nonlinearities, 2) accurate estimation of the unmeasured phase variables associated with the flat, or linearizing, output variables. These two key pieces of information are used in the proposed feedback controller in a) approximate, yet close, cancelation, as a lumped unstructured time-varying term, of the influence of the highly coupled nonlinearities and b) devising proper linear output feedback control laws based on the approximate estimates of the string of phase variables associated with the flat outputs simultaneously provided by the disturbance observers.
Keywords
PI control; feedback; helicopters; linear systems; machine control; multivariable control systems; nonlinear control systems; observers; regulation; robust control; rotors; time-varying systems; trajectory control; GPI observers; efficient regulation; generalized proportional integral observers; multivariable system; nonlinear system; quad-rotor system; robust linear output feedback control; time-varying term; trajectory tracking; Adaptive control; Additives; Observers; Polynomials; Trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference (ACC), 2011
Conference_Location
San Francisco, CA
ISSN
0743-1619
Print_ISBN
978-1-4577-0080-4
Type
conf
DOI
10.1109/ACC.2011.5990771
Filename
5990771
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