DocumentCode
2460810
Title
L1 adaptive control for autonomous rotorcraft
Author
Guerreiro, B.J. ; Silvestre, C. ; Cunha, R. ; Cao, C. ; Hovakimyan, N.
Author_Institution
Inst. for Syst. & Robot., Inst. Super. Tecnico, Lisbon, Portugal
fYear
2009
fDate
10-12 June 2009
Firstpage
3250
Lastpage
3255
Abstract
In this paper, the L1 adaptive control theory is used to design a high bandwidth inner loop controller to provide attitude and velocity stabilization of an autonomous small-scale rotorcraft in the presence of wind disturbances. The nonlinear model of the vehicle is expressed as a linear time-varying system for a predefined region of operation, for which an L1 adaptive controller is designed. The L1 adaptive controller ensures that an uncertain linear time-varying system has uniformly bounded transient response for system´s input and output signals, in addition to stable tracking. The performance bounds of L1 adaptive controller can be systematically improved by increasing the adaptation rate without hurting the robustness of the system. The performance achieved with the L1 controller is compared with that obtained via a linear state feedback controller for demanding reference signals in the presence of wind disturbances. Simulation results show that the performance of the L1 surpasses that of the linear controller illustrating the advantages of fast adaptation.
Keywords
adaptive control; attitude control; helicopters; linear systems; stability; state feedback; time-varying systems; velocity control; L1 adaptive control; attitude stabilization; autonomous rotorcraft; inner loop controller; linear state feedback; linear time-varying system; velocity stabilization; Adaptive control; Attitude control; Bandwidth; Control systems; Linear feedback control systems; Nonlinear control systems; Programmable control; Remotely operated vehicles; Time varying systems; Velocity control;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2009. ACC '09.
Conference_Location
St. Louis, MO
ISSN
0743-1619
Print_ISBN
978-1-4244-4523-3
Electronic_ISBN
0743-1619
Type
conf
DOI
10.1109/ACC.2009.5159940
Filename
5159940
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