DocumentCode
1158957
Title
Robust nonlinear motion control of a helicopter
Author
Isidori, Alberto ; Marconi, Lorenzo ; Serrani, Andrea
Author_Institution
Dipt. di Informatica e Sistemistica, Univ. di Roma "La Sapienza", Rome, Italy
Volume
48
Issue
3
fYear
2003
fDate
3/1/2003 12:00:00 AM
Firstpage
413
Lastpage
426
Abstract
We consider the problem of controlling the vertical motion of a nonlinear model of a helicopter, while stabilizing the lateral and horizontal position and maintaining a constant attitude. The reference to be tracked is given by a sum of a constant and a fixed number of sinusoidal signals, and it is assumed not to be available to the controller. This represents a possible situation in which the controller is required to synchronize the vehicle motion with that of an oscillating platform, such as the deck of a ship in high seas. We design a nonlinear controller which combines recent results on nonlinear adaptive output regulations and robust stabilization of systems in feedforward form by means of saturated controls. Simulation results show the effectiveness of the method and its ability to cope with uncertainties on the plant and actuator model.
Keywords
adaptive control; aircraft control; attitude control; control system synthesis; feedforward; helicopters; nonlinear control systems; robust control; constant attitude maintenance; feedforward systems; helicopter; horizontal position stabilization; lateral position stabilization; nonlinear adaptive output regulations; nonlinear controller design; oscillating platform; robust nonlinear motion control; robust stabilization; saturated controls; ship deck; uncertainties; vehicle motion synchronization; vertical motion control; Adaptive control; Attitude control; Control systems; Helicopters; Marine vehicles; Motion control; Nonlinear control systems; Programmable control; Robust control; Uncertainty;
fLanguage
English
Journal_Title
Automatic Control, IEEE Transactions on
Publisher
ieee
ISSN
0018-9286
Type
jour
DOI
10.1109/TAC.2003.809147
Filename
1184895
Link To Document