DocumentCode :
2611801
Title :
Non-linear predictive control of 2 DOF helicopter model
Author :
Dutka, Arkadiusz S. ; Ordys, Andrzej W. ; Grimble, Michael J.
Author_Institution :
Ind. Control Centre, Strathclyde Univ., Glasgow, UK
Volume :
4
fYear :
2003
fDate :
9-12 Dec. 2003
Firstpage :
3954
Abstract :
This paper presents the application of non-linear predictive control algorithm to a helicopter model. First, the model of the helicopter is discussed. Next, the nonlinear algorithm is introduced which is based on state-space GPC controller. The non-linearity is handled by converting the state-dependent state-space representation into the linear time-varying representation. The predictions of the future controls are used to calculate predictions of the future states and of the future time varying system parameters. Applied to the helicopter model, the algorithm performs well. It is capable of the stabilizing the system for maneuvers for which it´s linear counterpart fails.
Keywords :
aircraft control; helicopters; nonlinear control systems; predictive control; state-space methods; time-varying systems; 2 DOF helicopter model; 2 degrees of freedom; general predictive control; linear time varying representation; nonlinear algorithm; nonlinear predictive control; nonlinearity; state dependent state space representation; state space GPC controller; time varying system parameters; Control systems; Helicopters; Industrial control; Optimal control; Petrochemicals; Prediction algorithms; Predictive control; Predictive models; Stability; Time varying systems;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 2003. Proceedings. 42nd IEEE Conference on
ISSN :
0191-2216
Print_ISBN :
0-7803-7924-1
Type :
conf
DOI :
10.1109/CDC.2003.1271768
Filename :
1271768
Link To Document :
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