The paper is focused on optimal control algorithms design for mechanical dynamic system - laboratory helicopter model. The optimal control algorithms based on LQ principle (LQ control design with integral action) and the principle of receding strategy (model predictive control design) use model of the system in the state space. The algorithms of optimal control are verified by simulation schemes in language Matlab/Simulink using architecture of S-functions. The paper presents results of the tracking of reference trajectories by nonlinear helicopter model using LQG algorithm with integral action.
Optimal control design for laboratory helicopter model
Optimalregelungsentwurf für ein Hubschrauber-Labormodell
PC, International Conference on Process Control, 16 ; 124/1-124/8
2007
8 Seiten, 11 Bilder, 9 Quellen
Conference paper
Storage medium
English
Helicopter Modeling and Optimal Control in Autorotation
British Library Conference Proceedings | 2008
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