JACIII Vol.12 No.2 pp. 198-205
doi: 10.20965/jaciii.2008.p0198


State Dependant Anytime Control Methodology for Non-Linear Systems

Annamária R. Várkonyi-Kóczy

Dept. of Measurement and Information Systems, Budapest University of Technology and Economics, Magyar tudósok körútja 2. H-1521 Budapest, Hungary

September 7, 2007
November 7, 2007
March 20, 2008
nonlinear control, anytime systems, multiple models, parallel distributed compensation, aeroelastic wing section
Nowadays in solving control problems the processing is performed typically by model-based computer systems, which contain a representation of our knowledge about the nature and the actual circumstances of the problem in hand. If the nature and/or the actual circumstances change, the corresponding model should also be changed. Anytime techniques are very flexible in this respect and can advantageously be used when the operation should be performed under changing circumstances. In this paper, a nonlinear state dependant control methodology is proposed for anytime use and as an example is applied to globally stabilize a given prototypical aeroelastic wing section via one control surface.
Cite this article as:
A. Várkonyi-Kóczy, “State Dependant Anytime Control Methodology for Non-Linear Systems,” J. Adv. Comput. Intell. Intell. Inform., Vol.12 No.2, pp. 198-205, 2008.
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