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Abstract
This paper focuses on the practical problems of gas turbine engine local-optimal multi-variable control design and implementation. An algorithm for real-time resolution of the optimization problem is proposed for the non-linear optimal control design of the engine. The example of the turbo-jet engine multi-variable control presented shows that the method developed is highly efficient.
Acknowledgements
The authors wish to acknowledge the support of the EU INTAS programme under the INTAS-2000-757 project.