Abstract
The article deals with basics of modeling of our small experimental turbojet engine MPM 20 and the following design of a complex situational control system with elements of anytime control algorithms bound with a developed analytical model of the engine. By use of advanced algorithms using methods of artificial intelligence in a robust framework to achieve the aims of reliability and high efficiency, we are trying demonstrate their usability and proficiency in the area of turbojet engines. All the tests and data come from measurements on a real object of our experimental small turbojet engine and are therefore a good step to be used on normal sized engines.
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