Abstract
In this article, a calculation model for a fuel system of a light helicopter was developed for experimental and operational testing. The model analyzes the operation of not only the units, but also the whole fuel system, offering the basis for functional tests and failure detection. For an actual model-based design, it is necessary to ensure that the model conforms to a real object or process. This article addressed the problems of ensuring the accuracy of the calculation and the computational speed when developing a reliable mathematical model of an actual technological system using structural modeling methods. A system with evaluation criteria allows complex field tests to be replaced with validated calculation models.
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