Abstract
The integration of an aircraft engine and an aircraft is such a combination of their structural forms, aerodynamic and propulsive-economic characteristics and control systems (including thrust vector), which provides an improvement in certain flight performance characteristics of the aircraft. A program structural service of multi-mode aircraft aviation engine integration has been considered. It can be effectively applied for ensuring adaptation to changing flight modes by determining the shape of an aircraft and its aviation engine, from one side, for determining the purpose of aircraft, its parameters and aviation engine parameters, as well as flight modes by correct choice of control laws, from another side. The considered technique and service, based on mathematical modeling of the AIRCRAFT-AVIATION ENGINE-FUEL system, in combination with the use of multiparameter optimization methods, is an effective tool for choosing design parameters and forming the technical appearance of an aviation engine.
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Tovkach, S. (2022). Middleware Service for the Integration of Control Systems of the Aviation Engine and Aircraft. In: Bieliatynskyi, A., Breskich, V. (eds) Safety in Aviation and Space Technologies. Lecture Notes in Mechanical Engineering. Springer, Cham. https://doi.org/10.1007/978-3-030-85057-9_2
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DOI: https://doi.org/10.1007/978-3-030-85057-9_2
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