Кафедра електричної та енергомашинобудавання
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Відповідальна за розділ: Тимошенко Наталія Анатоліївна, доцент кафедри електричної та енергомашинобудавання. E-mail: n.tymoshenko@nau.edu.ua
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Browsing Кафедра електричної та енергомашинобудавання by Subject "aircraft"
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Item Automated identification system baseds on the changing of the temperature field of aircraft elements(National Aviation University, 2013) Шевчук, Д.О.In this article, system of identification collisions (structural damage) in the air, based on the change of the temperature field was given. Identification system provides information about type and size of aircraft damage to all systems during recovering the controllability of the aircraft when an unexpected problem occurs during a flight is proposedItem Intelligent Control System Against Aircraft’s Structural Damage in the Flight(IEEE 4th International Conference «Methods and Systems of Navigation and Motion Control» Conference Proceedings, 18-20 October 2016, Kyiv, Ukraine. – Р. 241-244., 2016) Shevchuk, D; Tymoshenko, NIn this paper, intelligent flight control system for recovering controllability of the aircraft when an unexpected problem (such as faults or failures to the actuators/sensors or structural damage) occurs during a flight is proposed.Item Thermal fields diagnostic method of changing aircraft aerodynamic state in flight(Electronics and control system. – 4(54). – 2017. - 40- 45 p., 2017) Shevchuk, D.O.; Kravchuk, M.P.; Shulevka, V.V.; Panchuk, L.V.A result of the research was the method of aerodynamic condition of the aircraft on the thermal fields. Based on the mathematical and natural experiments, regularities of formation of temperature gradients in the boundary layer of air that occurs when damage to the contours detected parameters that affect the behavior of the temperature gradient arising from damage, namely the speed and angle of attack of the aircraft, the shape of the profile wings, nature of damage, place of occurrence of damage relative to the outer contours.