novtexmechМехатроника, автоматизация, управлениеMekhatronika, Avtomatizatsiya, Upravlenie1684-64272619-1253Commercial Publisher «New Technologies»10.17587/mau.21.656-662novtexmech-901Research ArticleДИНАМИКА, БАЛЛИСТИКА И УПРАВЛЕНИЕ ДВИЖЕНИЕМ ЛЕТАТЕЛЬНЫХ АППАРАТОВDYNAMICS, BALLISTICS AND CONTROL OF AIRCRAFTРазработка метода определения сигнала управления безопасностью полета воздушного суднаDevelopment of a Method for Computation of Aircraft Safety Control SignalКуликА. А.KulikA. A.

Кандидат технических наук

Москва

Moscow

kulikalekse@yandex.ruНИУ "МЭИ"РоссияMoscow Power UniversityRussian Federation2020041120202111656662Copyright © Commercial Publisher «New Technologies», 20202020Commercial Publisher «New Technologies»Commercial Publisher «New Technologies»https://mech.novtex.ru/jour/about/submissions#copyrightNoticehttps://mech.novtex.ru/jour/article/view/901

Рассматривается оптимальное управление безопасностью полета воздушного судна, на базе которого проводится определение сигнала парирования угрозы авиационного происшествия. В процессе анализа воздействующих на безопасность полета воздушного судна факторов выделены в отдельные группы психофизическое состояние экипажа, исправность бортового оборудования летательного аппарата и погодные условия полета. На основе выполненного анализа предложена целевая функция управления безопасностью полета воздушного судна в виде максимума оценки безопасности полета, который обеспечивается выходным сигналом системы управления безопасности полета судна. Определение сигнала управления осуществляется на базе графа состояния условий полета воздушного судна, который позволяет оценить причинно-следственную взаимосвязь факторов угрозы авиационного происшествия, а также определить сигнал управления безопасностью полета судна.

Полученные в процессе выполнения работы результаты могут быть использованы для программно-аппаратной реализации систем управления безопасностью полета воздушных судов, а также при проектировании систем и комплексов его бортового оборудования.

The optimal flight safety management of an aircraft is considered, on the basis of which the signal for parrying the threat of an aviation accident is calculated. In the process of analyzing the factors affecting the flight safety of the aircraft, the psychophysical state of the crew, the serviceability of the aircraft’s onboard equipment and the flight weather conditions are separated into separate groups. Based on the performed analysis, a target function of aircraft flight safety management is proposed in the form of a maximum, which is provided by the output signal of the aircraft flight safety management system. The calculation of the control signal is based on a count state of the flight conditions of the aircraft, which allows us to estimate the causal relationship of the factors of threat of the accident, and to determine the control signal with the safety of the vessel. In the course of this work, an algorithm for calculating the aircraft safety control signal has been developed. The results obtained during the work can be used for software and hardware implementation of aircraft flight safety management systems, as well as for the design of systems and complexes of its onboard equipment.

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The authors declare that there are no conflicts of interest present.