Keyword: «flight safety»

This article discusses ways to improve the assessment of the technical condition of the automatic flight control system according to the data of the flight recorder in order to improve flight safety, combat readiness and reliability of control.

The article presents the results of theoretical and practical research aimed at the development of an electronic educational and methodological complex of the discipline Flight safety. The didactic model is substantiated, in which the electronic educational and methodological complex occupies a central place. The structure of the electronic educational and methodical complex is presented.

The article presents the results of theoretical research aimed at the formation of students' competencies in the field of flight safety. The proposals for making changes to the curriculum are substantiated. The structural and logical scheme of the order and sequence of the study of disciplines is presented.

The article discusses the main factors and psychophysiological features of flight work during the operation of modern helicopters in order to organize effective combat use, ensure flight safety and preserve the professional health of flight personnel.

The article presents the materials of the work carried out, the purpose of which is to identify and substantiate the energy indicators that characterize the energy state of the aircraft. A theoretical analysis of the scientific literature of domestic and foreign authors devoted to the energy approach in the implementation of aircraft control tasks and the development of crew warning systems about exceeding flight parameters is carried out.