An algorithm of formation of a conflicting situation for the Full Flight Simulator is described. The algorithm calculates the trajectory of the intruder that potentially can lead to the collision with "evading aircraft" - FFS. In case of near miss, traffic collision avoidance system (TCAS) triggers, after which the crew trains collision avoidance techniques.

The article deals with the problems of the simulator training of the crew of civil aviation. It is noted that the particular attention of the simulator training is paid to practising flying skills, though more complex activity remains out of the sphere of the estimation of the results of training.

This article considers the problem of assessment of data authenticity related to reliability of the flight data obtained in processing the information of portable GPS receivers’ during air accident investigations, which are characterized by the lack of standard flight data recording systems. Appropriate recommendations the improvement improving of the newly developed GPS receivers have been developed and implemented.

Investigation of the impact of aircraft noise on the population in the vicinity of the «Elizovo» airport. In the article investigates the impact of aircraft noise on people living near the population in the vicinity of the «Elizovo» airport. Different diseases obtained from noise exposure. The article have been analyzed provides methods and equipment which are used to measure and analyze the results. Inconclusion, the preliminary results obtained in the course of scientific research are cited.

The new dual methodology of expert estimation of the parameters of intermediate events tree in the development of aviation event / incident is elaborated in the article on the basis of logical and probabilistic model that combines the advantages of both widely used methods FMEA and FTA [1].

The article deals with the role of the maintenance personnel in the safety of flights. Statistical data and the reasons of wrong actions of the maintenance personnel are presented. The reasons of wrong actions of the personnel are analysed within the interrelation of personal and human factors.

The article continues a series of publications devoted to research of risk management problem of production environment during aeronautical equipment ground servicing to prevent non-routine situations in civil aviation. This article deals with formation of dynamic system environment factors of aircraft preparation for flight. As accumulation of risks from flight to flight occurs discretely, for mathematical formalization of the system of dynamic state the model is developed on the basis of discrete maps. The simplest stationary regimes and their stability have been studied. The possibility of system ambiguous behavior is considered.

The article deals with topical issues of development, introduction to businesses of aviation industry the experimental setup and test methods to determine the thermal stability of composites based on carbon materials (carbon fiber, matrix), which are the main structural material of heat-stressed components of aircraft engines of new generation. The article describes the ways of solving these problems.

The article describes the urgent problems which can arise at enterprises of aviation industries by the operating air during non-destructive damage control of products made of composite materials used in aircraft. The methods of control are very specific due to have a number of peculiarities in detecting damages in view of the complicated composite materials structure.

This paper investigates the problem of assessment of the vulnerability of transport infrastructure and means of transport as applied to civil aviation. The specific character of civil aviation is taken into account. An approached to vulnerability assessment, based on the concept of quality is offered. Show the interdependency of the concepts of vulnerability and quality is shown.

The article provides methodologies of decision-making when the designing the process of aviation equipment. Repair the standard diagram of decision making is presented. The basic directions of research and estimation of the system quality are offered.

This article describes the current condition of the onboard braking systems while rolling and the approach to the construction of the aircraft automatic braking system. The article analysis the main reasons for RW overrun and measures of reducing the risk.

The article describes aspects of some types of adaptations in different working conditions of modern extrimal production and possible consequences of work under specific conditions manufactures are shined. Possible tactics of adaptive behavior are presented and various ways of people behavior of working in different conditions are developed.

A methodology of calculation and trade of pollutants to form a united market of free allowances is being developed in the framework of reducing emissions of greenhouse gases from aircraft. The competences of the European Union in trading emissions trading quota have been determined. The ways of creating the system of greenhouse gases accounting offered by foreign countries were considered. The date of creating our own methodology of collating the data of pollutants from aircraft has been set.

The paper covers the problem how to control flight crew training on simulators to ensure the fulfillment requirements for the quality of their activity in training non-standard situations which can happen in flight. It is shown that the existing methodology of training pilots on simulators does not ensure the quality of their activity in those non-standard situations. The paper puts forward an adaptive control method (АМC-method) of the simulator training of flight crews using mathematical modeling the states of their operator competences. The main advantage of the new method is the possibility to obtain statistical quality indicators of flight crew activity in non-standard situations and, thereby, to control the fulfillment of prescribed requirements for safety and reliability of space missions.

The article deals with wavelet analysis of signals received from the sensors of electronic control systems of aircraft gas turbine engines, which will significantly improve the diagnostics of engine operating condition to prevent failure and ultimately to reduce the economic costs. A block diagram of automatic control of aircraft gas turbine engine is presented.

The article offers direct use of the recommendations of SMM ICAO Doc.9859, 3rd ed. 2013, for calculation the target and alert levels of safety indicators. Examples of calculation based on data of 2011 and monitoring of the current indicators during 2012 are presented. Safety indicators for airlines in terms of “numbers of incidents per 1000 flight hours” could be calculated on the basis of the state values through the «coefficient of conformity».

The article deals with the problem of providing an assessment of pilots training for work the airlines in order to ensure flight safety. In this regard, a draft comprehensive methodology for assessing professional training of pilots is offered. It is divided into three stages: 1) introduction into profession; 2) active flight activity and stage in improving professional of skills in case of incidents or accidents in flight.

This article considers the problems related to the reliability of aircraft and aircraft systems under the operating conditions of the North, Siberia and the Arctic, as well as the influence of the extremely low outside air temperatures on the operation of the Russian- and Western-built aircraft systems and components. Recommendations are given, which should be taken into account for the long-term location of the aircraft in the regions mentioned above

The article covers the problem of understanding of risk assessment necessity connected with aircraft production in accordance with Minimum Equipment List (MEL). The article presents calculation of fail-safe performance probability of Airbus A320 Family fuel system in the event of defect which rectification is postponed in accordance with MEL. The article also presents the results of risk assessment connected with aircraft production in accordance with MEL.

The article covers the problem of understanding of hazard identification necessity by using Minimum Equipment List (MEL) in civil aviation of the Russian Federation. The examples of hazards by using MEL are given in the article. It is also pointed out the seriousness of the consequences associated with the hazards and necessity of subsequent risk assessment.

The article deals with the issues of self-organization in small groups for example, personnel of industry and transport enterprises, including aviation and aircraft crew. Van der Pol non-linear dissipative oscillator is the basis of interaction in a small group model. The model describes interaction between the group members through synchronization of oscillators, which allows to take into account interaction, and counteraction, and coexistence of two types of interactions as the complex nature of unity and struggle of opposites for a selected center of interaction as a compulsory attribute of a small group.

Let M be Riemannian manifold with boundary and a diffeomorphism of . We consider the problem of the extension of from the boundary into the manifold to the volume-preserving diffeomorphism . The design of an explicit extension based on the representation theory is offered for the case of the sphere. We also extend the conformal and projective groups with the -sphere into the -ball. As a result, we construct examples of kinematic dynamo in the -ball.

The asymptotic behavior of solutions of the Burgers equation and its generalizations with initial value - boundary problem on a finite interval with constant boundary conditions is studied. Since the equation describes the movement in a dissipative medium, the initial profile of the solution will evolve to an time-invariant solution with the same boundary values. However there are three ways of obtaining the same result: the initial profile may regularly decay to the smooth invariant solution; or a Heaviside-type gap develops through a dispersive shock and multi-oscillations; or an asymptotic limit is a stationary ’sawtooth’ solution with periodical breaks of derivative.