Variants construction tracking system for orientation angle plate polarization electromagnetic wave are considered.

The article discusses the use of joint polarization and robust signal processing algorithms.

This article discusses identifying functional critical items of aircraft electrical power and distribution system.

Analysis the procedure of multi-objective selection of conflict-free trajectories at aircraft conflict resolution was performed.

The principles of operation of radio range finding interrogation-reply system to provide navigational and landing operations of aircraft are considered. A precise method of measuring of time delays of signals for determining the location of aircraft with high accuracy is proposed.

The article is an analysis of operation of navigation systems of unmanned aerial vehicles (UAVs) in the high latitudes, considered the requirements of navigation and security drones impact of the environment on the UAV navigation equipment.

The concept of structuring of radio equipment, mathematical and algorithmic tools to provide computing operations for determining the location of aircraft in spatial configuration of mobile (portable) multipositioning radio rangefinding interrogation-reply navigation and landing system is considered in this article. The mathematical modeling of algorithms of aircraft traffic terminal control is carried out. The results of calculations of potential system performance and its analysis for compliance with international safety requirements are represented.

This article discusses new approaches to improve the efficiency procedure MSG-3, based on the account of external factors.

The article is an analysis of the use of artificial neural networks in problems of navigation of unmanned aerial vehicles operated at high latitudes.

The article discusses the selection of functionally important elements of the electronic equipment aircrafts.

The article considers the application of non-classical inductive logic to search for failure causes avionics equipment.

Technical operation of the aircraft and its avionics is investigated as a process with the succession of states of operation. The models of the processes and systems of technical operation of avionics in the form of stationary and non-stationary Markov chains of the first and higher order are proposed. There are examples of the processes for two states of operation - able to work and disabled states.

Mathematical models in the electrical parameters of physico-chemical processes in lithium-ion batteries are developed. The developed model parameters (discharge mode) are identified out of family of discharging curve. By using of the parameters of this model we get the numerically model of lithium-ion battery.

This article is devoted to math modeling of channel of alternate current airborne electrical power-supply system. Considered to modeling of synchronous generator that runs on three-phase static load.

Work is devoted to the development of information management system for maintenance and repair, using telecommunication technologies to ensure the completeness, accuracy, continuity and timeliness required in the maintenance and repair information.

National system of training of aircraft maintenance engineering staff and aviation electrical systems and avionics staff requires improvement and harmonization with international requirements. The article represents the analysis of these requirements and the ways of such harmonization. Introduction of competency-based approach will significantly improve the quality of training and ensure compliance with international practice.

In this article presented the main result of numerical investigation of ability to improve the aerodynamic perfection of modern combat training aircraft. To determine the aerodynamic characteristic was used the discrete vortex method with closed vortex frames. In the work was presented the algorithm of a deflection of mechanization of a wing for increase of aerodynamic quality of the aircraft. The calculation of flight range and duration was at incremental extension and at realization of adaptive deflection of nose flap for Mach number M < 0.6.