DEVELOPMENT AND MODERNIZATION PRINCIPLES OF AIRCRAFT DIGITAL ROUND/AIR COMMUNICATIONS ARCHITECTURE

Abstract. In this paper are analyses the types and development principles of aircraft air/groundcommunication architecture, which is used for acquiring, conditioning and processing all required aircraftparameters, collected from the aircraft and data, receives on low and high speed ARINC 429 buses. The paper also considers the possibility of receiving and sending data via ARINC 618 […]

DEVELOPMENT AND MODERNIZATION PRINCIPLES OF AIRCRAFT DIGITALGROUND/AIR COMMUNICATIONS ARCHITECTURE

Abstract. In this paper are analyses the types and development principles of aircraft air/groundcommunication architecture, which is used for acquiring, conditioning and processing all required aircraftparameters, collected from the aircraft and data, receives on low and high speed ARINC 429 buses. The paper also considers the possibility of receiving and sending data via ARINC 618 […]

THE MATHEMATICAL AND SIMULINK MODELS FOR DETERMINING ATTITUDE OF AIRCRAFT USING MEMS SENSORS

Abstract. This paper analyses the features, types and principles of construction of miniature gyroscopes and accelerometers, as one of the main types of sensors of inertial measuring systems. An analysis is also being made of the possibilities and prospects for integrating magnetometers and GPS modules into inertial computing systems, which significantly improvers the performance of […]

ANALYZES OF MODERN PROBLEMS IN RADIO ALTIMETER SYSTEM AND ITS SOLUTION METHODS

Abstract. The modern problems of low-altitude aircraft radio altimeters is researched and a new diagnostic method is proposed to solve existing problems in this article. It is shown that controlling the correct operation of the radio altimeter system can be carry out based on the use of a new diagnostic method. As a result, it […]

THE APPLICATION OF MEMS TECHNOLOGY TO DETERMINE AN AIRCRAFT ORIENTATION

Abstract. This paper analyzes the features of MEMS and the possibility of their use to build AHRS with flexible parameters, with the aim of using them on unmanned aerial vehicles. It is shown that the correct use of newer versions of modern MEMS, which have 3-axis gyroscopes, accelerometers and magnetometers, can provide complete and accurate […]

THE APPLICATION OF MEMS TECHNOLOGY TO DETERMINE AN AIRCRAFT ORIENTATION

Abstract. This paper analyzes the features of MEMS and the possibility of their use to build AHRS with flexible parameters, with the aim of using them on unmanned aerial vehicles. It is shown that the correct use of newer versions of modern MEMS, which have 3-axis gyroscopes, accelerometers and magnetometers, can provide complete and accurate […]

INTEGRATED NAVIGATION SUBSYSTEM FOR NANO-SATELLITES

Abstract. The article examines the application of small, low-power satellite navigation receivers in nano-satellites, analyzes the technical performance of unified miniature GPS modules, microelectromechanical (MEMS) inertial measurement modules for nano-satellites and integrated navigation receivers and opportunities have been explored. The integrated navigation subsystem is used to estimate the position, velocity, and attitude of a vehicle […]