STRUCTUAL MODEL AND REPORTING METHODOLOGY OF THE PERSPECTIVE ANTI-ICING SYSTEM FOR CIVIL AVIATION AIRCRAFT
Abstract: In this article, analyzes the operational and technical characteristics of anti-icing systems used in modern civil aircraft, as a promising anti-icing system, a structural model of a system equipped with a microwave generator that can be installed on the wing of an aircraft, as well as on other aircraft surfaces that may be subject […]
REVIEW OF INNOVATIVE METHODS TO IMPROVE THE RELIABILITY OF RADAR INFORMATION IN AIR TRAFFIC CONTROL
Abstract: The paper looks into how onboard aircraft technology may negatively impact the efficiency of ATC operations. It specifically notes that secondary surveillance radars (SSRs) may experience interference from systems like the Airborne Collision Avoidance System (ACAS), Automatic Dependent Surveillance-Broadcast (ADS-B), and other related systems that operate on the same frequency band. The accuracy of […]
APPLICATION OF AN ARTIFICIAL INTELLIGENCE SYSTEM TO INCREASE THE INFORMATION CONTENT OF REMOTE CONTROL OF THE OPERATION OF ON-BOARD SYSTEMS OF AIRCRAFT
Abstract: This paper explores the application of artificial intelligence (AI) systems to augment the information content and efficacy of remote-control operations for on-board systems in aircraft. With the aviation industry rapidly advancing towards automation and digitalization, there is a growing need for intelligent solutions that optimize remote control processes. This study investigates various AI techniques […]
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 […]
