Наукові роботи проректора з наукової роботи НАУ Харченка В.П.
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Наукові роботи проректора з наукової роботи НАУ Харченка Володимира Петровича
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Item Mathematical Model of Errors of Odometry and Georeferencing Channels in Visual Correlation Extreme Navigation(2017) Харченко, Володимир Петрович; Mukhina, Maryna Petrivna; Kharchenko, Volodymyr PetrovychThe mathematic model of errors in correlation with the extreme navigation system (CENS) is developed basing on odometry and geo-referencing channels. The realization of the model is done in Simulink, and based on regular and random components of additive noise. The results of simulations prove accumulation of errors for odometry errors and its mitigation in case of geo-referencing in periods of correction.Item Theoretical Approaches for Safety Levels Measurements – Sequential Probability Ratio Test (SPRT)(Logistics and Transport, 2017) Харченко, Володимир Петрович; Kharchenko, Volodymyr; Antonova, Anna; Bugayko, Dmytro; Grigorak, Maria; Pawęska, MarcinThe principles of civil aviation safety are considered. At present time, aviation is an ultra-safe system, (i.e. a system that experiences less than one catastrophic safety breakdown every one million production cycles). But, unfortunately, we can never state that aviation activities will be absolutely safe. In current conditions the increase of the civil aviation safety level is one of the principal objectives of the world air transport development. The paper pays special attention to the civil aviation threats and risks in the context of globalization processes. The investigation deals with problems of global implementation of Annex 19 to the Convention of the International Civil Aviation. Present research paper discusses new theoretical approaches to searching for methods to assess the “safety space” of civil aviation activity. Special attention is paid to an effective test, proposed by A. Wald.Item Application of Imprecise Models in Analysis of Risk Management of Software Systems(Вісник Національного Авіаційного Університету, 2017) Харченко, Володимир Петрович; Kharchenko, Volodymyr; Alexeiev, Oleg; Rudas, Sergiy; Kozhokhina, Olena; Алексєєв, В.М.; Рудас, C.І.; Кожохіна, О.В.; Харченко, В.П.; Алексеев, В.Н.; Рудас, С.И.; Кожохина, Е.В.The analysis of functional completeness for existing detection systems was conducted. It made it possible to define information systems with a similar feature set, to assess the degree of similarity and the matching degree of the means from the "standard" model of risk management system, that considers the recommended ICAO practices and standards on aviation safety, to justify the advisability of decision-making support system creation, using imprecise model and imprecise logic for risk analysis at aviation activities. Imprecise models have a number of features regarding the possibility of taking into account the experts’ intuition and experience, the possibility of more adequate flight safety management processes modelling and obtaining the accurate decisions that correlate with the initial data; support for the rapid development of a safety management system with its further functionality complexity increase; their hardware and software implementation in control systems and decision making is less sophisticated in comparison with classical algorithms.Item МІЖНАРОДНЕ ПРАВОВЕ РЕГУЛЮВАННЯ БЕЗПЕКИ ВИКОРИСТАННЯ ДИСТАНЦІЙНО ПІЛОТОВАНИХ АВІАЦІЙНИХ СИСТЕМ(2017) Павеска, Марчин; Бо, Ван; Харченко, Володимир Петрович; Бугайко, Д. О.Дистанційно-пілотовані авіаційні системи (ДПАС) є новим компонентом авіаційної системи в цілому, вивченням, визначенням і в кінцевому підсумку інтеграцією якого в даний час займаються Міжнародна організація цивільної авіації (ІСАО), держави і галузеві організації. Ці системи, засновані на новітніх розробках в області авіаційно-космічних технологій, можуть відкрити нові і розширити наявні можливості цивільних / комерційних видів застосування і підвищити рівень безпеки польотів та ефективності діяльності всієї цивільної авіації.Item Justification of Control System Types of Unmanned Aerial Vehicle for Civil Aviation(Вісник Національного Авіаційного Університету, 2017-03) Харченко, Володимир Петрович; Kharchenko, Volodymyr; Мatiychyk, Denys; Матійчик, Д.М.; Харченко, B.П.; Матийчик, Д.М.Objective: The problem of unmanned aerial vehicle control systems is a complicated issue which requires consideration of the tasks and applications of unmanned aerial vehicles. The typology of control systems combination for civil unmanned aerial vehicle is suggested and justified. Methods: The methodology of the research was based on application of the varieties of the experts method for rationale of the variants of control system combinations for a specific type of unmanned aerial vehicle and the morphological analysis was used to generate the variants of control system combinations. Results: The causes that lead to discrepancies in types of control systems for civil unmanned aerial vehicle are revealed. Compliance between remote radio control application and type of feedback signal are considered. Based on morphological analysis method, 25 variants of combined unmanned aerial vehicle control systems are suggested. Discussion: Regulatory, substantive and technical components of basic unmanned aerial vehicle control systems are considered. The practical experience of the development by Scientific Production Center of Unmanned Aviation “Virazh” is used to demonstrate the applicability of findings.Item Models of Air Traffic Controllers Errors Prevention in Terminal Control Areas under Uncertainty Conditions(Вісник Національного Авіаційного Університету, 2017-03) Харченко, Володимир Петрович; Kharchenko, Volodymyr; Chynchenko, Yuriy; Чинченко, Ю.В.Purpose: the aim of this study is to research applied models of air traffic controllers’ errors prevention in terminal control areas (TMA) under uncertainty conditions. In this work the theoretical framework descripting safety events and errors of air traffic controllers connected with the operations in TMA is proposed. Methods: optimisation of terminal control area formal description based on the Threat and Error management model and the TMA network model of air traffic flows. Results: the human factors variables associated with safety events in work of air traffic controllers under uncertainty conditions were obtained. The Threat and Error management model application principles to air traffic controller operations and the TMA network model of air traffic flows were proposed. Discussion: Information processing context for preventing air traffic controller errors, examples of threats in work of air traffic controllers, which are relevant for TMA operations under uncertainty conditions.Item MODELLING OF DECISION MAKING OF UNMANNED AERIAL VEHICLE'S OPERATOR IN EMERGENCY SITUATIONS(Вісник Національного Авіаційного Університету, 2017-03) Харченко, Володимир Петрович; Kharchenko, Volodymyr; Shmelova, Tatyana; Znakovska, Yevgeniya; Bondarev, Dmitriy; Stratiy, Andriy; Шмельова, Т.Ф.; Знаковська, Є.А.; Бондарєв, Д.І.; Стратій, А.В.; Харченко, В.П.; Шмелева, Т.Ф.; Знаковська, Е.А.; Бондарев, Д.И.; Стратий, А.В.Purpose: lack of recommendation action algorithm of UAV operator in emergency situations; decomposition of the process of decision making (DM) by UAV’s Operator in emergency situations; development of the structure of distributed decision support system (DDSS) for remotely piloted aircraft; development of a database of local decision support system (DSS) operators Remotely Piloted Aircraft Systems (RPAS); working-out of models DM by UAV’s Operator. Methods: Algoritm of actions of UAV operator by Wald criterion, Laplace criterion, Hurwitz criterion. Results: The program "UAV_AS" that gives to UAV operator recommendations on how to act in case of emergency. Discussion: The article deals with the problem of Unmanned Aerial Vehicles (UAV) flights for decision of different tasks in emergency situation. Based on statistical data it was analyzing the types of emergencies for unmanned aircraft. Defined sequence of actions UAV operator and in case of emergencies.Item SYNTHESIS OF CONFLICT-FREE AIRCRAFT FLIGHT TRAJECTORIES USING MULTI-CRITERIA DYNAMIC PROGRAMMING(Taylor & Francis, 2017) Харченко, Володимир Петрович; Kharchenko, Volodymyr; Vasyliev, Denys; Vasyliev, VolodymyrThe paper discusses the problem of flight trajectory synthesis that is conducted to prevent potential conflict situations between two aircraft in air traffic. A method of multi-objective sequential synthesis of conflict-free flight trajectories is developed. This method provides the synthesis of Pareto conflict-free trajectories using multi-criteria dynamic programming and selection of the optimal trajectory. The paper also considers the principles of discretization concerning states and controls to apply dynamic programming. An analysis of the proposed method is performed using computer simulation.Item COMPLETE SEPARATION OF THE VERTICAL AND HORIZONTAL INDEPENDENT COMPONENTS OF THE FLIGHT IN POLICOPTER UAV NAU PKF "AURORA" AND MATHEMATICAL MODEL OF THIS FLIGHT(Вісник Національного Авіаційного Університету, 2017) Харченко, Володимир Петрович; Kharchenko, Volodymyr; Nakhaba, Alexandr; Нахаба, О.О.Purpose: This article presents a mathematical model and the experimental results of automatic flights of the policopter UAV NAU PKF "Aurora" of oktacopter scheme with additional elektroimpeler engines of horizontal thrust. Methods: UAV NAU PKF "Aurora" is developed for experimental flights in manual, semiautomatic and unmanned modes. The uniqueness and scientific novelty of data of flight testes is in a complete separation and isolation of vertical and horizontal components of the flight, which enables a fundamentally new way of moving of vehicle in the aerial space. This approach gives a ability to obtain all advantages and to eliminate disadvantages of helicopter and airplane in fundamentally new aircraft by structure and by function – namely in the policopter flyer with additional independent engines of the lateral thrust. Results: Obtained a new experimental data that allowed to better understand the nature of the physical forces, providing the flight of the policopter. Discussion: Revised a physical basis of the airscrew (propeller), namely on the example of flight of the policopter proved that most of the thrust of the propeller provided by the mechanical impulse (kinetic energy Ек=mv2/2) by the impulse, that a airscrew receives at his collisions with air molecules,but not by the gradient of air pressure below and above the airscrew. Is put forward a hypothesis of gravitational nature of the flight and introduced the notion of "functional antigravity", that a force completely identical in function and opposite on the direction of the force of gravity (gravity force). Deduced a mathematical formula of "functionally antigravitational" transport, namely:G·M·m/R2= mI·v2/2 – for the flights of the aircraft with a mass m over universal astronomical body with a mass M, and m·g = mI·v2/2 – for the flights of the aircraft with mass m over a planet Earth.Item PROBABILISTIC APPROACH TO OBJECT DETECTION AND RECOGNITION FOR VIDEOSTREAM PROCESSING(Вісник Національного Авіаційного Університету, 2017) Харченко, Володимир Петрович; Kharchenko, Volodymyr; Kukush, Alexander; Кукуш, О.Г.; Kuzmenko, Nataliia; Кузьменко, Н.С.; Ostroumov, Ivan; Остроумов, І.В.Purpose: The represented research results are aimed to improve theoretical basics of computer vision and artificial intelligence of dynamical system. Proposed approach of object detection and recognition is based on probabilistic fundamentals to ensure the required level of correct object recognition. Methods: Presented approach is grounded at probabilistic methods, statistical methods of probability density estimation and computer-based simulation at verification stage of development. Results: Proposed approach for object detection and recognition for video stream data processing has shown several advantages in comparison with existing methods due to its simple realization and small time of data processing. Presented results of experimental verification look plausible for object detection and recognition in video stream. Discussion: The approach can be implemented in dynamical system within changeable environment such as remotely piloted aircraft systems and can be a part of artificial intelligence in navigation and control systems.Item MUNICIPAL AVIATION FUNCTIONING AS ONE OF FUTURE TYPES OF THE AVIATION ACTIVITIES(Вісник Національного Авіаційного Університету, 2017) Kharchenko, Volodymyr; Alexeiev, Oleg; Yurchik, Roman; Ali, Ismail; Харченко, Володимир Петрович; Алексєєв, В.М.; Юрчик, Р.; Алі, І.; Харченко, В.П.; Алексеев, В.Н.; Юрчик, Р.; Али, И.In the article we represent the basic principles of municipal air transport within the metropolis. The main tasks of creating municipal transport are defined to further develop of aviation technologies for municipal economy and life support of the city and its air-transport system. In order to further development of aviation technology in the interests of the urban economy and life of the city, its air transportation system is necessary to decide three main objectives: development of aviation equipment and saturation of City Aviation park by light helicopters which will ensure solving of special tasks for the benefit of urban services, commercial transportation and air operations; development of urban aviation infrastructure, including heliports and helipads; the organization of safe use of the airspace over the city. The use of technology in aviation can be done while ensuring sanitary and environmental standards of environmental protection.Item FACTORS BEHIND EFFICIENCY OF INTERACTION BETWEEN REMOTE PILOT AND UNMANNED AERIAL VEHICLE(Вісник Національного Авіаційного Університету, 2017) Kharchenko, Volodymyr; Мatiychyk, Denys; Харченко, Володимир Петрович; Матійчик, Д.М.Objective. Based on probable reasons of aviation accidents in civil unmanned aviation and relative risks, various factors that influence safe and effective interaction of remote pilot and unmanned aerial vehicle are considered. Methods. To solve the problem some assumptions, which lie in the fact that one “humanmachine” system was considered, were made. This system consists of one human and one machine. Unmanned aviation complex that consists of unmanned aerial vehicle, ground control station and data links was taken as the machine. Problem is observed on the stage of operation life cycle of aviation engineering. Results. The following significant reasons (factors) are considered, defined and formalized: control mode of unmanned aerial vehicle, technical level of unmanned aviation system components, organization of operator’s workplace of remote pilot, ambient environment (meteorological conditions) and quality of decision making of human – remote pilot. Based on summarized desirability function of E. Harington three experiments were performed and results were obtained. Discussion. The question of safe and effective unmanned aerial vehicle operation of commercial application is considered to be very problematic and therefore urgent.Item A NEW METHOD OF UNIFIED PROCESSING OF THE INFORMATION, REFERRED IN THE FORM OF THE THREE-DIMENSIONAL ASSOCIATIVE-LOGICAL STRUCTURE FOR OPTIMIZATION OF THE MULTIROTOR UNMANED AVIATION SYSTEM(Вісник Національного Авіаційного Університету, 2017-09) Kharchenko, Volodymyr; Nakhaba, Alexandr; Харченко, В.П.; Нахаба, О.О.; Харченко, В.П.; Нахаба, А.А.; Харченко, Володимир ПетровичPurpose: This article presents a mathematical model and a new way of unified information processing. Methods: Three-dimensional associative-logical synthesis. Results: Obtained a new experimental data. Discussion: The present invention can be used in the following directions: 1) in epistemology, the basis for a more effective and purposeful scientific search in all branches of science; 2) in psychology and pedagogy - the basis for a more effective and universal thinking of man in almost all sections of science; 3) in electronics and computer science - the basis for the creation of artificial intelligence systems and high-quality systems for speech and images recognition, provided that are created the chips in which the storage elements are interconnected in three dimensions; 4) in the aerospace and robotics sectors - the possibility of developing a new, more advanced autopilot systems, capable of working according to the principles of the neural network of biological objects.Item ADS-B Satellite Communication Channel Based on IEEE 802.16 Standard(De Gruyter Open, 2017-12) Kharchenko, Volodymir; Grekhov, Andrii; Kondratiuk, Vasyl; Nagorna, KarinaOriginal models of “Aircraft-Satellite-Ground Station” communication channel based on IEEE 802.16 standard were built by using MATLAB Simulink. The influence of aircraft transmitter nonlinearity for different types of fading in the channel (Rayleigh and Rician) was studied and the possibility of correcting nonlinearity by using pre-distortion was revealed. The impact of space-time diversity (MISO 2 × 1) for different types of fading in channels was investigated. The effect of the Doppler frequency shift on the operation of communication channels was analyzed.Item MATHEMATICAL MODEL OF UNMANNED AERIAL VEHICLE CONTROL IN SINGLE CONTROL CHANNEL(Вісник Національного Авіаційного Університету, 2017-12) Kharchenko, Volodymyr; Мatiychyk, Denys; Харченко, B.П.; Матійчик, Д.М.; Харченко, B.П.; Матийчик, Д.М.; Харченко, Володимир ПетровичThe main aim of this research is development of the mathematical model. Developed model will allow deeper, qualitative and faster selection of the proper values of coefficients that are necessary for optimal and effective interaction between the human and machine. Methods. In order to develop a mathematical model of unmanned aerial vehicle control in a single control channel, the classical model of aircraft control was applied. Comparative analysis of turn execution in manual and semiautomatic control modes of unmanned aerial vehicle by remote pilot was applied. Results. The mathematical model “Remote pilot – Remote Control System – Unmanned Aerial Vehicle” under change of unmanned aerial vehicle heading on horizontal plane was proposed. The model takes into account the remote pilot’s actions during airplane control, as well as of aircraft maneuverability when it is equipped with radio control and has a flight controller with several modes of operation. Discussion. The proposed model gives a possibility to analyze peculiarities of different control modes used for unmanned aerial vehicle operation. Select the proper values of coefficients that are necessary for optimal and effective interaction between the human and the machine.Item AIRCRAFT NAVIGATION EFFICIENCY IMPROVING DURING LANDING USING SATELLITE NAVIGATION SYSTEM(Вісник Національного Авіаційного Університету, 2017-12) Kharchenko, Volodymyr; Konin, Valeriy; Olevinska, Tetiana; Харченко, Володимир Петрович; Конін, В.В.; Олевінська, Т.І.; Харченко, В. П.; Конин, В.В.; Олевинская, Т.И.; Харченко, Володимир ПетровичPurpose: Two algorithms have been considered in this article. Both of them make possible to improve aircraft navigation efficiency during landing by satellite navigation system signals. The first algorithm describes creation of two reference planes in space using measured coordinates of four points on the runway and the subsequent calculation of the aircraft horizontal and vertical angular deviation from these planes. The second algorithm describes an autonomous integrity control in the aerodrome area when four satellites are visible. Methods: methods of experiment planning, analytic geometry and linear algebra have been used. Results: obtained a new experimental data. Discussion: The results of experimental research of the first algorithm showed the principal possibility of deviation calculation in this way. It is shown that implementation of this technology will make it possible to increase the efficiency of small aircrafts navigation during landing at aerodromes and landing areas that are currently not equipped with radio equipment for instrument landing. The results of research of the second algorithm showed that it allows reducing the number of satellite navigation system failures and also enhances navigation efficiency. These results can be used in the aerospace sector for reducing the number of small aircraft non-flying periods.Item PULSE CHARACTERISTICS OF NETWORK SATELLITE SYSTEMS ADAPTIVE ANTENNA FOR ASSESSING CORRELATION INTERFERENCE MATRIX(Вісник Національного Авіаційного Університету, 2017-12) Kharchenko, Volodymyr; Харченко, В. П.; Харченко, В. П.; Shvets, Valerian; Швець, В. А.; Швец, В. А.; Харченко, Володимир ПетровичPurpose: On the basis of spatial filtering, we propose a method for direct calculation of the inverse correlation interference matrix with unknown parameters of the input action for controlling the pattern of the adaptive antenna array using the impulse response of the spatial filter. Methods: the approach is based on the theory of random processes and adaptive signal processing. Results: the proposed method of direct calculation of the inverse correlation matrix has shown the possibility of carrying out such calculations without a prior knowledge of the interference direction, the correlation function of the interference, and also the spectral characteristics of the interference. The method allows to reduce the calculation time of the inverse correlation matrix and eliminate the errors caused by constructive inaccuracies of the radio channels of the adaptive antenna array, which in turn reduces the error in measuring the direction of the interference source. Discussion: the method is suggested in order to ensure availability and consistency of network satellite systems’ navigation data.Item SIMPLE OBJECTS DETECTION AND RECOGNITION BY THE PROBABILISTIC APPROACH(Вісник Національного Авіаційного Університету, 2017-12-27) Kharchenko, Volodymyr; Kukush, Alexander; Chyrka, Iurii; Харченко, В.П.; Кукуш, О.Г.; Чирка, Ю.Д.; Харченко, Володимир ПетровичPurpose: The represented research results are aimed to better understanding of computer vision methods and their capabilities. The statistical approach of object detection and recognition allows processing of typical objects with simple descriptors. Methods: Considered approach is grounded at probabilistic methods, kernel density estimation and computer-based simulation as a verification tool. Results: Considered approach for object detection and recognition has shown several advantages in comparison with existing methods due to its simple realization and small time of data processing. Presented results of experimental verification prove that the considered method can be applied for detection and classification of objects with various shapes. Discussion: The approach can be implemented in a variety of computer vision systems that observe objects in difficult noisy conditions.Item Мультирівнева модель даних для ідентифікації забезпеченості вимог відповідно нормативно-правовому забезпеченню кібербезпеки цивільної авіації(Національний авіаційний університет, 2017-03) Харченко, Володимир Петрович; Харченко, Владимир Петрович; Kharchenko, Volodymyr; Корченко, Александр Григорьевич; Корченко, Олександр Григорович; Korchenko, Oleksandr; Гнатюк, Сергій Олександрович; Гнатюк, Сергей Александрович; Gnatyuk, SergiyЗахист критичної інфраструктури на сьогодні є одним із першочергових завдань держави, особливо гостро це питання постає перед державами, які впроваджують новітні інформаційно-комунікаційні технології в усіх критичних галузях. Зазначені технології, крім іншого, породжують цілу низку нових уразливостей та потенційних кіберзагроз. У галузі цивільної авіації рівень критичності значно підсилюється комунікацією та взаємодією між наземними системами і повітряними суднами. Відома модель формування вимог до забезпечення кібербезпеки цивільної авіації дозволяє форма- лізувати процес створення повної множини вимог, які необхідно забезпечити для захисту цивільної авіації від кіберзагроз, проте відсутній механізм визначення забезпеченості певних режимів безпеки внаслідок реалізації методів та засобів, задекларованих у відповідних вимогах. З огляду на це, актуальною є розробка підходу до визначення забезпеченості режимів безпеки, що враховуватимуть додаткові характеристики безпеки. У цій роботі запропоновано мультирівневу модель даних, яка за рахунок використання базової моделі формування вимог до забезпечення кібербезпеки цивільної авіації, конкатенації бінарних послідовностей, що характеризують режими безпеки, та бінарно-шістнадцяткового кодового представлення характеристик безпеки, множини моделей безпеки та підмножин характеристик безпеки (з урахуванням додаткових характеристик), дозволяє формалізувати процес ідентифікації забезпеченості вимог та визначення режимів безпеки критичних авіаційних інформаційних систем. У подальших дослідженнях планується розробити метод оцінювання повноти забезпечення вимог у результаті реалізації відповідних методів та засобів захисту.Item Нелінійне та багатокритеріальне моделювання процесів у системах керування рухом(2015) Харченко, Володимир Петрович; Писарчук, В.П.У монографії запропоновано нове вирішення актуальної науково-прикладної проблеми розроблення й удосконалення методів побудови нелінійних та багатокритеріальних моделей для систем і процесів керування рухом з використанням диференціальних перетворень та нелінійної схеми компромісів. Зокрема розглянуто: метод побудови нелінійних моделей руху динамічних об’єктів за експериментальними даними на базі диференціальних перетворень; метод визначення просторових координат рухомих об’єктів на основі порівнянь ортогональних відображень теоретичної та експериментальної моделей їх руху; багатокритеріальну математичну модель визначення оптимальної просторової структури багатопозиційної інформаційної системи та системи накопичення цільової інформації; методики вироблення рішень з використанням багатокритеріальних моделей, які забезпечують розв’язання задач оптимального розподілу обмежених ресурсів, оцінювання ефективності досліджуваних процесів та систем, ідентифікацію технічних засобів і контрольованих ситуацій за сукупністю ознак. Монографія буде корисна науковцям, аспірантам та студентам, які працюють у галузі науки, що охоплює проблеми розроблення й удосконалення математичного та інформаційного забезпечення систем навігації і керування рухом.