Аналіз обмінної потужності в системі живлення дрону

التفاصيل البيبلوغرافية
العنوان: Аналіз обмінної потужності в системі живлення дрону
المصدر: Microsystems, Electronics and Acoustics; Vol. 27 No. 1 (2022); 252748-1-252748-5
Микросистемы, Электроника и Акустика; Том 27 № 1 (2022); 252748-1-252748-5
Мікросистеми, Електроніка та Акустика; Том 27 № 1 (2022); 252748-1-252748-5
بيانات النشر: National Technical University of Ukraine "Igor Sikorsky Kyiv Polytechnic Institute", 2022.
سنة النشر: 2022
مصطلحات موضوعية: електротранспорт, обмінна потужність, unmanned aerial vehicle, безпілотний літальний апарат, UDC 621.314, drone, УДК 621.314, exchange power, electric vehicles, дрон
الوصف: The classification of drones - both military and civilian according to the relevant criteria - is presented. Block diagrams of a typical unmanned aerial vehicle and its power system are shown. Typically, a drone power system of the "micro", "mini" or "short range" category, according to the UVS international classification, is a set of DC / DC converters with a microprocessor control system. The power source for such aircraft is usually a battery, less often - fuel cells. During the flight, the engine speed is variable, and its change depends not only on changes in flight speed or direction, but also on weather conditions, such as wind, as the stabilization system constantly aligns the drone. This leads to the fact that the power supply system of such a device is actually a significant part of the time in transition condition. This leads to a significant content of the component of exchange energy that battery consumed which in turn will increase losses, and thus reduces the range of the unmanned aerial vehicle. The phenomenon of the occurrence of exchange power in the power supply systems of electric vehicles which powered from DC sources and specifically in the power supply system of an unmanned aerial vehicle is analyzed. The time diagrams of current, voltage, active and inactive components of power consumed from the mains power supply network of electric locomotive DE1 are illustrated. It can be seen that with a sharp change in the modes of operation of traction units there is a significant component of exchange power in the motor-network system. Such processes are typical for almost any electric vehicle and are associated with the presence of a significant number of reactive elements in the power supply systems, as well as frequent changes in load parameters. A block diagram of a typical unmanned aerial vehicle is presented. The unmanned aerial vehicle system consists of three parts: the air part, the unmanned aerial vehicle itself, the ground control station, which can be autonomous or manned, the control system, which provides communication and data transmission. The block diagram of the power system of a typical unmanned aerial vehicle is presented A simplified schematic diagram of the DC motor power supply system is presented. The relations for determining the amount of exchange power in the power supply system of an unmanned aerial vehicle are derived. It is concluded that to reduce the impact of this phenomenon, it is necessary to modify the power supply system by adding compensation units of inactive power component.
Представлена класифікація дронів – як військових так і цивільних за відповідними критеріями. Показані блок-схеми типового безпілотного літального апарату та його силової системи. Проаналізовано явище виникнення обмінної потужності в системах живлення електротранспорту від джерел постійного струму і конкретно в системі живлення безпілотного літального апарату. Представлена спрощена принципова схема системи живлення двигуна постійного струму. Виведено співвідношення для визначення величини обмінної потужності в системі живлення.
وصف الملف: application/pdf; image/png; image/tiff
اللغة: Ukrainian
تدمد: 2523-4447
2523-4455
DOI: 10.20535/2523-4455.2022.27.1
URL الوصول: https://explore.openaire.eu/search/publication?articleId=scientific_p::12ae5c92a90100db79580e4fab43128c
http://elc.kpi.ua/article/view/252748
حقوق: OPEN
رقم الأكسشن: edsair.scientific.p..12ae5c92a90100db79580e4fab43128c
قاعدة البيانات: OpenAIRE
الوصف
تدمد:25234447
25234455
DOI:10.20535/2523-4455.2022.27.1