title: Ð¡Ð¸ÑÑÐµÐ¼Ð° Ð¼Ð°Ð³Ð½Ð¸ÑÐ½Ð¾Ð¹ Ð¾ÑÐ¸ÐµÐ½ÑÐ°ÑÐ¸Ð¸ Ð¼Ð°Ð»ÑÑ ÐºÐ¾ÑÐ¼Ð¸ÑÐµÑÐºÐ¸Ñ Ð°Ð¿Ð¿Ð°ÑÐ°ÑÐ¾Ð²
title: Ð²ÑÐ¿ÑÑÐºÐ½Ð°Ñ ÐºÐ²Ð°Ð»Ð¸ÑÐ¸ÐºÐ°ÑÐ¸Ð¾Ð½Ð½Ð°Ñ ÑÐ°Ð±Ð¾ÑÐ° Ð¼Ð°Ð³Ð¸ÑÑÑÐ°
titleType: Subtitle
title: Magnetic orientation system for a small spacecraft
Creators: name: ÐÐ»ÑÑÐ¸Ð½Ð°, ÐÐ°ÑÐ¸Ñ
Publisher: name: Ð¡Ð°Ð½ÐºÑ-ÐÐµÑÐµÑÐ±ÑÑÐ³ÑÐºÐ¸Ð¹ Ð¿Ð¾Ð»Ð¸ÑÐµÑÐ½Ð¸ÑÐµÑÐºÐ¸Ð¹ ÑÐ½Ð¸Ð²ÐµÑÑÐ¸ÑÐµÑ ÐÐµÑÑÐ° ÐÐµÐ»Ð¸ÐºÐ¾Ð³Ð¾
Year: 2023
Subjects: ÐÐ¾ÑÐ¼Ð¸ÑÐµÑÐºÐ¸Ðµ Ð»ÐµÑÐ°ÑÐµÐ»ÑÐ½ÑÐµ Ð°Ð¿Ð¿Ð°ÑÐ°ÑÑ
ÐÐ°ÑÑÐ¸ÐºÐ¸
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Ð¼Ð°Ð»ÑÐ¹ ÑÐ¿ÑÑÐ½Ð¸Ðº
Ð°ÐºÑÐ¸Ð²Ð½Ð°Ñ ÑÐ¸ÑÑÐµÐ¼Ð° Ð¾ÑÐ¸ÐµÐ½ÑÐ°ÑÐ¸Ð¸
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ÑÑÐ°Ð±Ð¸Ð»Ð¸Ð·Ð°ÑÐ¸Ñ
Ð¸ÑÐ¿Ð¾Ð»Ð½Ð¸ÑÐµÐ»ÑÐ½ÑÐ¹ ÑÐ»ÐµÐ¼ÐµÐ½Ñ
magnetic orientation system
small satellite
active orientation system
passive orientation system
stabilization
actuating element

description: ÐÐ±ÑÐµÐºÑ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ â ÑÐ¸ÑÑÐµÐ¼Ð° Ð¼Ð°Ð³Ð½Ð¸ÑÐ½Ð¾Ð¹ Ð¾ÑÐ¸ÐµÐ½ÑÐ°ÑÐ¸Ð¸. Ð¦ÐµÐ»Ñ ÑÐ°Ð±Ð¾ÑÑ â ÑÐ°Ð·ÑÐ°Ð±Ð¾ÑÐºÐ° ÑÐ¸ÑÑÐµÐ¼Ñ Ð¼Ð°Ð³Ð½Ð¸ÑÐ½Ð¾Ð¹ Ð¾ÑÐ¸ÐµÐ½ÑÐ°ÑÐ¸Ð¸ Ð¼Ð°Ð»Ð¾Ð³Ð¾ ÐºÐ¾ÑÐ¼Ð¸ÑÐµÑÐºÐ¾Ð³Ð¾ Ð°Ð¿Ð¿Ð°ÑÐ°ÑÐ°. Ð ÑÐµÐ·ÑÐ»ÑÑÐ°ÑÐµ ÑÐ°Ð±Ð¾ÑÑ Ð±ÑÐ»Ð° ÑÐ°Ð·ÑÐ°Ð±Ð¾ÑÐ°Ð½Ð° ÑÐ¸ÑÑÐµÐ¼Ð° Ð¼Ð°Ð³Ð½Ð¸ÑÐ½Ð¾Ð¹ Ð¾ÑÐ¸ÐµÐ½ÑÐ°ÑÐ¸Ð¸ Ð´Ð»Ñ ÑÐ¿ÑÑÐ½Ð¸ÐºÐ° ÐºÐ»Ð°ÑÑÐ° CubeSat, ÑÐ¸ÑÑÐµÐ¼Ð° Ð¾ÑÐ¸ÐµÐ½ÑÐ°ÑÐ¸Ð¸ Ð¸Ð¼ÐµÐµÑ Ð²Ð¸Ð´ Ð¿ÐµÑÐ°ÑÐ½Ð¾Ð¹ Ð¿Ð»Ð°ÑÑ, ÑÐ°Ð·Ð¼ÐµÑÐ¾Ð¼ 8 Ð½Ð° 8 ÑÐ¼2. ÐÑÑÐ¾Ð´Ñ Ð¸Ð· Ð½Ð°Ð·Ð½Ð°ÑÐµÐ½Ð¸Ñ ÑÐ¿ÑÑÐ½Ð¸ÐºÐ° Ð¸ ÐµÐ³Ð¾ Ð³Ð°Ð±Ð°ÑÐ¸ÑÐ¾Ð² Ð±ÑÐ»Ð° Ð²ÑÐ±ÑÐ°Ð½Ð° Ð°ÐºÑÐ¸Ð²Ð½Ð°Ñ ÑÐ¸ÑÑÐµÐ¼Ð° Ð¾ÑÐ¸ÐµÐ½ÑÐ°ÑÐ¸Ð¸ Ð¸ Ð¸ÑÐ¿Ð¾Ð»ÑÐ·Ð¾Ð²Ð°Ð½Ð¸ÐµÐ¼ Ð² ÐºÐ°ÑÐµÑÑÐ²Ðµ Ð¸ÑÐ¿Ð¾Ð»Ð½Ð¸ÑÐµÐ»ÑÐ½Ð¾Ð³Ð¾ ÑÐ»ÐµÐ¼ÐµÐ½ÑÐ° ÑÐ¾ÐºÐ¾Ð²Ð¾Ð¹ ÐºÐ°ÑÑÑÐºÐ¸, ÐºÐ¾ÑÐ¾ÑÐ°Ñ Ð²ÑÑÑÐ¾ÐµÐ½Ð° Ð² Ð¿ÐµÑÐ°ÑÐ½ÑÑ Ð¿Ð»Ð°ÑÑ. ÐÑÐ»Ð° Ð¿ÑÐ¾Ð¸Ð·Ð²ÐµÐ´ÐµÐ½Ð° Ð¾ÑÐµÐ½ÐºÐ° Ð²ÐµÐ»Ð¸ÑÐ¸Ð½Ñ ÑÑÐµÐ±ÑÐµÐ¼Ð¾Ð³Ð¾ Ð¼Ð°Ð³Ð½Ð¸ÑÐ½Ð¾Ð³Ð¾ Ð¼Ð¾Ð¼ÐµÐ½ÑÐ° ÐºÐ°ÑÑÑÐºÐ¸ Ð¸ Ð² ÑÐ¾Ð¾ÑÐ²ÐµÑÑÑÐ²Ð¸Ð¸ Ñ Ð¿Ð¾Ð»ÑÑÐµÐ½Ð½ÑÐ¼Ð¸ Ð´Ð°Ð½Ð½ÑÐ¼Ð¸ Ð±ÑÐ»Ð¸ ÑÐ°ÑÑÑÐ¸ÑÐ°Ð½Ñ Ð½ÐµÐ¾Ð±ÑÐ¾Ð´Ð¸Ð¼ÑÐµ Ð¿Ð°ÑÐ°Ð¼ÐµÑÑÑ Ð¿ÐµÑÐ°ÑÐ½Ð¾Ð¹ ÐºÐ°ÑÑÑÐºÐ¸. Ð ÑÐ¾Ð´Ðµ ÑÐ°Ð±Ð¾ÑÑ Ð±ÑÐ»Ð° ÑÐ¾Ð·Ð´Ð°Ð½Ð°Â ÑÑÑÑÐºÑÑÑÐ½Ð°Ñ Ð¸ Ð¿ÑÐ¸Ð½ÑÐ¸Ð¿Ð¸Ð°Ð»ÑÐ½Ð°Ñ ÑÑÐµÐ¼Ð° ÑÑÑÑÐ¾Ð¹ÑÑÐ²Ð°, Ð¿Ð¾Ð´Ð¾Ð±ÑÐ°Ð½Ð° ÑÐ»ÐµÐ¼ÐµÐ½ÑÐ½Ð°Ñ Ð±Ð°Ð·Ð°. ÐÑÐ»Ð° ÑÐ°Ð·ÑÐ°Ð±Ð¾ÑÐ°Ð½Ð° Ð¿ÐµÑÐ°ÑÐ½Ð°Ñ Ð¿Ð»Ð°ÑÐ° ÑÑÑÑÐ¾Ð¹ÑÑÐ²Ð°. ÐÐ¾ÑÐ»Ðµ Ð¿ÑÐ¾Ð³ÑÐ°Ð¼Ð¼Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ð¸Â  Ð¿ÐµÑÐ°ÑÐ½Ð¾Ð¹ Ð¿Ð»Ð°ÑÑ Ð±ÑÐ»Ð¾ Ð¿ÑÐ¾Ð²ÐµÐ´ÐµÐ½Ð° Ð¿ÑÐ¾Ð²ÐµÑÐºÐ° ÑÐ°Ð±Ð¾ÑÐ¾ÑÐ¿Ð¾ÑÐ¾Ð±Ð½Ð¾ÑÑÐ¸ ÑÑÑÑÐ¾Ð¹ÑÑÐ²Ð°. Ð£ÑÑÐµÐ½Ñ ÑÐµÑÐ¼Ð¸Ð½Ð¾Ð»Ð¾Ð³Ð¸ÑÐµÑÐºÐ¸Ðµ Ð¾ÑÐ¾Ð±ÐµÐ½Ð½Ð¾ÑÑÐ¸ Ð¿ÑÐµÐ´Ð¼ÐµÑÐ½Ð¾Ð¹ Ð¾Ð±Ð»Ð°ÑÑÐ¸ Ð¸ Ð¿ÑÐ¸Ð¼ÐµÐ½ÐµÐ½Ñ Ð¿ÑÐ¾Ð³ÑÐ°Ð¼Ð¼Ð½ÑÐµ ÑÑÐµÐ´ÑÑÐ²Ð° Ð´Ð»Ñ ÑÐµÑÐµÐ½Ð¸Ñ Ð·Ð°Ð´Ð°Ñ. ÐÑÐ¸Ð¼ÐµÐ½ÐµÐ½Ð¾ ÑÐ¿ÐµÑÐ¸Ð°Ð»Ð¸Ð·Ð¸ÑÐ¾Ð²Ð°Ð½Ð½Ð¾Ðµ Ð¿ÑÐ¾Ð³ÑÐ°Ð¼Ð¼Ð½Ð¾-Ð¼Ð°ÑÐµÐ¼Ð°ÑÐ¸ÑÐµÑÐºÐ¾Ðµ Ð¾Ð±ÐµÑÐ¿ÐµÑÐµÐ½Ð¸Ðµ MatLab, EasyEda, STM32CubeIDE.
description: The subject of the graduate qualification work is âMagnetic orientation systemâ. The given work is devoted to a magnetic orientation system for a small spacecraft. As a result of the work, a magnetic orientation system was developed for a CubeSat satellite, the orientation system has the form of a printed circuit board, 8 by 8 cm2 in size. Based on the purpose of the satellite and its dimensions, an active orientation system was chosen and using a current coil as an actuating element, which is built into the printed circuit board. The value of the required magnetic moment of the coil was estimated and, in accordance with the data obtained, the necessary parameters of the printed coil were calculated. In the course of the work, a structural and schematic diagram of the device was created, and the element base was selected. The printed circuit board of the device was developed. After programming the printed circuit board, the device was tested for operability. The terminological features of the subject area are taken into account and software tools are used to solve problems. Specialized software and mathematical software MatLab, EasyEda, STM32CubeIDE was used.