Low-Cost Orientation Determination System for CubeSat Based Solely on Solar and Magnetic Sensors

CubeSats require accurate determination of their orientation relative to the Sun, Earth, and other celestial bodies to operate successfully and collect scientific data. This paper presents an orientation system based on solar and magnetic sensors that offers a cost-effective and reliable solution fo...
Ausführliche Beschreibung

Gespeichert in:

Autor*in:	Yerkebulan Nurgizat [verfasserIn] Abu-Alim Ayazbay [verfasserIn] Dimitri Galayko [verfasserIn] Gani Balbayev [verfasserIn] Kuanysh Alipbayev [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2023

Schlagwörter:	CubeSat satellite orientation solar sensors magnetic sensors attitude determination satellite–Sun vector

Übergeordnetes Werk:	In: Sensors - MDPI AG, 2003, 23(2023), 14, p 6388
Übergeordnetes Werk:	volume:23 ; year:2023 ; number:14, p 6388

Links:	Link aufrufen Link aufrufen Link aufrufen Journal toc

DOI / URN:	10.3390/s23146388

Katalog-ID:	DOAJ093830467

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spelling	10.3390/s23146388 doi (DE-627)DOAJ093830467 (DE-599)DOAJ1b5660a80a214375ae79f1e789bef870 DE-627 ger DE-627 rakwb eng TP1-1185 Yerkebulan Nurgizat verfasserin aut Low-Cost Orientation Determination System for CubeSat Based Solely on Solar and Magnetic Sensors 2023 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier CubeSats require accurate determination of their orientation relative to the Sun, Earth, and other celestial bodies to operate successfully and collect scientific data. This paper presents an orientation system based on solar and magnetic sensors that offers a cost-effective and reliable solution for CubeSat navigation. Solar sensors analyze the illumination on each face to measure the satellite’s orientation relative to the Sun, while magnetic sensors determine the Earth’s magnetic field vector in the satellite’s reference frame. By combining the measured data with the known ephemeris of the satellite, the satellite–Sun vector and the magnetic field orientation can be reconstructed. The orientation is expressed using quaternions, representing the rotation from the internal reference system of the satellite to the selected reference system. The proposed system demonstrates the ability to accurately determine the orientation of a CubeSat using only two sensors, making it suitable for installations where more complex and expensive instruments are impractical. Additionally, the paper presents a mathematical model of a low-cost CubeSat orientation system and a hardware implementation of the sensor. The technology, using solar and magnetic sensors, provides a reliable and affordable solution for CubeSat navigation, supporting the increasing sophistication of miniature payloads and enabling accurate satellite positioning in space missions. CubeSat satellite orientation solar sensors magnetic sensors attitude determination satellite–Sun vector Chemical technology Abu-Alim Ayazbay verfasserin aut Dimitri Galayko verfasserin aut Gani Balbayev verfasserin aut Kuanysh Alipbayev verfasserin aut In Sensors MDPI AG, 2003 23(2023), 14, p 6388 (DE-627)331640910 (DE-600)2052857-7 14248220 nnns volume:23 year:2023 number:14, p 6388 https://doi.org/10.3390/s23146388 kostenfrei https://doaj.org/article/1b5660a80a214375ae79f1e789bef870 kostenfrei https://www.mdpi.com/1424-8220/23/14/6388 kostenfrei https://doaj.org/toc/1424-8220 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_206 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2005 GBV_ILN_2009 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2111 GBV_ILN_2507 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 23 2023 14, p 6388
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allfieldsSound	10.3390/s23146388 doi (DE-627)DOAJ093830467 (DE-599)DOAJ1b5660a80a214375ae79f1e789bef870 DE-627 ger DE-627 rakwb eng TP1-1185 Yerkebulan Nurgizat verfasserin aut Low-Cost Orientation Determination System for CubeSat Based Solely on Solar and Magnetic Sensors 2023 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier CubeSats require accurate determination of their orientation relative to the Sun, Earth, and other celestial bodies to operate successfully and collect scientific data. This paper presents an orientation system based on solar and magnetic sensors that offers a cost-effective and reliable solution for CubeSat navigation. Solar sensors analyze the illumination on each face to measure the satellite’s orientation relative to the Sun, while magnetic sensors determine the Earth’s magnetic field vector in the satellite’s reference frame. By combining the measured data with the known ephemeris of the satellite, the satellite–Sun vector and the magnetic field orientation can be reconstructed. The orientation is expressed using quaternions, representing the rotation from the internal reference system of the satellite to the selected reference system. The proposed system demonstrates the ability to accurately determine the orientation of a CubeSat using only two sensors, making it suitable for installations where more complex and expensive instruments are impractical. Additionally, the paper presents a mathematical model of a low-cost CubeSat orientation system and a hardware implementation of the sensor. The technology, using solar and magnetic sensors, provides a reliable and affordable solution for CubeSat navigation, supporting the increasing sophistication of miniature payloads and enabling accurate satellite positioning in space missions. CubeSat satellite orientation solar sensors magnetic sensors attitude determination satellite–Sun vector Chemical technology Abu-Alim Ayazbay verfasserin aut Dimitri Galayko verfasserin aut Gani Balbayev verfasserin aut Kuanysh Alipbayev verfasserin aut In Sensors MDPI AG, 2003 23(2023), 14, p 6388 (DE-627)331640910 (DE-600)2052857-7 14248220 nnns volume:23 year:2023 number:14, p 6388 https://doi.org/10.3390/s23146388 kostenfrei https://doaj.org/article/1b5660a80a214375ae79f1e789bef870 kostenfrei https://www.mdpi.com/1424-8220/23/14/6388 kostenfrei https://doaj.org/toc/1424-8220 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_206 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2005 GBV_ILN_2009 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2111 GBV_ILN_2507 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 23 2023 14, p 6388
language	English
source	In Sensors 23(2023), 14, p 6388 volume:23 year:2023 number:14, p 6388
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callnumber-first	T - Technology
author	Yerkebulan Nurgizat
spellingShingle	Yerkebulan Nurgizat misc TP1-1185 misc CubeSat misc satellite orientation misc solar sensors misc magnetic sensors misc attitude determination misc satellite–Sun vector misc Chemical technology Low-Cost Orientation Determination System for CubeSat Based Solely on Solar and Magnetic Sensors
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topic_title	TP1-1185 Low-Cost Orientation Determination System for CubeSat Based Solely on Solar and Magnetic Sensors CubeSat satellite orientation solar sensors magnetic sensors attitude determination satellite–Sun vector
topic	misc TP1-1185 misc CubeSat misc satellite orientation misc solar sensors misc magnetic sensors misc attitude determination misc satellite–Sun vector misc Chemical technology
topic_unstemmed	misc TP1-1185 misc CubeSat misc satellite orientation misc solar sensors misc magnetic sensors misc attitude determination misc satellite–Sun vector misc Chemical technology
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title	Low-Cost Orientation Determination System for CubeSat Based Solely on Solar and Magnetic Sensors
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title_full	Low-Cost Orientation Determination System for CubeSat Based Solely on Solar and Magnetic Sensors
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title_sort	low-cost orientation determination system for cubesat based solely on solar and magnetic sensors
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title_auth	Low-Cost Orientation Determination System for CubeSat Based Solely on Solar and Magnetic Sensors
abstract	CubeSats require accurate determination of their orientation relative to the Sun, Earth, and other celestial bodies to operate successfully and collect scientific data. This paper presents an orientation system based on solar and magnetic sensors that offers a cost-effective and reliable solution for CubeSat navigation. Solar sensors analyze the illumination on each face to measure the satellite’s orientation relative to the Sun, while magnetic sensors determine the Earth’s magnetic field vector in the satellite’s reference frame. By combining the measured data with the known ephemeris of the satellite, the satellite–Sun vector and the magnetic field orientation can be reconstructed. The orientation is expressed using quaternions, representing the rotation from the internal reference system of the satellite to the selected reference system. The proposed system demonstrates the ability to accurately determine the orientation of a CubeSat using only two sensors, making it suitable for installations where more complex and expensive instruments are impractical. Additionally, the paper presents a mathematical model of a low-cost CubeSat orientation system and a hardware implementation of the sensor. The technology, using solar and magnetic sensors, provides a reliable and affordable solution for CubeSat navigation, supporting the increasing sophistication of miniature payloads and enabling accurate satellite positioning in space missions.
abstractGer	CubeSats require accurate determination of their orientation relative to the Sun, Earth, and other celestial bodies to operate successfully and collect scientific data. This paper presents an orientation system based on solar and magnetic sensors that offers a cost-effective and reliable solution for CubeSat navigation. Solar sensors analyze the illumination on each face to measure the satellite’s orientation relative to the Sun, while magnetic sensors determine the Earth’s magnetic field vector in the satellite’s reference frame. By combining the measured data with the known ephemeris of the satellite, the satellite–Sun vector and the magnetic field orientation can be reconstructed. The orientation is expressed using quaternions, representing the rotation from the internal reference system of the satellite to the selected reference system. The proposed system demonstrates the ability to accurately determine the orientation of a CubeSat using only two sensors, making it suitable for installations where more complex and expensive instruments are impractical. Additionally, the paper presents a mathematical model of a low-cost CubeSat orientation system and a hardware implementation of the sensor. The technology, using solar and magnetic sensors, provides a reliable and affordable solution for CubeSat navigation, supporting the increasing sophistication of miniature payloads and enabling accurate satellite positioning in space missions.
abstract_unstemmed	CubeSats require accurate determination of their orientation relative to the Sun, Earth, and other celestial bodies to operate successfully and collect scientific data. This paper presents an orientation system based on solar and magnetic sensors that offers a cost-effective and reliable solution for CubeSat navigation. Solar sensors analyze the illumination on each face to measure the satellite’s orientation relative to the Sun, while magnetic sensors determine the Earth’s magnetic field vector in the satellite’s reference frame. By combining the measured data with the known ephemeris of the satellite, the satellite–Sun vector and the magnetic field orientation can be reconstructed. The orientation is expressed using quaternions, representing the rotation from the internal reference system of the satellite to the selected reference system. The proposed system demonstrates the ability to accurately determine the orientation of a CubeSat using only two sensors, making it suitable for installations where more complex and expensive instruments are impractical. Additionally, the paper presents a mathematical model of a low-cost CubeSat orientation system and a hardware implementation of the sensor. The technology, using solar and magnetic sensors, provides a reliable and affordable solution for CubeSat navigation, supporting the increasing sophistication of miniature payloads and enabling accurate satellite positioning in space missions.
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title_short	Low-Cost Orientation Determination System for CubeSat Based Solely on Solar and Magnetic Sensors
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up_date	2024-07-03T19:38:17.022Z
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Low-Cost Orientation Determination System for CubeSat Based Solely on Solar and Magnetic Sensors

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