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High-precision CubeSat sun sensor coupled with infrared Earth horizon detector. / Pelemeshko, Anatoly; Kolesnikova, Alena; Melkov, Alexander et al.

In: IOP Conference Series: Materials Science and Engineering, Vol. 734, No. 1, 012012, 29.01.2020.

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Pelemeshko A, Kolesnikova A, Melkov A, Prokopyev V, Zadorozhny A. High-precision CubeSat sun sensor coupled with infrared Earth horizon detector. IOP Conference Series: Materials Science and Engineering. 2020 Jan 29;734(1):012012. doi: 10.1088/1757-899X/734/1/012012

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Pelemeshko, Anatoly ; Kolesnikova, Alena ; Melkov, Alexander et al. / High-precision CubeSat sun sensor coupled with infrared Earth horizon detector. In: IOP Conference Series: Materials Science and Engineering. 2020 ; Vol. 734, No. 1.

BibTeX

@article{d65a430a761940bb9f10564a0055694a,
title = "High-precision CubeSat sun sensor coupled with infrared Earth horizon detector",
abstract = "This paper presents a novel miniature module of orientation sensors for CubeSat nanosatellites. A high-precision sun sensor and a detector of the Earth horizon are located in one small module body. A two-axis digital sun sensor built into the orientation module is based on the registration of the sunspot formed on the matrix CMOS image sensor when the sun's rays pass through a pinhole in the front mask. A commercially available miniature array of infrared thermometers is used as the Earth horizon sensor. The paper is mainly devoted to the development of the sun sensor. For laboratory tests, a prototype of the orientation module was developed. Laboratory tests and sun sensor calibration confirmed the sun sensor field of view of 120° and made it possible to determine its angular resolution of ±0.015°. The final accuracy of determining the direction to the Sun by the sensor that was calibrated using the existing experimental setup is ±0.15° with 95% confidence. It is possible to improve the accuracy of the sun sensor by improving the experimental setup for its calibration.",
author = "Anatoly Pelemeshko and Alena Kolesnikova and Alexander Melkov and Vitaliy Prokopyev and Alexander Zadorozhny",
year = "2020",
month = jan,
day = "29",
doi = "10.1088/1757-899X/734/1/012012",
language = "English",
volume = "734",
journal = "IOP Conference Series: Materials Science and Engineering",
issn = "1757-8981",
publisher = "IOP Publishing Ltd.",
number = "1",
note = "2nd International Scientific Conference on Advanced Technologies in Aerospace, Mechanical and Automation Engineering, MIST: Aerospace 2019 ; Conference date: 18-11-2019 Through 21-11-2019",

}

RIS

TY - JOUR

T1 - High-precision CubeSat sun sensor coupled with infrared Earth horizon detector

AU - Pelemeshko, Anatoly

AU - Kolesnikova, Alena

AU - Melkov, Alexander

AU - Prokopyev, Vitaliy

AU - Zadorozhny, Alexander

PY - 2020/1/29

Y1 - 2020/1/29

N2 - This paper presents a novel miniature module of orientation sensors for CubeSat nanosatellites. A high-precision sun sensor and a detector of the Earth horizon are located in one small module body. A two-axis digital sun sensor built into the orientation module is based on the registration of the sunspot formed on the matrix CMOS image sensor when the sun's rays pass through a pinhole in the front mask. A commercially available miniature array of infrared thermometers is used as the Earth horizon sensor. The paper is mainly devoted to the development of the sun sensor. For laboratory tests, a prototype of the orientation module was developed. Laboratory tests and sun sensor calibration confirmed the sun sensor field of view of 120° and made it possible to determine its angular resolution of ±0.015°. The final accuracy of determining the direction to the Sun by the sensor that was calibrated using the existing experimental setup is ±0.15° with 95% confidence. It is possible to improve the accuracy of the sun sensor by improving the experimental setup for its calibration.

AB - This paper presents a novel miniature module of orientation sensors for CubeSat nanosatellites. A high-precision sun sensor and a detector of the Earth horizon are located in one small module body. A two-axis digital sun sensor built into the orientation module is based on the registration of the sunspot formed on the matrix CMOS image sensor when the sun's rays pass through a pinhole in the front mask. A commercially available miniature array of infrared thermometers is used as the Earth horizon sensor. The paper is mainly devoted to the development of the sun sensor. For laboratory tests, a prototype of the orientation module was developed. Laboratory tests and sun sensor calibration confirmed the sun sensor field of view of 120° and made it possible to determine its angular resolution of ±0.015°. The final accuracy of determining the direction to the Sun by the sensor that was calibrated using the existing experimental setup is ±0.15° with 95% confidence. It is possible to improve the accuracy of the sun sensor by improving the experimental setup for its calibration.

UR - http://www.scopus.com/inward/record.url?scp=85079676168&partnerID=8YFLogxK

U2 - 10.1088/1757-899X/734/1/012012

DO - 10.1088/1757-899X/734/1/012012

M3 - Conference article

AN - SCOPUS:85079676168

VL - 734

JO - IOP Conference Series: Materials Science and Engineering

JF - IOP Conference Series: Materials Science and Engineering

SN - 1757-8981

IS - 1

M1 - 012012

T2 - 2nd International Scientific Conference on Advanced Technologies in Aerospace, Mechanical and Automation Engineering, MIST: Aerospace 2019

Y2 - 18 November 2019 through 21 November 2019

ER -

ID: 23593008