Calculating electric power generated by 3U CubeSat's photoconverters depending the orbit and orientation parameters

V. N. Gorev; V. Yu Prokopiev; Yu M. Prokopiev; L. D. Sinitsina; A. A. Sidorchuk

doi:10.1088/1757-899X/537/2/022079

Calculating electric power generated by 3U CubeSat's photoconverters depending the orbit and orientation parameters

V. N. Gorev, V. Yu Prokopiev, Yu M. Prokopiev, L. D. Sinitsina, A. A. Sidorchuk

Результат исследования: Научные публикации в периодических изданиях › статья по материалам конференции

1 Цитирования (Scopus)

Аннотация

The paper describes a computational program developed in MatLab Simulink, that performs calculation of electric power generated by photoconverters for various missions of nanosatellites in low Earth orbit (LEO). Electric power generated by nanosatellite's solar panels was estimated for polar LEO of 450 km altitude for two versions of the satellite's static orientation. The results show how orientation maneuver at the Earth's surface point affects power generated by the satellite's solar panels.

Язык оригинала	английский
Номер статьи	022079
Число страниц	7
Журнал	IOP Conference Series: Materials Science and Engineering
Том	537
Номер выпуска	2
DOI	https://doi.org/10.1088/1757-899X/537/2/022079
Состояние	Опубликовано - 25 июн 2019
Событие	International Workshop on Advanced Technologies in Material Science, Mechanical and Automation Engineering - MIP: Engineering-2019 - Krasnoyarsk, Российская Федерация Продолжительность: 4 апр 2019 → 6 апр 2019

Доступ к документу

10.1088/1757-899X/537/2/022079

Link to publication in Scopus

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Цитировать

Gorev, V. N., Prokopiev, V. Y., Prokopiev, Y. M., Sinitsina, L. D., & Sidorchuk, A. A. (2019). Calculating electric power generated by 3U CubeSat's photoconverters depending the orbit and orientation parameters. IOP Conference Series: Materials Science and Engineering, 537(2), [022079]. https://doi.org/10.1088/1757-899X/537/2/022079

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abstract = "The paper describes a computational program developed in MatLab Simulink, that performs calculation of electric power generated by photoconverters for various missions of nanosatellites in low Earth orbit (LEO). Electric power generated by nanosatellite's solar panels was estimated for polar LEO of 450 km altitude for two versions of the satellite's static orientation. The results show how orientation maneuver at the Earth's surface point affects power generated by the satellite's solar panels.",

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Calculating electric power generated by 3U CubeSat's photoconverters depending the orbit and orientation parameters. / Gorev, V. N.; Prokopiev, V. Yu ; Prokopiev, Yu M.; Sinitsina, L. D.; Sidorchuk, A. A.

В: IOP Conference Series: Materials Science and Engineering, Том 537, № 2, 022079, 25.06.2019.

Результат исследования: Научные публикации в периодических изданиях › статья по материалам конференции

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