Standard

Calculating electric power generated by 3U CubeSat's photoconverters depending the orbit and orientation parameters. / Gorev, V. N.; Prokopiev, V. Yu; Prokopiev, Yu M. и др.

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

Результаты исследований: Научные публикации в периодических изданиях › статья по материалам конференции › Рецензирование

Harvard

Gorev, VN, Prokopiev, VY, Prokopiev, YM, Sinitsina, LD & Sidorchuk, AA 2019, 'Calculating electric power generated by 3U CubeSat's photoconverters depending the orbit and orientation parameters', IOP Conference Series: Materials Science and Engineering, Том. 537, № 2, 022079. https://doi.org/10.1088/1757-899X/537/2/022079

APA

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

Vancouver

Gorev VN, Prokopiev VY, Prokopiev YM, Sinitsina LD, Sidorchuk AA. Calculating electric power generated by 3U CubeSat's photoconverters depending the orbit and orientation parameters. IOP Conference Series: Materials Science and Engineering. 2019 июнь 25;537(2):022079. doi: 10.1088/1757-899X/537/2/022079

Author

Gorev, V. N. ; Prokopiev, V. Yu ; Prokopiev, Yu M. и др. / Calculating electric power generated by 3U CubeSat's photoconverters depending the orbit and orientation parameters. в: IOP Conference Series: Materials Science and Engineering. 2019 ; Том 537, № 2.

BibTeX

@article{938804a8bc1947af9785ad7f802b90c8,
title = "Calculating electric power generated by 3U CubeSat's photoconverters depending the orbit and orientation parameters",
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.",
author = "Gorev, {V. N.} and Prokopiev, {V. Yu} and Prokopiev, {Yu M.} and Sinitsina, {L. D.} and Sidorchuk, {A. A.}",
year = "2019",
month = jun,
day = "25",
doi = "10.1088/1757-899X/537/2/022079",
language = "English",
volume = "537",
journal = "IOP Conference Series: Materials Science and Engineering",
issn = "1757-8981",
publisher = "IOP Publishing Ltd.",
number = "2",
note = "International Workshop on Advanced Technologies in Material Science, Mechanical and Automation Engineering - MIP: Engineering-2019 ; Conference date: 04-04-2019 Through 06-04-2019",

}

RIS

TY - JOUR

T1 - Calculating electric power generated by 3U CubeSat's photoconverters depending the orbit and orientation parameters

AU - Gorev, V. N.

AU - Prokopiev, V. Yu

AU - Prokopiev, Yu M.

AU - Sinitsina, L. D.

AU - Sidorchuk, A. A.

PY - 2019/6/25

Y1 - 2019/6/25

N2 - 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.

AB - 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.

UR - http://www.scopus.com/inward/record.url?scp=85068892936&partnerID=8YFLogxK

U2 - 10.1088/1757-899X/537/2/022079

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

M3 - Conference article

AN - SCOPUS:85068892936

VL - 537

JO - IOP Conference Series: Materials Science and Engineering

JF - IOP Conference Series: Materials Science and Engineering

SN - 1757-8981

IS - 2

M1 - 022079

T2 - International Workshop on Advanced Technologies in Material Science, Mechanical and Automation Engineering - MIP: Engineering-2019

Y2 - 4 April 2019 through 6 April 2019

ER -

ID: 20851325