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Design a Solar Power system for Earth orbiting satellite
M. Raja1 , Vijayalaxmi Matolia2
Section:Research Paper, Product Type: Journal-Paper
Vol.7 ,
Issue.1 , pp.53-56, Feb-2020
Online published on Feb 28, 2020
Copyright © M. Raja, Vijayalaxmi Matolia . This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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IEEE Style Citation: M. Raja, Vijayalaxmi Matolia, “Design a Solar Power system for Earth orbiting satellite,” International Journal of Scientific Research in Mathematical and Statistical Sciences, Vol.7, Issue.1, pp.53-56, 2020.
MLA Style Citation: M. Raja, Vijayalaxmi Matolia "Design a Solar Power system for Earth orbiting satellite." International Journal of Scientific Research in Mathematical and Statistical Sciences 7.1 (2020): 53-56.
APA Style Citation: M. Raja, Vijayalaxmi Matolia, (2020). Design a Solar Power system for Earth orbiting satellite. International Journal of Scientific Research in Mathematical and Statistical Sciences, 7(1), 53-56.
BibTex Style Citation:
@article{Raja_2020,
author = {M. Raja, Vijayalaxmi Matolia},
title = {Design a Solar Power system for Earth orbiting satellite},
journal = {International Journal of Scientific Research in Mathematical and Statistical Sciences},
issue_date = {2 2020},
volume = {7},
Issue = {1},
month = {2},
year = {2020},
issn = {2347-2693},
pages = {53-56},
url = {https://www.isroset.org/journal/IJSRMSS/full_paper_view.php?paper_id=1742},
publisher = {IJCSE, Indore, INDIA},
}
RIS Style Citation:
TY - JOUR
UR - https://www.isroset.org/journal/IJSRMSS/full_paper_view.php?paper_id=1742
TI - Design a Solar Power system for Earth orbiting satellite
T2 - International Journal of Scientific Research in Mathematical and Statistical Sciences
AU - M. Raja, Vijayalaxmi Matolia
PY - 2020
DA - 2020/02/28
PB - IJCSE, Indore, INDIA
SP - 53-56
IS - 1
VL - 7
SN - 2347-2693
ER -
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Abstract :
A satellite is an object in space that orbits or circles around a bigger object in space. The satellite has four parts – a power system (which could be solar or nuclear), a way to control its attitude, an antenna to transmit and receive information and a payload to collect information such as a camera or a particle detector. The Satellites has used for some applications, such as communicate and interchanges weather forecast, navigation, earth/space perception, and logical examinations. To calculates the efficiency of solar cell using MATLAB Environment.
Key-Words / Index Term :
LEO, Photovoltaic Cell, Ultraviolet Degradation, DC to AC Convertion
References :
[1] Mukund R. Patel, “Spacecraft Power Systems”, CRC Press, 2004.
[2] G. N. Tiwari, Solar Energy, Narosa Publishing House, 2013.
[3] C. M. Mackenzie, Solar Power Systems for satellites in Near-Earth Orbit.
[4] Craig S. Clarke, Alejandro Lopez Mazarias, “Power system challenges for small satellite missions”.
[5] Frohlich, R. C., Contemporary measures of the solar constant: The solar output and its variation, Colorado Associated University Press, Boulder, CO, 1977.
[6] V Parameswaram, Mateen Khan, M Pathan, “Solar power satellite and microwave transmission from space to Earth for generating Electrical power”.
[7] M Maqsood and M Nauman Nasir, Wireless electricity (Power) transmission using solar based power satellite technology.
[8] G. D. Rai, “Solar Energy” Utilisation, Khana Publishers, 2005.
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