Modeling and Simulation of Solar Power Calculations for GOES-13 & SS-1 Satellite

M. Raja¹ , Akanksha Mahawer² , Shubhangini Shrimali³ , Vijayalaxmi Matolia⁴

Section:Research Paper, Product Type: Journal-Paper
Vol.7 , Issue.2 , pp.100-103, Jun-2020

Online published on Jun 30, 2020

Copyright © M. Raja, Akanksha Mahawer, Shubhangini Shrimali, 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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Abstract :
The proposed work to calculate the orbital velocity, orbital period and efficiency for different power conditions of GOES 13 and SS 1 satellites. The Satellite Power System (SPS) is a possibility for delivering critical amounts of base-load power utilizing sunlight-based vitality as the source such as photovoltaic (PV) cell. In order to ensure that the persistent tasks of the satellite are kept up; it is basic to plan and create its capacity frameworks to meet different prerequisites of the satellites that are available in the earth orbits known as Earth orbit satellites. The satellites, which spin at an elevation over 35,000km, collectively known as Geo-synchronous satellites, which are available in the Geo-synchronous orbits. To control these sort of satellites a special asset of intensity framework is required

Key-Words / Index Term :
Current parameters, PV module, Photovoltaic cell, Power system, Solar efficiency, Time period

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