Evaluation of Sun Position and Angular Rates Using the Photovoltaic Conversion System for On-Board Functions in an Artificial Satellite

Despite metrological limitations, photovoltaic (PV) cells can be used as orbital sensors in order to evaluate sunlight incidence angles, sun position, and angular rates with acceptable accuracy for several on-board functions in an artificial satellite. This information is assessed using short-circuit currents and open-circuit voltages of PV cells, which can be measured and acquired from the power regulator operation. This article presents the feasibility of the use of PV conversion systems in the evaluation of sun position and angular rates for on-board functions in a parallelepiped-shaped prismatic artificial satellite.

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Publication Details

Journal
IEEE Transactions on Aerospace and Electronic Systems
Published
2024-08-05
DOI
https://doi.org/10.1109/taes.2024.3438088
Primary Topic
Spacecraft Design and Technology
Type
article
Field-Weighted Citation Impact
0.00

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article

Evaluation of Sun Position and Angular Rates Using the Photovoltaic Conversion System for On-Board Functions in an Artificial Satellite

Adrielle C. Santana, Ronilson Rocha, Jo ̃ao Carlos Vilela de Castro
1 links
IEEE Transactions on Aerospace and Electronic Systems
Spacecraft Design and Technology
article

Evaluation of Sun Position and Angular Rates Using the Photovoltaic Conversion System for On-Board Functions in an Artificial Satellite

Adrielle C. Santana, Ronilson Rocha, Jo ̃ao Carlos Vilela de Castro
article en

Abstract

Despite metrological limitations, photovoltaic (PV) cells can be used as orbital sensors in order to evaluate sunlight incidence angles, sun position, and angular rates with acceptable accuracy for several on-board functions in an artificial satellite. This information is assessed using short-circuit currents and open-circuit voltages of PV cells, which can be measured and acquired from the power regulator operation. This article presents the feasibility of the use of PV conversion systems in the evaluation of sun position and angular rates for on-board functions in a parallelepiped-shaped prismatic artificial satellite.

IEEE Transactions on Aerospace and Electronic SystemsVol. 60(6)
Universidade Federal de Ouro Preto (BR)
Fundação Gorceix, Agência Espacial Brasileira
Affordable and clean energy
Openalex Percentile: Top 81%
Spacecraft Design and Technology
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