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Coarse Sun Acquisition for Micro Satellites Using only Sun Sensors

摘要


This paper formulated an algorithm for coarse sun acquisition with sun sensors, specifically for the case of microsatellites. In contrast to a larger satellite, a microsatellite has limited power and thus generally lacks a functional attitude estimator in the launching stage. After the detumbling stage, the microsatellite must acquire the sun's position as soon as possible using the designated algorithm. This paper presents the development of an algorithm for the blind search of the sun's position in the case where only coarse sun sensors are used. We also considered the case of a solar eclipse. A model with 6 degrees of freedom was developed for a Monte Carlo simulation to verify the developed algorithm. The developed algorithm can be used in any microsatellite with similar equipment.

參考文獻


Rocha R, and Rodrigues L, “Photovoltaic Panels as Attitude Sensors for Artificial Satellites,” IEEE Aerospace and Electronic Systems Magazine, 31. pp. 14-23, 2016
Lü X et al., “Sun sensor using a nanosatellites solar panels by means of time division multiplexing,” IET Science, Measurement & Technology, Vol. 11, No. 4, 2017, pp. 489-494.
Guy M, Young T, “Creating Eclipses: Using Scale Models to Explore How Eclipses Happen,” Science Activities, Vol. 47, 2010, pp. 75-82.
Sumanth RM, “Computation of Eclipse Time for Low-Earth Orbiting Small Satellites,” International Journal of Aviation, aeronautics, and Aerospace, Vol. 6, Iss. 5, Article 15, 2019.
Malcolm DS, “Uniform Attitude Probability Distributions,” the Journal of the Astronautical Sciences, Vol. 51, No. 4, 2003, pp. 451-475.

被引用紀錄


Sedelnikov, A. (2022). Algorithm for Restoring Information of Current from Solar Panels of a Small Satellite Prototype "Aist" with Help of Normality Conditions. Journal of Aeronautics, Astronautics and Aviation, 54(1), 67-75. https://doi.org/10.6125/JoAAA.202203_54(1).05

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