Attitude Control Development of the AGU Remote Innovative CubeSat Alert System -2

AGU Remote Innovative CubeSat Alert system -2 (ARICA-2) is the 2U CubeSat for demonstrating the real-time alert system of transient astronomical sources using commercial satellite network services. 1U CubeSat ARICA, which has same mission goals as ARICA-2, was launched in 2021. However, it has never successfully transmitted or received data to date. The lack of attitude control, power balance issues and short communication time with commercial satellites are considered as the causes of the defects. With these considerations, we started to develop ARICA-2 as a re-challenging mission of ARICA. Since attitude control is essential for satellite operation and mission accomplishment, ARICA-2 uses magnetic torquers for attitude control. We are currently building a system that will be able to determine the position of the satellite using 9-axis sensors, sun sensors, infrared sensors, and GPS, and to control the attitude using 3-axis magnetic torquers. Our satellite uses magnetic torquer for passive magnetic attitude control. We will present an overview of ARICA-2 and its attitude control system, as well as the components used and the operational modes being considered.

Publication Details

Journal
Digital Commons - USU (Utah State University)
Published
2024-08-04
Primary Topic
Spacecraft Design and Technology
Type
article
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article

Attitude Control Development of the AGU Remote Innovative CubeSat Alert System -2

Digital Commons - USU (Utah State University)
Spacecraft Design and Technology
article

Attitude Control Development of the AGU Remote Innovative CubeSat Alert System -2

article en

Abstract

AGU Remote Innovative CubeSat Alert system -2 (ARICA-2) is the 2U CubeSat for demonstrating the real-time alert system of transient astronomical sources using commercial satellite network services. 1U CubeSat ARICA, which has same mission goals as ARICA-2, was launched in 2021. However, it has never successfully transmitted or received data to date. The lack of attitude control, power balance issues and short communication time with commercial satellites are considered as the causes of the defects. With these considerations, we started to develop ARICA-2 as a re-challenging mission of ARICA. Since attitude control is essential for satellite operation and mission accomplishment, ARICA-2 uses magnetic torquers for attitude control. We are currently building a system that will be able to determine the position of the satellite using 9-axis sensors, sun sensors, infrared sensors, and GPS, and to control the attitude using 3-axis magnetic torquers. Our satellite uses magnetic torquer for passive magnetic attitude control. We will present an overview of ARICA-2 and its attitude control system, as well as the components used and the operational modes being considered.

Digital Commons - USU (Utah State University)
Openalex Percentile: Top 28%
Spacecraft Design and Technology
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Attitude Control Development of the AGU Remote Innovative CubeSat Alert System -2 · Digital Commons - USU (Utah State University) (2024) | TGRS Research Map | TGRS