Attitude Control and Determination System (ACDS) for a CubeSat: B-dot detumbling and 3-axis quaternion PID pointing, with IGRF-13 geomagnetic and SGP4 orbit models.
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Sep 5, 2026 - C
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magnetorquer
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To determine the physical parameters, model and mathematical representation of a magnetorquer.
control model space satellite modeling mathematical-expressions cubesat attitude mathematical-modelling actuator gnc adcs attitude-control magnetorquer active-actuator
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Updated
May 30, 2024
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