Abstract:This paper carries out an iterative computer simulation approach to tune B-dot detumbling and 3-axis PD attitude controller gains for magnetically-actuated CubeSats. The effect of different gains for 1U and 2U CubeSats are investigated along with the effect on PD control performance when nonidealities are included in the simulator such as Sun sensor noise, magnetometer sensor noise, rate gyroscope sensor noise and CubeSat eclipse conditions (when the Satellite cannot estimate its attitude using Sun sensors due… Show more
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