A nonlinear-propagation MPC policy outperformed orbital-scheduling and linear-propagation policies for magnetically actuated dual-spin CubeSat attitude control in simulation.
Applications of a Single-Vector Inertial Aiding Scheme for 3U CubeSats,
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Time-Varying Model Predictive Attitude Control for Magnetically Actuated Dual-Spin Satellites
A nonlinear-propagation MPC policy outperformed orbital-scheduling and linear-propagation policies for magnetically actuated dual-spin CubeSat attitude control in simulation.