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Model Predictive Approach for Detumbling an Underactuated Satellite
This research proposes an innovative approach to detumble satellites' triple-axis angular velocities with only one single-axis magnetic torquer.
Nonlinear Model Predictive Detumbling of Small Satellites with a Single-axis Magnetorquer
Magnetic torquers have been extensively investigated for momentum management of spacecraft with momentum wheels and for nutation damping of spin satellites, momentum-biased, and dual-spin satellites.
Pulse Width Modulation Method Applied to Nonlinear Model Predictive Control on an Under-actuated Small Satellite
Among various satellite actuators, magnetic torquers have been widely equipped for stabilization and attitude control of small satellites.
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