Time-Varying Model Predictive Attitude Control for Magnetically Actuated Dual-Spin Satellites
Robert D. Halverson, Ryan J. Caverly

TL;DR
This paper develops and compares time-varying model predictive control strategies for magnetically actuated dual-spin CubeSats, optimizing attitude control with minimal actuation and computational effort.
Contribution
It introduces a nonlinear prediction-based MPC approach for dual-spin satellite attitude control, outperforming linear methods in constraint satisfaction and actuation minimization.
Findings
Nonlinear prediction policy achieves better constraint adherence.
Nonlinear MPC reduces control effort compared to linear methods.
The proposed approach is computationally efficient for onboard implementation.
Abstract
Attitude control hardware for small satellites is often limited in power and space availability given the importance of the science instruments they exist to transport. To mitigate this, a dual-spin stabilized satellite actuated via magnetic torque rods reduces the space and power required of the attitude control system, but may require advanced control policies. This paper explores the attitude control of a magnetically actuated dual-spin stabilized CubeSat with model predictive control using time-varying prediction dynamics. An inertial pointing objective is used as a representative mission, where the satellite is able to deviate from its nominal orientation within some allowable amount. Three time-varying MPC policies are developed and compared to ensure the system does not violate constraints while minimizing control effort. These policies include a prediction model that accounts…
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Taxonomy
TopicsSpace Satellite Systems and Control · Inertial Sensor and Navigation · Spacecraft Design and Technology
