What is it about?
An electrostatically charged spacecraft is subject to the Lorentz forces and torques when moving in the geomagnetic field. We propose a coupled relative orbit and attitude control scheme by using the hybrid Lorentz torques, the magnetic torques, the Lorentz forces, and the thruster-generated control forces.
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This page is a summary of: Coupled Relative Orbit and Attitude Control Augmented by the Geomagnetic Lorentz Propulsions, Journal of Guidance Control and Dynamics, February 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g005212.
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