2023
DOI: 10.1177/09544100231162662
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Optimal hybrid Coulomb control for on-track rendezvous and docking of spacecraft

Abstract: This paper investigates the dynamics of on-track rendezvous and docking of two spacecraft, and stabilization using hybrid Coulomb control. Modeling electrostatic forces and torques for control of complex spacecraft geometries like cylinders is challenging. Point mass assumption of the spacecraft that disregards the chaser dynamics will lead to errors in force estimation during the terminal docking phase, resulting in a mission failure. This paper uses the effective sphere method to model Coulomb interactions b… Show more

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