Control Allocation for Hybrid Coulomb Spacecraft Formations
Optimization and Control
2022-07-14 v1 Systems and Control
Systems and Control
Abstract
This paper proposes an algorithm which can be used in hybrid Coulomb spacecraft formations to minimize propellant by maximizing the amount of force that is generated by Coulomb forces. This problem is difficult due to the nonlinearities inherent in Coulomb's law. The problem is posed as a series of matrix rank minimization problems which can be solved efficiently using a trace heuristic. A numerical example is provided which shows that, using the proposed control allocation algorithm, the amount of propellant required to perform a reconfiguration maneuver is reduced by approximately 40% compared to using solely thrusters.
Keywords
Cite
@article{arxiv.2207.05881,
title = {Control Allocation for Hybrid Coulomb Spacecraft Formations},
author = {Adam M Tahir},
journal= {arXiv preprint arXiv:2207.05881},
year = {2022}
}