Abstract Hall thrusters, characterized by high specific impulses and extended operational durations, are increasingly recognized as promising electric propulsion devices for long-duration missions and station keeping of cislunar satellites. However, the failure of channel wall erosion induced by sputtering remains a significant challenge, compromising the functionality and reliability of Hall thrusters. This article proposes a novel Hall thruster remaining useful life (RUL) prediction approach based on adaptive self-cognizant dynamic system (ASDS) with multiphysics modeling. First, a low-fidelity plasma discharge model and a semi-empirical sputter model are integrated to reveal the erosion mechanism and efficiently generate degradation data. Then, a state-space ASDS model, employing fully connected neural networks (FCNNs) as system modelers, is established based on the erosion mechanism and trained offline using simulation data. Upon receiving online telemetry observations, the state of health (SOH) and FCNN parameters are estimated and updated through the particle filter. The RUL and its distribution are finally predicted by forwarding SOH across different particles. Case study on SPT-100 Hall thruster validates the effectiveness of the proposed ASDS approach, which not only captures the fundamental failure mechanisms and adjusts to system variations but also provides the uncertainty of RUL as valuable prior information for thruster refueling and maintenance decision-making.
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Jiang et al. (Wed,) studied this question.
synapsesocial.com/papers/69a75c8ac6e9836116a257ea — DOI: https://doi.org/10.1115/1.4070967
Yuan Jiang
University of Illinois Urbana-Champaign
Alexandra N. Leeming
University of Illinois Urbana-Champaign
Joshua L. Rovey
University of Illinois Urbana-Champaign
Journal of Mechanical Design
University of Illinois Urbana-Champaign
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