{
  "abstract": "The complex and nonlinear load characteristics of Hall thrusters remain a key challenge in the design of propulsion power-supply output stages. In existing power-supply simu-lations for electric propulsion systems, the Hall thruster is often simplified as a fixed im-pedance or a prescribed current source, which makes it difficult to capture the real-time interaction between the power-supply output stage and the thruster discharge process. To address this issue, this study encapsulates a one-dimensional discharge model as an externally callable thruster slave and proposes a HallThruster.jl-Saber-Simulink co-simu-lation method. The proposed method enables synchronized closed-loop exchange be-tween the power-port voltage Vcmd and the thruster discharge current Iout . The results show that the discharge current under the co-simulation condition exhibits a sustained low-frequency response at approximately 11 kHz. Compared with a fixed-voltage standalone simulation, the co-simulation shows observable differences in port waveforms, spectral characteristics, and internal field distributions. This method provides a co-simu-lation basis for realistic load analysis of propulsion power supplies and subsequent stress evaluation of key components.",
  "abstract_shown": true,
  "affiliations": [],
  "article_type": null,
  "arxiv": "2606.28743",
  "author_total": 7,
  "authors": [
    {
      "name": "Zirui Fan"
    },
    {
      "name": "Yinjian Zhao"
    },
    {
      "name": "Jingjing Li"
    },
    {
      "name": "Yingying Tian"
    },
    {
      "name": "Leilei Shi"
    },
    {
      "name": "Suliang Wu"
    },
    {
      "name": "Liqiu Wei"
    }
  ],
  "bibtex": "https://research.draconitic.com/paper/dfy0n11236tme.bib",
  "cited_by": 0,
  "doi": "10.48550/arxiv.2606.28743",
  "fulltext_url": null,
  "id": "dfy0n11236tme",
  "issns": [],
  "landing_url": "https://arxiv.org/abs/2606.28743",
  "language": null,
  "licence": "LicenseRef-arXiv-nonexclusive-1.0",
  "licence_label": "arXiv licence",
  "licence_source": "article",
  "licence_url": "http://arxiv.org/licenses/nonexclusive-distrib/1.0/",
  "metadata_licence": "CC0-1.0",
  "native_subjects": [
    [
      "arxiv",
      "physics.plasm-ph"
    ]
  ],
  "openalex": null,
  "pdf_url": "https://arxiv.org/pdf/2606.28743",
  "pmcid": null,
  "pmid": null,
  "published": "2026-06-27",
  "publisher": null,
  "ris": "https://research.draconitic.com/paper/dfy0n11236tme.ris",
  "sources": [
    {
      "first_seen": "2026-10-30T12:20:12Z",
      "native_id": "2606.28743",
      "source": "arxiv",
      "url": "https://arxiv.org/abs/2606.28743"
    }
  ],
  "subjects": [
    {
      "field": "physics",
      "origin": "arxiv:physics.plasm-ph",
      "subfield": "plasma"
    }
  ],
  "title": "Simulation Study of Coupling Effects Between a Hall Thruster and a Power Processing Unit",
  "title_text": "Simulation Study of Coupling Effects Between a Hall Thruster and a Power Processing Unit",
  "type": "preprint",
  "updated_at": "2026-10-30T12:20:12Z",
  "url": "https://research.draconitic.com/paper/dfy0n11236tme",
  "venue": "arXiv",
  "versions": [
    {
      "doi": "10.3390/aerospace13080687",
      "pid": null,
      "relation": "published-as",
      "title": null,
      "venue": null
    }
  ]
}