A Comparative Analysis of a Novel Stability Criterion Versus the Generalized Nyquist Stability Criterion in More-Electric Aircraft Cascaded System

Zixiao Xu, Yufeng Wang, Hongwei Zhao, Weilin Li

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

As the power demands of onboard electrical equipment continue to rise, more-electric aircraft (MEA) power supply systems require an increasing number of converters to provide controlled voltage or frequency power. However, the extensive use of converters and their interaction with generators lead to instability in AC bus voltage, posing potential safety risks to aircraft. Therefore, analyzing the stability of cascaded systems consisting of generators and converters is crucial. This paper proposes a novel stability criterion based on the Gershgorin circle theorem to accurately assess the AC output voltage stability of MEA cascaded systems. Compared to the generalized Nyquist stability criterion (GNSC), the proposed method aligns more closely with the actual stability state of aircraft systems and allows for the pre-design customization of stability margins, providing valuable guidance for aircraft system design. Finally, simulations validate the advantages and accuracy of this method through comparative analysis.

Original languageEnglish
Title of host publication2024 5th International Conference on Power Engineering, ICPE 2024
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages427-432
Number of pages6
ISBN (Electronic)9798331531140
DOIs
StatePublished - 2024
Event5th International Conference on Power Engineering, ICPE 2024 - Shanghai, China
Duration: 13 Dec 202415 Dec 2024

Publication series

Name2024 5th International Conference on Power Engineering, ICPE 2024

Conference

Conference5th International Conference on Power Engineering, ICPE 2024
Country/TerritoryChina
CityShanghai
Period13/12/2415/12/24

Keywords

  • cascaded system
  • Gershgorin circle theorem
  • impedance modeling
  • more-electric aircraft
  • stability criterion

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