The stability analysis of the aircraft electrical system with regulated buck-boost converter unit

Name: Wiphusana Chayinthu

Organization : Rajamangala University of Technology Suvarnabhumi (RUS). Department of Electrical Engineering

Email : wiphusana.c@rmutsb.ac.th

keyword: Aircraft electrical system

LCSH: Power electronics

; Stability analysis

; Buck-boost converter

Abstract: Generally, a regulated buck-boost converter unit behaves as a constant power loads. This load can corrupt the regarded system instability. Thus, stability analysis is very significant. In this paper, the eigenvalue theorem is suggested to diagnose the stability of the electric aircraft system with a regulated buckboost converter unit. The results display that the offers model can affirm the unstable point predicted to the prepared model versus an eigenvalue theorem. Good acceptance between theory and simulation can be achieved.

King Mongkut's University of Technology North Bangkok. Central Library

Address: BANGKOK

Email: library@kmutnb.ac.th

Created: 2021

Modified: 2025-12-16

Issued: 2025-12-16

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application/pdf

BibliograpyCitation : In Electrical Engineering Academic Association (Thailand), IEEE Thailand Section, and College of Engineering. Rangsit University. The 2021 9th International Electrical Engineering Congress (iEECON 2021) (P00697). Pathum Thani : Rangsit University, 2021

eng

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