TY - GEN
T1 - A Comparative Analysis of a Novel Stability Criterion Versus the Generalized Nyquist Stability Criterion in More-Electric Aircraft Cascaded System
AU - Xu, Zixiao
AU - Wang, Yufeng
AU - Zhao, Hongwei
AU - Li, Weilin
N1 - Publisher Copyright:
© 2024 IEEE.
PY - 2024
Y1 - 2024
N2 - 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.
AB - 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.
KW - cascaded system
KW - Gershgorin circle theorem
KW - impedance modeling
KW - more-electric aircraft
KW - stability criterion
UR - http://www.scopus.com/inward/record.url?scp=105002253128&partnerID=8YFLogxK
U2 - 10.1109/ICPE64565.2024.10929341
DO - 10.1109/ICPE64565.2024.10929341
M3 - 会议稿件
AN - SCOPUS:105002253128
T3 - 2024 5th International Conference on Power Engineering, ICPE 2024
SP - 427
EP - 432
BT - 2024 5th International Conference on Power Engineering, ICPE 2024
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 5th International Conference on Power Engineering, ICPE 2024
Y2 - 13 December 2024 through 15 December 2024
ER -