TY - JOUR
T1 - Large-Signal Stabilization of the Voltage Source Rectifier-Fed More-Electric Aircraft Power System
AU - Jiang, Wentao
AU - Fan, Enquan
AU - Li, Xiangke
AU - Dong, Chaoyu
AU - Wang, Zhishuang
AU - Wang, Rui
AU - Ma, Rui
AU - Zhou, Yang
N1 - Publisher Copyright:
© 2015 IEEE.
PY - 2025
Y1 - 2025
N2 - With the increasing penetration of power electronic devices in the power system of the more-electric aircraft (MEA), the stabilization of the onboard power system meets a great challenge. To alleviate the issue, in this article, a fixed-time sliding mode controller (FTSMC) is proposed for a voltage source rectifier (VSR) interfaced MEA power system. The adoption of the fixed-time disturbance observer (FTDO) technique allows the disturbances to be estimated within a fixed time. As a result, the system's dynamic performance is improved. The proposed FTSMC guarantees a fixed-time convergence of the dc bus voltage to its expectation. In addition, a reduced-order model of the VSR is derived to simplify the design of the proposed control strategy. A strict stability analysis is carried out to show the large-signal stability of the regulated system, and some simulation, hardware-in-the-loop (HIL) test, and hardware experimental results are demonstrated to validate the effectiveness of the proposed control strategy.
AB - With the increasing penetration of power electronic devices in the power system of the more-electric aircraft (MEA), the stabilization of the onboard power system meets a great challenge. To alleviate the issue, in this article, a fixed-time sliding mode controller (FTSMC) is proposed for a voltage source rectifier (VSR) interfaced MEA power system. The adoption of the fixed-time disturbance observer (FTDO) technique allows the disturbances to be estimated within a fixed time. As a result, the system's dynamic performance is improved. The proposed FTSMC guarantees a fixed-time convergence of the dc bus voltage to its expectation. In addition, a reduced-order model of the VSR is derived to simplify the design of the proposed control strategy. A strict stability analysis is carried out to show the large-signal stability of the regulated system, and some simulation, hardware-in-the-loop (HIL) test, and hardware experimental results are demonstrated to validate the effectiveness of the proposed control strategy.
KW - AC/DC rectifier
KW - constant power load (CPL)
KW - large-signal stabilization
KW - more-electric aircraft (MEA)
UR - https://www.scopus.com/pages/publications/105010089923
U2 - 10.1109/TTE.2025.3585632
DO - 10.1109/TTE.2025.3585632
M3 - 文章
AN - SCOPUS:105010089923
SN - 2332-7782
VL - 11
SP - 12089
EP - 12103
JO - IEEE Transactions on Transportation Electrification
JF - IEEE Transactions on Transportation Electrification
IS - 5
ER -