Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (13): 329573-329573.doi: 10.7527/S1000-6893.2023.29573
• Electronics and Electrical Engineering and Control • Previous Articles
Zhenyang HAO, Fengting ZHANG(), Jian YANG, Xin CAO
Received:
2023-09-13
Revised:
2023-10-06
Accepted:
2023-11-08
Online:
2023-12-02
Published:
2023-11-22
Contact:
Fengting ZHANG
E-mail:zhangft@nuaa.edu.cn
Supported by:
CLC Number:
Zhenyang HAO, Fengting ZHANG, Jian YANG, Xin CAO. Vibration damping electric actuator system based on parallel independent control strategy[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(13): 329573-329573.
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[1] | HAO Zhenyang, WANG Tao, CAO Xin, ZHU Tao. Decoupling control strategy of position loop for vibration damping electric actuator [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 325884-325884. |
[2] | JIANG Jun, ZHANG Bendong, WANG Kai, LI Wenyuan, ZHANG Chaohai. Partial discharge rule of more-electric-aircraft with pulse voltage waveform [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(9): 323889-323889. |
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All copyright © editorial office of Chinese Journal of Aeronautics
Total visits: 6658907 Today visits: 1341