Shuai Wu
Gender:Male
Education Level:博士研究生
Alma Mater:Beihang University
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.[22] S. Wu, C. Li, X. Zhao, and Z. Jiao, “High accuracy position adjustment and vibration isolation actuator with the controlled ferrofluid,” Appl. Phys. Lett., vol. 111, no. 21, 2017, doi: 10.1063/1.5012975.
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.[21] S. Wu, P. C. K. Luk, C. Li, X. Zhao, and Z. Jiao, “Investigation of an Electromagnetic Wearable Resonance Kinetic Energy Harvester with Ferrofluid,” IEEE Trans. Magn., vol. 53, no. 9, 2017, doi: 10.1109/TMAG.2017.2714621.
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.[20] S. Wu, B. Yu, Z. Jiao, Y. Shang, and P. C. K. K. Luk, “Preliminary design and multi-objective optimization of electro-hydrostatic actuator,” Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng., vol. 000, no. 7, pp. 1258–1268, 2017, doi: 10.1177/0954410016654181.
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.[19] S. Wu, X. Zhao, C. Li, Z. Jiao, and F. Qu, “Multiobjective Optimization of a Hollow Plunger Type Solenoid for High Speed On/Off Valve,” IEEE Trans. Ind. Electron., vol. 65, no. 4, pp. 3115–3124, 2018, doi: 10.1109/TIE.2017.2756578.
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.[18] Y. Shang, X. Liu, Z. Jiao, and S. Wu, “An integrated load sensing valve-controlled actuator based on power-by-wire for aircraft structural test,” Aerosp. Sci. Technol., vol. 77, pp. 117–128, 2018, doi: 10.1016/j.ast.2018.02.030.
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.[17] Y. SHANG, X. LIU, Z. JIAO, and S. WU, “A novel integrated self-powered brake system for more electric aircraft,” Chinese J. Aeronaut., 2018, doi: 10.1016/j.cja.2017.11.015.
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.[16] Z. LI, Y. SHANG, Z. JIAO, Y. LIN, S. WU, and X. LI, “Analysis of the dynamic performance of an electro-hydrostatic actuator and improvement methods,” Chinese J. Aeronaut., 2018, doi: 10.1016/j.cja.2018.03.014.
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.[15] Z. Li, Y. Shang, Z. Jiao, S. Wu, and J. Yao, “Surplus Torque Elimination Control of Electro-Hydraulic Load Simulator Based on Actuator Velocity Input Feedforword Compensating Method,” J. Dyn. Syst. Meas. Control. Trans. ASME, vol. 140, no. 10, 2018, doi: 10.1115/1.4039663.
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.[14] T. YANG, S. BOZHKO, P. WHEELER, S. WANG, and S. WU, “Generic functional modelling of multi-pulse auto-transformer rectifier units for more-electric aircraft applications,” Chinese J. Aeronaut., vol. 31, no. 5, 2018, doi: 10.1016/j.cja.2018.03.010.
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.[13] B. Yu, S. Wu, Z. Jiao, and Y. Shang, “Multi-Objective Optimization Design of an Electrohydrostatic Actuator Based on a Particle Swarm Optimization Algorithm and an Analytic Hierarchy Process,” Energies, vol. 11, no. 9, p. 2426, 2018, doi: 10.3390/en11092426.