.[12] C. Li, S. Wu, B. Yu, Z. Jiao, and S. Member, “Finite Element Analysis of A new Multi-DOF Flexible Micro-Displacement Manipulator Based on Ferrofluid,” in 2018 IEEE/ASME International Conference on Advanced Intelligent Mechatronics (AIM), 2018, pp. 980–985, doi: 10.1109/AIM.2018.8452460.
.[11] C. Li, S. Wu, P. C. K. Luk, M. Gu, and Z. Jiao, “Enhanced Bandwidth Nonlinear Resonance Electromagnetic Human Motion Energy Harvester Using Magnetic Springs and Ferrofluid,” IEEE/ASME Trans. Mechatronics, vol. 24, no. 2, pp. 710–717, 2019, doi: 10.1109/tmech.2019.2898405.
.[10] Y. Shang, X. Li, S. Wu, and Q. Pan, “A Novel Electro Hydrostatic Actuator System with Energy Recovery Module for More Electric Aircraft,” IEEE Trans. Ind. Electron., vol. PP, no. c, p. 1, 2019, doi: 10.1109/TIE.2019.2905834.
.[9] Z. Jiao, D. Sun, Y. Shang, X. Liu, and S. Wu, “A high efficiency aircraft anti-skid brake control with runway identification,” Aerosp. Sci. Technol., vol. 91, 2019, doi: 10.1016/j.ast.2019.05.001.
.[8] L. Xue, S. Wu, Y. Xu, and D. Ma, “A simulation-based multi-objective optimization design method for pump-driven electro-hydrostatic actuators,” Processes, vol. 7, no. 5, 2019, doi: 10.3390/pr7050274.
.[7] R. Chen, Z. Jiao, L. Yan, Y. Shang, and S. Wu, “Nonlinear synchronous control for H-Type gantry stage used in electric vehicles manufacturing,” Energies, vol. 12, no. 12, 2019, doi: 10.3390/en12122305.
.[6] Z. Jiao et al., “An intelligent design method for actuation system architecture optimization for more electrical aircraft,” Aerosp. Sci. Technol., vol. 93, 2019, doi: 10.1016/j.ast.2019.03.048.
.[5] D. SUN, Z. JIAO, Y. SHANG, S. WU, and X. LIU, “High-efficiency aircraft antiskid brake control algorithm via runway condition identification based on an on-off valve array,” Chinese J. Aeronaut., vol. 32, no. 11, 2019, doi: 10.1016/j.cja.2019.08.020.
.[4] Y. Shang et al., “A novel hydraulic pulsation reduction component based on discharge and suction self-oscillation: Principle, design and experiment,” Proc. Inst. Mech. Eng. Part I J. Syst. Control Eng., vol. 234, no. 4, 2020, doi: 10.1177/0959651819871775.
.[3] Z. Jiao, H. Zhang, Y. Shang, X. Liu, and S. Wu, “A power-by-wire aircraft brake system based on high-speed on-off valves,” Aerosp. Sci. Technol., vol. 106, p. 106177, 2020, doi: 10.1016/j.ast.2020.106177.