Mr. Mingliang Bai | Electric propulsion Award | Best Researcher Award
Mr. Mingliang Bai, Beihang university, China
Mingliang Bai is a dedicated Ph.D. candidate in Aerospace Propulsion Theory and Engineering at Beihang University, specializing in hybrid-electric propulsion systems and sustainable energy ๐ฑโ๏ธ. He has significantly contributed to aerospace technology with 20 published papers, 10 in SCI-indexed journals, and holds 10 patents ๐๐ฌ. His research includes collaborations with international institutions and focuses on optimizing energy management for greener aviation ๐. As an IEEE student member, his work is recognized for advancing the field of aerospace propulsion and energy efficiency ๐ก๐ง.
Publication Profile
Academic Background ๐
Mingliang Bai is pursuing a Ph.D. in Aerospace Propulsion Theory and Engineering at Beihang University. His specialization includes optimization design, optimal control, and energy management for aerospace hybrid-electric propulsion systems. Mingliang’s research aims at enhancing efficiency and sustainability in aerospace propulsion.
Research Focus
Mingliang Bai’s research is centered around the development and optimization of hybrid-electric propulsion systems for aerospace applications, with a particular emphasis on energy management and sustainability ๐ฑ. His work spans from improving the performance of hybrid unmanned aerial vehicles to analyzing superconducting materials for advanced propulsion systems ๐. Baiโs studies include the integration of turbo-electric hybrid propulsion, the use of superconducting materials for energy efficiency, and the application of fuzzy logic for optimal energy management in UAVs ๐ค๐. His innovative contributions aim to enhance energy-saving and emission reduction in the aerospace sector ๐.
Publication Top Notes
- Research on energy management of hybrid unmanned aerial vehicles to improve energy-saving and emission reduction performance ๐โ๏ธ | Cited by: 31 | Year: 2020
- Electromagnetic performance analysis of superconducting hybrid excitation homopolar inductor alternator โก๐ฌ | Cited by: 12 | Year: 2021
- Rotor Design of HTS homopolar inductor alternator based on multi-physics field ๐๐ | Cited by: 9 | Year: 2021
- Sizing Methodology and Energy Management of an AirโGround Aircraft with Turbo-Electric Hybrid Propulsion System ๐ฑโ๏ธ | Cited by: 5 | Year: 2022
- Effect of composite superconductor structure on dynamic properties of superconducting interface and formation in space application ๐ง๐ฐ๏ธ | Cited by: 5 | Year: 2020
- Testing and comparison of levitation forces and rotational friction in different superconducting tape stacks โ๏ธ๐งฒ | Cited by: 4 | Year: 2020
- Experiments and simulation of electromagnetic properties in an HTS knitted tape stack ๐ก๐ฌ | Cited by: 4 | Year: 2019
- Fuzzy-based optimal energy management strategy of series hybrid-electric propulsion system for UAVs ๐ค๐ | Cited by: 2 | Year: 2023
- Equivalent Consumption Minimization Strategy based on fuzzy logic control for the energy management of hybrid Unmanned Aerial Vehicle ๐๐ธ | Cited by: 2 | Year: 2021
- Control Strategies of Motor for Shaftless Rim-Driven Aviation Electric Propulsion System โ๏ธโ๏ธ | Cited by: 1 | Year: 2022