Finite-Time Model Predictive Stabilization of DC Electrical Power Systems Feeding CPLs in More Electric Aircraft.
IEEE Trans. Ind. Electron., October, 2024
An Improved Active Damping Method for Enhancing Robustness of LCL-Type, Grid-Tied Inverters under Weak Grid Conditions.
Sensors, October, 2023
Optimization of Hybrid Energy Storage System Sizing With Considering Energy Management Strategy for High-Power Pulsed Load in Aircraft.
IEEE Trans. Veh. Technol., April, 2023
Composite Fast Terminal Sliding Mode Control of DC-DC Converters for Renewable Energy Systems.
Proceedings of the IEEE Industry Applications Society Annual Meeting, 2022
Advanced Control Design of Interleaved Boost Converter for Fuel Cell Applications.
Proceedings of the 46th Annual Conference of the IEEE Industrial Electronics Society, 2020
Improved-Droop Control for Electrical Power System in More Electric Aircraft Integrated with Energy Storage System.
Proceedings of the 46th Annual Conference of the IEEE Industrial Electronics Society, 2020
Design of a electro-hydrostatic actuator controller based on disturbance observer.
Proceedings of the IECON 2017 - 43rd Annual Conference of the IEEE Industrial Electronics Society, Beijing, China, October 29, 2017
Study on the linear parameterization method for the peak friction coefficient of aircraft braking system.
Proceedings of the IECON 2017 - 43rd Annual Conference of the IEEE Industrial Electronics Society, Beijing, China, October 29, 2017
Control analysis of inverter parallel system based on virtual synchronous generator.
Proceedings of the IECON 2017 - 43rd Annual Conference of the IEEE Industrial Electronics Society, Beijing, China, October 29, 2017
Design and analysis of the energy conversion device in the electromagnetic aeroelastic energy harvesting system.
Proceedings of the IECON 2017 - 43rd Annual Conference of the IEEE Industrial Electronics Society, Beijing, China, October 29, 2017
Numerical and Analytical Modeling of Switched Reluctance Machines.
J. Comput., 2012
Research on Simulation of Aircraft Electro-Hydrostatic Actuator (EHA) Anti-Skid Braking System.
J. Comput., 2011