Dynamic Performance Improvement of Wound Rotor Synchronous Starter/Generator System Based on PWM Rectifier
Author:
Affiliation:
1. Center for More-Electric-Aircraft Power System, Nanjing University of Aeronautics and Astronautics, Nanjing, China
Funder
National Natural Science Foundation of China
“Ye Qisun” Science Foundation
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Electrical and Electronic Engineering,Energy Engineering and Power Technology,Transportation,Automotive Engineering
Link
http://xplorestaging.ieee.org/ielx7/6687316/10251026/10050188.pdf?arnumber=10050188
Reference29 articles.
1. Control Design and Voltage Stability Analysis of a Droop-Controlled Electrical Power System for More Electric Aircraft
2. Research and Realization of High-Power Medium-Voltage Active Rectifier Concepts for Future Hybrid-Electric Aircraft Generation
3. Modeling and Impedance Analysis of a Single DC Bus-Based Multiple-Source Multiple-Load Electrical Power System
4. An Improved Voltage Compensation Approach in A Droop-Controlled DC Power System for the More Electric Aircraft
5. Wide speed range permanent magnet synchronous generator design for a DC power system;miao;Chin J Electr Eng,2019
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