Initial Rotor Position Estimation Method for Aircraft Three-Stage Starter/Generator Based on Self-Injected Harmonic Signal
Author:
Affiliation:
1. Center for More Electric Aircraft Power System (CMEAPS), College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China
2. Department of Automation Engineering, Wuxi Taihu University, Wuxi, China
Funder
National Nature Science Foundation of China
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/ielx7/6687316/10050348/09868792.pdf?arnumber=9868792
Reference32 articles.
1. Design of a Brushless Rotor Supply for a Wound Rotor Synchronous Machine for Integrated Starter Generator
2. Design and Control of a Two-Phase Brushless Exciter for Aircraft Wound-Rotor Synchronous Starter/Generator in the Starting Mode
3. A New Rotor Position Estimation Method of IPMSM Using All-Pass Filter on High-Frequency Rotating Voltage Signal Injection
4. Design and Characterization of a Single-Phase Main Exciter for Aircraft Wound-Rotor Synchronous Starter–Generator
5. Rotor Position Estimation Method for Brushless Synchronous Machine Based on Second-Order Generated Integrator in the Starting Mode
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Analysis and Optimization for Winding Topology of Multiphase High Power DC Generator in Future Hybrid Electric Propulsion Aircraft;2023 26th International Conference on Electrical Machines and Systems (ICEMS);2023-11-05
2. Improved Rotor Position Estimation Method for Brushless Synchronous Starter/Generator Based on Field Harmonic Signals Self-Injection Scheme;IEEE Transactions on Transportation Electrification;2022
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