Double-Side Voltage-Behind-Reactance Model of Main Machine in Aircraft Wound-Rotor Synchronous Starter-Generator Considering Saliency Factor Change and Equivalent Iron Loss Resistance
Author:
Affiliation:
1. Department of Electrical Engineering, Northwestern Polytechnical University, Xi'an, China
Funder
National Natural Science Foundation of China
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Electrical and Electronic Engineering,Energy Engineering and Power Technology
Link
http://xplorestaging.ieee.org/ielx7/60/10050374/09894057.pdf?arnumber=9894057
Reference20 articles.
1. Saturable and Decoupled Constant-Parameter VBR Model for Six-Phase Synchronous Machines in State-Variable Simulation Programs
2. Constant‐parameter synchronous machine model including main flux saturation
3. Integrated Model of Aircraft Two-stage Synchronous Starter-Generator Considering Magnetic Saturation
4. Double-Side Voltage-Behind-Reactance Model of Brushless Exciter in Aircraft Wound-Rotor Synchronous Starter-Generator Considering Magnetic Saturation
5. Unified Model Formulations for Synchronous Machine Model With Saturation and Arbitrary Rotor Network Representation
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1. Fault Diagnosis of Rotating Rectifier in Aircraft Wound-Rotor Synchronous Starter–Generator Based on Stator Currents Under all Operational Processes;IEEE Transactions on Power Electronics;2023-12
2. A MRAS Based Identification Method of Stator Resistance Considering Iron Loss for Main Machine in Wound-Rotor Synchronous Starter-Generator;2023 26th International Conference on Electrical Machines and Systems (ICEMS);2023-11-05
3. A Virtual High-Frequency Signal Injection Based Maximum Torque per Ampere Control Method Considering Iron Loss for Aircraft Wound-Rotor Synchronous Starter-Generator in the Starting Mode;IECON 2023- 49th Annual Conference of the IEEE Industrial Electronics Society;2023-10-16
4. An efficient integrated model for diesel‐engine three stage brushless synchronous generator;IET Electric Power Applications;2023-08-24
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