Decoupling start control method for aircraft wound‐rotor synchronous starter‐generator based on main field current estimation-Reference-Cited by-同舟云学术

Decoupling start control method for aircraft wound‐rotor synchronous starter‐generator based on main field current estimation

Published:2018-11-14 Issue:7 Volume:13 Page:863-870
ISSN:1751-8660
Container-title:IET Electric Power Applications
language:en
Short-container-title:IET Electric Power Applications

Author:

Jiao Ningfei¹^ORCID,Liu Weiguo¹,Meng Tao¹,Sun Chenghao¹,Jiang Yu²

Affiliation:

1. Shaanxi Key Laboratory of Small & Special Electrical Machine and Drive TechnologySchool of AutomationNorthwestern Polytechnical UniversityXi'anShaanxi710072People's Republic of China

2. AVIC Shaanxi Aero Electric Co., LtdXi'anShaanxi710065People's Republic of China

Funder

National Natural Science Foundation of China

Publisher

Institution of Engineering and Technology (IET)

Subject

Electrical and Electronic Engineering

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1049/iet-epa.2018.5140

Reference28 articles.

1. More Electric Aircraft: Review, Challenges, and Opportunities for Commercial Transport Aircraft

2. Integrated starter generator

3. Electric Starter Generators: Their Integration into Gas Turbine Engines

4. A HESM‐based variable frequency AC starter‐generator system for aircraft applications;Zhang Z.;IEEE Trans. Energy Convers.,2018

5. Design and Characterization of a Three-Phase Brushless Exciter for Aircraft Starter/Generator

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