A Comprehensive Model of Variable Pitch Electric Propulsion Unit for Optimal-Power Thrust Control
Author:
Affiliation:
1. Department of Electrical Engineering, Harbin Institute of Technology, Harbin, China
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Link
http://xplorestaging.ieee.org/ielx7/7/10552647/10413566.pdf?arnumber=10413566
Reference21 articles.
1. System Approach to Electric Machines Development for Aviation Hybrid Propulsion Systems Under Economic Crisis
2. Aircraft Distributed Electric Propulsion Technologies—A Review
3. Minimum-time Trajectory Generation of eVTOL in Low-Speed Phase: Application in Control Law Design
4. Powered Yaw Control for Distributed Electric Propulsion Aircraft: A Model Predictive Control Approach
5. More Electric Aircraft: Review, Challenges, and Opportunities for Commercial Transport Aircraft
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