The paper reports the control design for an aircraft electric starter-generator system based-on high-speed permanent magnet machine operated in a flux-weakening mode and controlled by an active front-end rectifier. The proposed system utilizes advances of modern power electronics allowing the use of novel machine types and the introduction of controlled power electronics into the main path of energy flow. The paper focuses on control design for such system and includes development of flux weakening control of high-speed permanent magnet machine and droop control of the system output dc-link current. The achieved analytical design results and the expected system performance are confirmed by time-domain simulations.
Control Design for Electric Starter-Generator Based on a High-Speed Permanent-Magnet Machine Fed by an Active Front-End Rectifier
Sae Technical Papers
SAE 2014 Aerospace Systems and Technology Conference ; 2014
2014-09-16
Aufsatz (Konferenz)
Englisch
British Library Conference Proceedings | 2014
|Permanent Magnet Starter-Generator for Aircraft Application
SAE Technical Papers | 2014
|Permanent Magnet Starter-Generator for Aircraft Application
British Library Conference Proceedings | 2014
|