Potential starter/generator technologies for future aerospace applications
- 1 May 1997
- journal article
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Aerospace and Electronic Systems Magazine
- Vol. 12 (5), 24-31
- https://doi.org/10.1109/62.587815
Abstract
No abstract availableThis publication has 37 references indexed in Scilit:
- Design and performance of a high frequency link induction motor drive operating at unity power factorPublished by Institute of Electrical and Electronics Engineers (IEEE) ,2003
- Generating with the switched reluctance motorPublished by Institute of Electrical and Electronics Engineers (IEEE) ,2002
- Switched reluctance generators for wind energy applicationsPublished by Institute of Electrical and Electronics Engineers (IEEE) ,2002
- Detailed design of a 30-kW switched reluctance starter/generator system for a gas turbine engine applicationIEEE Transactions on Industry Applications, 1995
- Design and implementation of a five-hp, switched reluctance, fuel-lube, pump motor drive for a gas turbine engineIEEE Transactions on Power Electronics, 1995
- Control of a polyphase induction generator/induction motor power conversion system completely isolated from the utilityIEEE Transactions on Industry Applications, 1994
- System design considerations for a high-power aerospace resonant link converterIEEE Transactions on Power Electronics, 1993
- A new resonant link aircraft power generating systemIEEE Transactions on Aerospace and Electronic Systems, 1993
- The control of high-speed variable-reluctance generators in electric power systemsIEEE Transactions on Industry Applications, 1993
- Field-oriented control of an induction machine in a high frequency link power systemIEEE Transactions on Power Electronics, 1990