Abstract
This paper describes the fitter inductor design of a resonant phase leg inverter for for an aerospace application. Attention has been given to the high frequency switching current existing in the inductor and weight and size restrictions for the aerospace application.
| Original language | English |
|---|---|
| Journal | IEE Colloquium (Digest) |
| Issue number | 54 |
| Publication status | Published - 1 Dec 1996 |
| Externally published | Yes |
ASJC Scopus subject areas
- Electrical and Electronic Engineering