Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
9638383 | Fusion Engineering and Design | 2005 | 5 Pages |
Abstract
This paper describes the hardware and the software structure of a new controller for the JET error field correction coils (EFCC) system, a set of ex-vessel coils that recently replaced the internal saddle coils. The EFCC controller has been developed on a conventional VME hardware platform using a new software framework, recently designed for real-time applications at JET, and replaces the old disruption feedback controller increasing the flexibility and the optimization of the system. The use of conventional hardware has required a particular effort in designing the software part in order to meet the specifications. The peculiarities of the new controller will be highlighted, such as its very useful trigger logic interface, which allows in principle exploring various error field experiment scenarios.
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Authors
L. Zanotto, F. Sartori, M. Bigi, F. Piccolo, M. De Benedetti,