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Architecture Design and Internal Implementation of a Universal Coupling Between Controllers and Physics in a Tokamak Flight Simulator

Wu, Chuanren ORCID iD icon 1; David, Pierre; Fable, Emiliano; Frattolillo, Domenico; Di Grazia, Luigi Emanuel; Mattei, Massimiliano; Siccinio, Mattia; Treutterer, Wolfgang; Zohm, Hartmut
1 Institut für Hochleistungsimpuls- und Mikrowellentechnik (IHM), Karlsruher Institut für Technologie (KIT)

Abstract (englisch):

The flight simulator predicts the dynamic behavior of a full plasma discharge (described in terms of one-dimensional profiles) by employing multiple control loops based on synthetic diagnostics, which could also emulate realistic sensor and actuator models. It serves as a valuable tool for designing and optimizing plasma scenarios, as well as for assessing the feasibility of controlling discharges. The Fenix flight simulator, originally developed for the ASDEX Upgrade, has been ported to EU-DEMO and is capable of modeling any tokamak.

One of the essential elements in a flight simulator is the link between the co-simulated plasma physics and the control loops. This element is tightly coupled to the specifications of both the plasma model and the control algorithms to be implemented; but on the other hand, to ensure the portability and applicability of the flight simulator to different scenarios or devices, the coupling between plasma and control algorithms should be neutral to any concrete device and configuration. In addition, as a serial component of the control loop, data exchange takes place at every single step of the control simulation, therefore an efficient implementation is critical for the overall simulation performance. ... mehr


Postprint §
DOI: 10.5445/IR/1000162112
Veröffentlicht am 31.08.2024
Cover der Publikation
Zugehörige Institution(en) am KIT Institut für Hochleistungsimpuls- und Mikrowellentechnik (IHM)
Publikationstyp Zeitschriftenaufsatz
Publikationsjahr 2024
Sprache Englisch
Identifikator ISSN: 1536-1055, 1943-7641
KITopen-ID: 1000162112
HGF-Programm 31.13.02 (POF IV, LK 01) Plasma Heating & Current Drive Systems
Erschienen in Fusion Science and Technology
Verlag Taylor and Francis
Band 80
Heft 6
Seiten 766-771
Projektinformation EUROfusion (EU, EU 9. RP, 101052200)
Vorab online veröffentlicht am 30.08.2023
Schlagwörter Flight simulator, feedback control, full discharge, co-simulation, ASDEX Upgrade.
Nachgewiesen in Web of Science
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Scopus
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