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High-speed feedback control of an oscillating magnetic helicity injector using a graphics processing unit.
Morgan, K D; Hossack, A C; Hansen, C J; Nelson, B A; Sutherland, D A.
Afiliação
  • Morgan KD; Department of Aeronautics and Astronautics, University of Washington, Seattle, Washington 98195, USA.
  • Hossack AC; Department of Aeronautics and Astronautics, University of Washington, Seattle, Washington 98195, USA.
  • Hansen CJ; Department of Aeronautics and Astronautics, University of Washington, Seattle, Washington 98195, USA.
  • Nelson BA; Department of Aeronautics and Astronautics, University of Washington, Seattle, Washington 98195, USA.
  • Sutherland DA; CTFusion, Inc., Seattle, Washington 98121, USA.
Rev Sci Instrum ; 92(5): 053530, 2021 May 01.
Article em En | MEDLINE | ID: mdl-34243306
ABSTRACT
A real-time control system has been developed to control the amplitude, phase, and offset of bulk plasma parameters inside an oscillating magnetic helicity injector. Control software running entirely on an Nvidia Tesla P40 graphical processing unit is able to receive digitizer inputs and send response patterns to a Pulse Width Modulation (PWM) controller with a minimum control loop period of 12.8 µs. With an input digitization rate of 10 MS/s, a three-parameter proportional integral differential controller is shown to be sufficient to inform the PWM controller to drive the desired oscillating plasma waveform with a frequency of 16.6 kHz that is located near the resonance of a coupled RLC circuit. In particular, the temporal phase of the injector waveform is held within 10° of the target value. Control is demonstrated over the toroidal modal structure of the imposed magnetic perturbations of the helicity injection system, allowing a new class of discharges to be studied.

Texto completo: 1 Base de dados: MEDLINE Idioma: En Ano de publicação: 2021 Tipo de documento: Article

Texto completo: 1 Base de dados: MEDLINE Idioma: En Ano de publicação: 2021 Tipo de documento: Article