nstx fy2007 physics results 1 strike point control dynamics supported by office of science college...

1NSTX FY2007 Physics Results

Strike Point Control Dynamics

Supported byOffice ofScience

College W&MColorado Sch MinesColumbia UComp-XGeneral AtomicsINELJohns Hopkins ULANLLLNLLodestarMITNova PhotonicsNew York UOld Dominion UORNLPPPLPSIPrinceton USNLThink Tank, Inc.UC DavisUC IrvineUCLAUCSDU ColoradoU MarylandU RochesterU WashingtonU Wisconsin

Culham Sci CtrU St. Andrews

York UChubu UFukui U

Hiroshima UHyogo UKyoto U

Kyushu UKyushu Tokai U

NIFSNiigata UU Tokyo

JAEAHebrew UIoffe Inst

RRC Kurchatov InstTRINITI

KBSIKAIST

ENEA, FrascatiCEA, Cadarache

IPP, JülichIPP, Garching

ASCR, Czech Rep

Egemen Kolemen, Princeton University

in colloboration with D. Gates, C. Rowley, J. Kasdin, K. Taira

For the NSTX Research Teamat

NSTX 2009 Advanced Scenarios and Control,

B252 - PPPLFebruary 2nd, 2009

2/11

High : ne reduced by 25%

LLD

R=0.65 R=0.84

20cm

15cm

10cm

Shown for different LLD-1 widths

DensityReduction

Low : ne reduced by 50%

LLD

R=0.65 R=0.84

10cm

15cm

20cm


Henry Kugel,

R. Maingi, ORNL

V. Soukhanovskii, LLNL

• Density reduction depends on proximity of outer strike point to LLD-1

DensityReduction

Motivation: Density Reduction via Strike Point Control

3/11

• We expect the strike point predominantly depend on PF2L.

• We can turn the system into a SISO black box control problem.

• Introduce dynamics by assuming the plant as a time constant, , later.

Preliminary Study: SISO System No Dynamics System

The change in the strike point with different PF2L current (isolver)

PF2L=2 kAmp/MAmp PF2L=3 kAmp/MAmp PF2L=4 kAmp/MAmp

4/11

• Change strike point location by changing PF2L while keeping other coils currents constant.

• While achieving (in order of importance):– Low Inner Gap, High Kappa

• Which other parameters are important? Squareness, Triangularity…

• Scan by changing PF2L only:

PF2L Scan: Shot 115495

The change in the strike point for 115495.00501 with different PF2L current (isolver)

5/11

• Change strike point location by changing PF2L while keeping other coils currents constant.

• While achieving (in order of importance):– Low Inner Gap, High Kappa

• Which other parameters are important? Squareness, Triangularity…

• Scan by changing PF2L only:

PF2L Scan: Shot 120001

The change in the strike point for 120001.00650 with different PF2L current (isolver)

6/11

Strike Point versus PF2L current

7/11

• Use the insight from the non-dynamic model to design a PID controller to keep the strike point at the center of LLD, with ~1 cm variation from the reference value.

• Experiment:– Put perturbations in the PF2 request & measure the response of the strike point.

– Test and tune the strike point controller.

• Study the compromise with respect to the loss in control for shape control and other control aims.

• In this case, s=position and r=reference position of the strike point.

Aim: Design a Real Time Controller for the Strike Point Motion

8/11

• Choose two plasma shapes (and strike points) from the scan.

• Stabilize the plasma for the 1st shape.

• We know the coil currents need to take us to the 2nd equilibrium.

• Put a step input for the coil currents that gives the 2nd equilibrium.

• Measure the time constant of the strike point motion to the change in current.

• Repeat for many other equilibrium.

Experiment Procedure: Step Response and Time Constant, .

PF2L

PF2L

9/11

• Shot 115495.00501 is given as the requested profile.

• This is an old shot.

• Instead choose from shot 120001 with similar profile and same strike point.

Experiment: Starting Condition

10/11

• Depending on li and strike point distance choose the control input.

• Experiment runs ~ 8-10 shots

• Use shot120001 with strike point between 0 and 25 cm.

• Strike Point distance start with 0 then 25 cm then interpolate as much points as possible in the experiment day. 0, 25, 12, 6, 18...

Experiment Current Request: li Dependence

11/11

• Example x-point scan: Move it horizontally (Stefan Gerhardt)

• The following scan varies multiple variables at the same time.

• Try to keep the basic shape constant except for lower outer squareness.

Further Study: Multiple Control Input Variation

Normalized Current Requests Vs. KappaLower X-Point at -1.37 m, profiles from 127267, t=0.4

0

0.005

0.01

0.015

0.02

0.025

0.3 0.35 0.4 0.45 0.5 0.55 0.6 0.65 0.7 0.75

Achieved Lower Triangularity

Curr

ent Request

(kA/M

A)

ISOLVER PF1A/Ip

ISOLVER PF2L/Ip

Real Shots, PF1AU/Ip

Real Shots, PF2L/Ip

ISOLVER Scans PF1AU/Ip PF1AL/ip PF2U/Ip PF2L/Ip

high 0.005 0.02 0 0

medium high 0.02 0.02 0 0.0045

medium 0.02 0.02 0 0.0065

medium low 0.02 0.01 0 0.009

low 0.02 0 0 0.01

12/11

Extra

13/11

Extra

14/11


• Experiment:– Put perturbations in the PF2 request & measure the response of the strike point.





sensor

plantcontrollerPID

15/11

• a


16/11

• a


17/11

• Used rtefit with no dynamics model to see the effect of the control PF coils on the strike point position.

• Preliminary Study: – Strike point seems to be very much dependant on the X-point

– It is not sensitive to the change in any coil but PF2L.

Preliminary Study: No-Dynamics Model

Example Shot and the change of the strike point with different PF3L current.

PF3L=1 kAmp

PF3L=2 kAmp

PF3L=4 kAmp

18/11

• a


19/11

• Choose two plasma shapes (and strike points) from the scan.

• Stabilize the plasma for the 1st shape.

• We know the coil currents need to take us to the 2nd equilibrium.

• Put a step input for the coil currents that gives the 2nd equilibrium.

• Measure the time constant of the strike point motion to the change in current.

• Repeat for many other equilibrium.

Experiment Procedure

20/11


• Experiment (0.5 Day): – Put perturbations in the PF2 request & measure the response of the strike point.





sensor

plantcontrollerPID

21/11

• a

Stefan Scan for x point – move it horizontally

22/11

• a


23/11

• a

Stefan Scan for x point – move it horizontally

24/11

• Extra

25/11

• Liquid lithium divertor (LLD) on NSTX, enables experiments with the first complete liquid metal divertor target in a high-power device in 2009.

• The location in the vacuum vessel is shown schematically in figure 1.• Reduced recycling with LLD.• The most important parameter that defines the density reduction is strike point position.

Background: Liquid Lithium Divertor & Edge Density

1. Schematic of NSTX showing location of Liquid Lithium Divertor inside vacuum vessel

2. Edge density profiles calculating with UEDGE for NSTX Liquid Lithium Divertor assuming different recycling coefficients

26/11

• A liquid lithium divertor (LLD) is being installed on NSTX, to enable experiments with the first complete liquid metal divertor target in a high-power device in 2009. The location in the vacuum vessel is shown schematically in Fig. 9. The LLD is a conic section with four 90-degree segments, each consisting of a 1.9 cm-thick copper plate with a 0.02 cm-thick stainless steel liner that is isolated toroidally with carbon tiles. Molybdenum will be plasma sprayed onto the liner in vacuum, to form a 0.01 cm-thick layer with 50% porosity. This will become the plasma-facing surface when filled with lithium, which will be kept liquid by resistive heaters in the plates. The present outer divertor (Fig. 1) consists of concentric rows of ATJ graphite tiles on copper baseplates. Lithium evaporated onto the tiles prior to a shot would solidify, and pump only while the hydrogenic atoms can react with the surface layer of the lithium coating. The LLD will replace part of these tiles with lithium that will be kept molten. Because the lithium will continue reacting with hydrogen or deuterium until it is volumetrically converted to hydrides,[12] the LLD is expected to provide better pumping than lithium coatings on carbon PFC’s. FIG. 9. Schematic of NSTX showing location of Liquid Lithium Divertor inside vacuum vessel Detailed edge plasma modeling has begun with the UEDGE transport code to simulate the effects of reduced recycling expected from the LLD.[13] The simulations start with adjusting the transport coefficients until the edge temperatures and densities match the data from the multipoint Thomson scattering diagnostic for existing NSTX plasmas. New profiles are then generated for a variety of recycling coefficients (Fig. 10). The results of the simulations have the same nonlinear radial dependence as the SOL measurements during high lithium evaporation. The simulations, however, do not show the linear density rise observed at the low lithium evaporation rate during NSTX experiments. This suggests that more work needs to be done on the transport modeling before further conclusions can be drawn from the UEDGE calculations.

Background: Liquid Lithium Divertor & Edge Density

FIG. 1. (left) Elevation of NSTX showing position of LITERs. (right) NSTX plan viewing indicating toroidal

location of LITERs and coating regions blocked by center stack.

Schematic of NSTX showing location of Liquid Lithium Divertor inside vacuum vessel

FIG. 10. Edge density profiles calculating with UEDGE for NSTX Liquid Lithium Divertor assuming

different recycling coefficients

27

LLD-1 Overview

• Geometry:, 0.01cm thick, 50% porous Mo flame-sprayed on 0.02 cm SS brazed to 1.9 cm Cu. 20 cm wide, Ri = 0.65 m, Ro = 0.85 m. Li loading via LITER.

• Operating temperature: typ. =205°C

• Power Handling: SNL thermal analysis for the cases for the strike point on the LLD with peak Li temperature set at 400 °C, - can sustain a peak of ~2MW/m2 for 10s and 4 MW/m2 for ~3s. - Less Li, higher heat transfer.

• Interlocks: similar to LITER (Heater Power off during fields, vacuum event, if temperature >set point,…..) - presently no automatic LLD-1 thermal interlock to interrupt plasma position or NBI - Fast and slow IR cameras will monitor LLD-1 front-face temperature. - Visible cameras will monitor divertor region.

Li thermal conductivity is low. (~ W/m-°K 400 Cu, 150 Mo, 45 Li, 15 SS)

28

Day-1: Slowly increase Li and Test Pumping by LLD-1 on Outer Divertor to Provide Density Control for Inner Divertor Broad SOL Dα Profile, High δ Plasmas

LLD

High : reduce ne by 25%

• Density reduction will depend on proximity of outer strike point to LLD-1

20cm

15cm

10cm

R. Maingi, ORNL

Soukhanovskii LLNL


DensityReduction

29

Day-2: Test Pumping by LLD-1 with Strike Point on Outer Divertor to Provide Density Control for Low δ Plasmas

R. Maingi, ORNL

Low : reduce ne by 50%

LLNL

LLD

DensityReduction

10cm

15cm

20cm


R=0.65 R=0.85

30

Due to High Flux Expansion, Pumping by 20 cm Wide LLD-1 on Outer Divertor Will Provide Density Control for Both High and Low δ Plasmas

High : ne reduced by 25%

LLD

R=0.65 R=0.84

20cm

15cm

10cm


DensityReduction

Low : ne reduced by 50%

LLD

R=0.65 R=0.84

10cm

15cm

20cm


R. Maingi, ORNL V. Soukhanovskii, LLNL

• Density reduction will depend on proximity of outer strike point to LLD-1

DensityReduction

nstx fy2007 physics results 1 strike point control dynamics supported by office of science college...

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