J. Branlard ALCPG11 – 19-23 March 2011 – Eugene OR, USA Results from 9mA studies on achieving flat gradients with beam loading P K |Q L studies at FLASH.

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Presentation transcript:

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Results from 9mA studies on achieving flat gradients with beam loading P K |Q L studies at FLASH during the Feb test in DESY J. Branlard ALCPG11 – March 2011 – Eugene OR, USA

OVERVIEW Problem statement and historical background – Why do we care about individual flat gradients? – What solutions were offered to achieve flat gradients with beam loading? – What can we actually implement at FLASH? The Feb.’11 study at FLASH – What approach have we followed during the FLASH test studies? – Results of the P K |Q L studies Conclusions and lessons learnt – Study insights – Approach limitations – Improvements 2

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Introduction: problem statement Why do we care about individual flat gradients? “Effect of Cavity Tilt and RF Fluctuations to Transverse Beam Orbit Change in ILC Main Linac” K. Kubo, Jan all Q L  3x10 6 no beam no tilts all Q L  3x10 6 I b = 3 mA tilts +/- 2MV/m +/- 10 % 3 FLASH ACC6 & ACC7

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Introduction: problem statement FNAL approach to cavity quench due to beam ON/OFF operations “Optimal Coupler and Power Settings for Superconductive Linear Accelerators”, J. Branlard, B. Chase, Linac  produces fixed P K /Q L settings (unique to each cavity) which is safe for all beam loadings (i.e. no tuning action required to prevent quench)  individual cavities gradients have tilts with beam Beam OFF Beam ON

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Introduction: problem statement Published “solutions” to flat cavity gradient with beam “RF Distribution Optimization in the Main Linacs of the ILC” Bane, Adolphsen, Nantista - WEPMS037.pdf, 2007  Assumes a square forward power pulse  Assumes adjustable P K ’s 5

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Problem space at FLASH  Focus on ACC6 and ACC7  Motorized couplers (Q L adjustments, limited range)  Fixed power distribution (i.e. P K ), except for 3dB hybrid  Motorized static tuners  Dynamic cavity resonance control with piezo Introduction: problem statement 6

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Introduction: problem statement Published “solutions” to flat cavity gradient with beam “PkQl-like control for ACC6/7 at FLASH” PkQl_FLASHver3.docxShin Michizono, Sept “To flatten the cavity gradient for ACC6/7” FLASH101022BV2.pdfShin Michizono, Nov  solves the same problem but using existing P K distribution  no PK adjustments for different beam loading, only Q L changes  version1: assumes a square forward power pulse yield very low Q L values  version2: assumes a fill time / flat top power step yield Q L values within acceptable range 7

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Introduction: problem statement Published “solutions” to flat cavity gradient with beam “PkQl-like control for ACC6/7 at FLASH” PkQl_FLASHver3.docxShin Michizono, Sept “To flatten the cavity gradient for ACC6/7” FLASH101022BV2.pdfShin Michizono, Nov  solves the same problem but using existing P K distribution  no PK adjustments for different beam loading, only Q L changes  version1: assumes a square forward power pulse yield very low Q L values  version2: assumes a fill time / flat top power step yield Q L values within acceptable range 8

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA FLASH studies: 5 shift overview no beam, low gradient Friday 2/4 night shift: no beam, low gradient – no beam – ACC6/7 vector sum calibration 100 bunches, 1 MHz, 1.6 nC – QL tuners characterization for ACC6/7 – simulator calibration to reflect ACC6/7 power distribution 1 mA, low gradient Saturday 2/5 night shift:1 mA, low gradient – 1mA beam, low gradient (100 MeV – 200 MeV) – Successfully implemented QL adjustments to flatten cavity gradients – beam loading tilts correction (all tilts below 1%) using simulator predicted values – Simulated values are reliable 1.6 mA, mid-gradient Sunday 2/6 night shift:1.6 mA, mid-gradient – 1.6mA beam, low gradient (200 MeV) – low gradient, beam loading tilts Q L correction (below 1%) – beam current scan – QL scan 3.0 mA mA, mid and high gradient Monday 2/7 night shift:3.0 mA mA, mid and high gradient – 3.0mA beam, 200 MeV – QL adjusted for gradient flat at 3mA – beam scan from 0.9 to 4.5 mA – 4.5mA beam, 300 MeV – QL adjusted for gradient flat at 4.5 mA – beam current scan 4.2 mA, highest gradient Tuesday 2/8 afternoon shift:4.2 mA, highest gradient – 4.2mA beam, 360 MeV – Lorentz force detuning compensation – Use calculator to predict QL  gives very accurate prediction – Flatten ACC6/7 gradients tilts to ~ 1.5% – beam current scan 9

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA ACC6 & ACC7 Q L settings limits ACC6cav1cav2cav3cav4cav5cav6cav7cav8 Q L min [x10 6 ] Q L max [x10 6 ] ACC7cav1cav2cav3cav4cav5cav6cav7cav8 Q L min [x10 6 ] Q L max [x10 6 ] not “hard” limits 10

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Fermilab Beams Doc database: Beams-doc

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Fermilab Beams Doc database: Beams-doc

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Calibration procedure 1.Load V cav from DAQ 2.Compute actual Q L, P K and  f from DAQ data 3.Type in Q L, P K and  f into simulator 4.Check agreement between simulated and FLASH data 5.Adjust Q L in simulator to flatten tilts 6.Implement Q L corrections in FLASH 7.Check gradient flatness DAQ data: Feb , 22:37 I b = 4.5 mA FLASH DAQ data 13 (retune cavities if needed)

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Calibration procedure 1.Load V cav from DAQ 2.Compute actual Q L, P K and  f from DAQ data 3.Type in Q L, P K and  f into simulator 4.Check agreement between simulated and FLASH data 5.Adjust Q L in simulator to flatten tilts 6.Implement Q L corrections in FLASH 7.Check gradient flatness simulated data vector sum 14 (retune cavities if needed)

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Calibration procedure 1.Load V cav from DAQ 2.Compute actual Q L, P K and  f from DAQ data 3.Type in Q L, P K and  f into simulator 4.Check agreement between simulated and FLASH data 5.Adjust Q L in simulator to flatten tilts 6.Implement Q L corrections in FLASH 7.Check gradient flatness FLASH DAQ data simulated data vector sum 15 (retune cavities if needed)

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Calibration procedure 1.Load V cav from DAQ 2.Compute actual Q L, P K and  f from DAQ data 3.Type in Q L, P K and  f into simulator 4.Check agreement between simulated and FLASH data 5.Adjust Q L in simulator to flatten tilts 6.Implement Q L corrections in FLASH 7.Check gradient flatness simulated data vector sum 16 (retune cavities if needed)

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Calibration procedure 1.Load V cav from DAQ 2.Compute actual Q L, P K and  f from DAQ data 3.Type in Q L, P K and  f into simulator 4.Check agreement between simulated and FLASH data 5.Adjust Q L in simulator to flatten tilts 6.Implement Q L corrections in FLASH 7.Check gradient flatness simulated data vector sum 17 (retune cavities if needed)

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Calibration procedure 1.Load V cav from DAQ 2.Compute actual Q L, P K and  f from DAQ data 3.Type in Q L, P K and  f into simulator 4.Check agreement between simulated and FLASH data 5.Adjust Q L in simulator to flatten tilts 6.Implement Q L corrections in FLASH 7.Check gradient flatness FLASH DAQ data simulated data vector sum 18 (retune cavities if needed)

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA (retune cavities if needed) Calibration procedure 1.Load V cav from DAQ 2.Compute actual Q L, P K and  f from DAQ data 3.Type in Q L, P K and  f into simulator 4.Check agreement between simulated and FLASH data 5.Adjust Q L in simulator to flatten tilts 6.Implement Q L corrections in FLASH 7.Check gradient flatness FLASH DAQ data simulated data vector sum 19

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Assessing the accuracy of the model Q L scan  Keep beam current constant but walk Q L ’s around optimized value I B scan  Keep optimized Q L ’s but ramp beam up/down  Q L gradient tilts [%] 20

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Assessing the accuracy of the model Q L scan  Keep beam current constant but walk Q L ’s around optimized value I B scan  Keep optimized Q L ’s but ramp beam up/down 21

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Beam scans Su 02/06 night shiftMo 02/07 night shift Tu 02/08 afternoon shift 200 MeV 1.6mA 200 MeV 3.0mA 300 MeV 4.5mA 360 MeV 4.5mA 22

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA The analytical solution  assumes “perfect” tuning  solve for Q Li when possible cavity i loaded Q cavity i forward power during fill time [W] DC beam current [A] fill time (  beam arrival time) [s] fill time to flat top voltage ratio (including beam compensation) Given a fixed power distribution, a known beam current and beam compensation, find individual Q L ’s that will flatten cavity gradients during beam time * “Note on solving QL for flat gradients at FLASH ACC6 and ACC7”, J. Branlard, Feb 2011, FNAL Beams-doc-3796 “Analytical solution to the cavity tilt problem.docx”, G. Cancelo, Feb 2011 * 23

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Beam ON/OFF DAQ data 02/08 5:46:14DAQ data 02/08 5:51:36 Ib = 4.5 mAIb = 0 mA  Cavities below vector sum rise without beam  Cavities above vector sum drop without beam  Need for an automatic safety feature to shorten RF pulse to prevent quench 24

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Study insights What went well Very stable machine  long study time Motorized couplers / tuners  optimal study conditions automated scripts + skilled operators Simulator proved to be very useful Predicted optimized Q L values were accurate  to 0.2e6 Successfully implemented the tuning plan  tilts < 0.1MV/m What we’ve learnt Cavity resonance control is crucial for gradient tilts Limitations to the simulation approach: – How accurately can we measure the power distribution?  John’s slide – How accurately can we compensate for LFD OR include in model?  next slide – How accurately can we measure and set Q L ’s  +/- 2 to 5% – Fine tuning “by-eye” is compromised by operating in closed loop What is still unanswered No proposed solution for high beam currents (>6mA) implementable at FLASH There is not always a solution to flatten all cavities (especially when gradient spread is large) No solution to bring up the machine at its highest gradient 25

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA 26 Before freq. tuner adjustmentsAfter freq. tuner adjustments AMPLITUDE PHASE ~ 0.1 MV/m Q L = 1.58x10 6  f = 70 Hz

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Bringing up a linac Traditional approach (i.e. FLASH) 1.Make target gradient with FF 2.Turn FB on 3.Compensate for LFD 4.Send a couple of pilot bunches (~10) (automated beam loading compensation) 5.Minimize losses 6.Gradually increase bunch length to full train (while minimizing beam losses) 7.Learning feed forward 1.Bring cavity to their nominal gradient  typically: quench gradient -2-3 MV/m 2. Adjust Q L so cavities are flat with beam  cavity will quench (because no beam) 3. Shorten pulse length to avoid quench  typically <200 usec for high beam currents Q L ’s  can’t see LFD effects (can’t compensate for LFD)  can’t walk pilot bunch across flat top 4. As you increase bunch length  increase flat top length  compensate for LFD  minimize losses 5. The LLRF quench monitoring system should  truncate the flat top length to prevent quenches  every time bunch train is shorter than expected One “possible” scenario for flat gradients 27

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA References “RF Distribution Optimization in the Main Linacs of the ILC”, Bane, Adolphsen, Nantista - WEPMS037.pdf “Optimal Coupler and Power Settings for Superconductive Linear Accelerators”, J. Branlard, B. Chase, Linac 2008 “Optimizing Cavity Gradient in Pulsed Linacs Using the Cavity Transient Response”, G. Cancelo, A. Vignoni, Linac 2008 “Effect of Cavity Tilt and RF Fluctuations to Transverse Beam Orbit Change in ILC Main Linac”, K. Kubo, Jan “PkQl-like control for ACC6/7 at FLASH” S. Michizono, PkQl_FLASHver3.docx, Sept “To flatten the cavity gradient for ACC6/7” S. Michizono, FLASH101022BV2.pdf, Nov “Analytical solution to the cavity tilt problem.docx”, G. Cancelo, Feb 2011 “Note on solving QL for flat gradients at FLASH ACC6 and ACC7”, J. Branlard, FNAL Beams-doc-3796 SIMCAV version 4.8 (FLASH ACC6 and ACC7 16 cavity MATLAB simulator), FNAL Beams-doc

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA THANK YOU 29

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA BACKUP SLIDES 30

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA SUMMARY Why do we care about individual flat gradients? – KEK paper What can we actually implement at FLASH? – No P K adjustments – Only Q L can be changed – Limited range in Q L changes What solutions were offered to achieve flat gradients with beam loading? – SLAC paper, using Q L and P K adjustments – Shin’s solution with square P fwd pulse – Shin’s solution with step ratio P fwd pulse What approach have we followed during the FLASH test studies? – Procedure (issues with adjusting Q L when beam is OFF) – When beam is ON, beam compensation is ON too – Which tools did we use – The analytical solution Results of the P K |Q L studies – Assess Q L ranges – Low gradient / mid gradient – Low beam / mid beam current – Beam scans – Q L scans Conclusions and lessons learnt – How accurate were the tuning adjustments? – What limited the accuracy of tuning adjustments? – Difference between solving the problem open / close loop – Impact of detuning on tilts (static & dynamic) – No solution to bringing the machine up to its maximum gradient 31

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Shift-by shift highlights 32

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Friday 2/4 night shift – highlights: no beam ACC6/7 vector sum calibration 100 bunches, 1 MHz, 1.6 nC Q L tuners characterization for ACC6/7 simulator calibration to reflect ACC6/7 power distribution 33

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Q L = 3e6Q L = 2.65e6 Saturday 2/5 night shift – highlights: 1mA beam, low gradient (100–200 MeV) Successfully implemented QL adjustments to flatten cavity gradients beam loading tilts correction (all tilts below 1%) using simulator predicted values Simulated values are reliable 34

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Sunday 2/6 night shift – highlights: 1.6mA beam, low gradient (200 MeV) beam loading tilts Q L correction (below 1%) (several cavities at once, with beam on) beam current scan Q L scan Ql config is for ACC7: cav1 : 2.8 e6 cav2 : 2.8 e6 cav3 : 2.8 e6 cav4 : 2.8 e6 cav5 : 2.5 e6 cav6 : 2.5 e6 cav7 : 3.1 e6 cav8 : 3.2 e6 35

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Monday 2/7 night shift – highlights: 3.0mA beam, 200 MeV Q L adjusted for gradient flat at 3mA beam scan from 0.9 to 4.5 mA 4.5mA beam, 300 MeV QL adjusted for gradient flat at 4.5 mA beam current scan 36

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA ACC7 Q L values Predicted Implemented cav e6 cav e6 cav e6 cav e6 cav e6 cav e6 cav e6 cav e6 Beam OFF Beam ON Tuesday 2/8 afternoon shift – highlights: 4.2mA beam, 360 MeV Lorentz force detuning compensation Use calculator to predict QL  very accurate prediction Flatten ACC6/7 gradients tilts to ~ 1.5% (tuned for 4.2mA) beam current scan to 4.5 mA ACC6 ACC7 37

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA Power ratios 38 Power ratio (dB)

J. Branlard ALCPG11 – March 2011 – Eugene OR, USA 3 sequences of detuning: cav1, then cav2 then cav3. when we reach the end of the detuning range of one cavity, the detuning of the adjacent cavity is affected Q L changes with the detuning for all three cavity (cav1 and 2 in one direction, cav3 in the opposite direction) We see that Q L (cav1) and Q L (cav2) are coupled. Similarly, Q L (cav3) and Q L (cav4), but no cav3-cav1 coupling Power coupling between adjacent cavities 39