beam instrumentation for orbit stability i. pinayev

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Beam Instrumentation for Orbit Stability I. Pinayev

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Page 1: Beam Instrumentation for Orbit Stability I. Pinayev

Beam Instrumentation for Orbit Stability

I. Pinayev

Page 2: Beam Instrumentation for Orbit Stability I. Pinayev

Complement of Storage Ring Diagnostics/Beam Instrumentation

Monitor Quantity Function4-button pick-ups 226 Beam position, dispersion, response matrix,

turn-by-turn dynamicsStripline pick-up 1 Longitudinal and transverse frequency

componentsTune monitor 1 Betatron tunes measurement, impedanceLoss monitors 10 Beam losses monitoring Fluorescent flags 4 Position and profile of injected beam Transverse feedback 2 Suppress beam instabilitiesStreak-camera 1 Bunch length measurementDCCT 2 Beam current measurementFCT 2 Filling pattern monitoringBeam scrapers 4 Machine studies (beam size, energy aperture),

haloFireWire camera 1 Transverse beam characteristicsEmittance monitor 1 Transverse beam sizesUndulator radiation 1 Energy spread, beam divergence, momentum

compaction factorPinhole camera 1 Horizontal emittance (using undulator radiation)Counter 1 RF frequency monitorPhoton BPMs 10 Photon beam angle and position

Page 3: Beam Instrumentation for Orbit Stability I. Pinayev

RF BPMs

• Design similar to one adopted at RHIC• 5-mm radius buttons• Stray capacitance 1-4 pF

(2π×500MHz×50Ω×3pF≈0.5)• Signal level -1.1 dBm for 500 mA at 500

MHz• Dependence of vacuum chamber

shape/size and button capacitance (and hence sensitivity) on fill pattern and circulating current can be significant

• Switch to strip-line geometry?• Electronics front-end overload• Monitors of the vacuum chamber position

can be affected by the EM noise• Other factors?

Page 4: Beam Instrumentation for Orbit Stability I. Pinayev

Processing Units

• Utilized at Elettra, NSSRC, Diamond, Soleil, PLS • Fast acquisition 10 kHz sampling rate, 2 kHz BW• Slow acquisition: 10 Hz sampling rate, ~4 Hz BW• 32 bit data• RMS uncertainty (for 10 mm scale in 1 kHz BW) -90.5dB

→0.3µm @ Pin = -20 dBm • 8-hour stability (ΔT=±1°C) -80dB→1µm • Temperature drift (T=10–35°C) -94dB/°C → 0.2µm/°C • MTBF ≥ 100,000 hours• For 270 units failure rate will be one unit in 17 days

• Can filtering improve RMS uncertainty to required level?

• Spares?• In-situ calibrators?• Other receivers?

Page 5: Beam Instrumentation for Orbit Stability I. Pinayev

Photon Beam Position Monitors

• Will provide information on photon beam position and angle (to account for errors in the wiggler field)

• Use of photon BPMs will allow sub-microradian pointing stability

• Contamination with dipole radiation can be of less concern due to reduced magnetic field in the bending magnet

• Can be used for orbit feedback and/or control of users optics

• 2D translation stages will precisely locate the photon BPM

• Should withstand high power density• Response time?• Noise susceptibility?• Other sensors: CVD diamond photoresistors,

bolometers, etc?

Page 6: Beam Instrumentation for Orbit Stability I. Pinayev

Photon Beam Intensities for Dipole and Undulator

• E=3 GeV• ρ=25 m• B= 0.4 T

• εc=2.4 keV

• λc=0.52 nm• ψ=1/γ=0.17 mrad

• Ptot=143 kW (@ 0.5 A)

• U19: λU=19 mm

• K=1

• LU=3 m (NU=158)

• λU=0.4 nm

• εU=3.1 keV

• σr′≈(λU/LU)½=11.5 μrad

• Ptot=2.7 kW (@ 0.5 A)

213.0mrad

kW

d

dP

Low dipole field – do we need Decker distortion?

220mrad

MW

d

dP

Page 7: Beam Instrumentation for Orbit Stability I. Pinayev

Back-Fluorescent Hard X-ray BPMs

• Hard X-rays hit Cu target which re-radiates 8.05 keV photons

• Insensitive to dipole radiation• High level signals• 12 keV photons are presently

tested• A lot of R&D still required• Can we extend range down to

softer X-rays?

Presented by G. Decker at BIW’06

Page 8: Beam Instrumentation for Orbit Stability I. Pinayev

Diagnostics with Synchrotron Radiation

• FireWire Camera eliminates need for frame-grabber– Exposure from 20 μs– Trigger jitter ±10 ns– 120 fps (full resolution)– 463 fps (100×100 ROI)

• Position sensitive diodes provide signal proportional to the displacement of center of gravity– 0.3 μs response time– 0.6 μ position sensitivity– Can be used to monitor beam

motion in the dipole

Page 9: Beam Instrumentation for Orbit Stability I. Pinayev

Auxiliary Equipment

• Two DCCT for monitoring of circulating current• Two fast current transformer for monitoring filling

pattern• What other beam parameters we need to

monitor to insure high stability?

Page 10: Beam Instrumentation for Orbit Stability I. Pinayev

Fast Orbit Stabilization System (FOSS)

• BW ultimately limited by corrector magnets (<500Hz)

• Basic building blocks– Libera Electron– Fast private communication

system– Computational engines– PS interfaces and corrector

magnets• What is optimal configuration?

– reliability– cost– flexibility

Page 11: Beam Instrumentation for Orbit Stability I. Pinayev

Characteristics for FOSS Components

• Available data: amplitudes, positions, status• FPGA communication module is user specific• Synchronization to external clock• Fast network

– 270 Liberas * 72 bytes * 10 kHz = 194 MB/s

• Latency– 1Gb/s: 40 μs on one cable– Processing latency 350 usec

• Reliability of GB switch is a must• Different computational engines are available

Following Tomaž Karčnik from I-Tech