Title: Performance Analysis Using Genesis 1.3
1Performance Analysis Using Genesis 1.3
- Sven Reiche
- LCLS Undulator Parameter Workshop
- Argonne National Laboratory
- 10/24/03
2Overview
- Modeling in Genesis 1.3
- SASE - Performance
- Undulator Taper
- Tolerance Study
3Modeling - Electron Beam
- Using Design Parameter
- Flat profile (70 mm FWHM)
- Current of 3.4 kA
- Normalized emittance of 1.2 mm.mrad
- RMS energy spread of 5.5 MeV
- No variation of beam parameters along bunch
- No runs with start-end distributions
- Correct bunching statistic up to 3rd harmonics
- Up to 20000 Slices à 32000 macro particles for
full bunch ( 700 million macro particles) - 2 weeks of CPU time on single node 1.7 GHz
processor
4Modeling - Undulator
- For SASE simulations (Dz8.lu)
- Module length 112.lu
- Quadrupole length 8.lu (gradient 12.74 T/m /
-12.59 T/m) - Drift length 16.lu (no super-period)
- Energy loss by SR and taper excluded.
- For taper simulations (Dz4.lu)
- Similar as above but with super-period
- Drift length 16/16/20.lu
- Stepwise taper (constant field per module)
- For field error simulations (Dzlu/2)
- Steady-state simulation only
- For simpler analysis no drift spaces
5Modeling - Wakefields
- 3 mm bore radius
- Copper plated chamber
- 100 rms roughness with 5001 aspect ratio
Transient amplitude reduced from 250 keV/m to 180
keV/m, but longer transient region (20 mm)
Flat current profile
6Modeling - FEL Process
- SASE Process at Ångstrom level very CPU
intensive. Full bunch simulation only for 1.0,
1.5 and 15 Å, with and without wake fields. - Subsection of about a third of full bunch length
used for tapered SASE FEL at 1.5 Å. - Dependence on emittance, energy spread, beam
offsets and field errors in steady-state mode
(FEL amplifier). Change in saturation power,
saturation length or gain length with respect to
ideal case.
7SASE-Results
Wavelength Sat. Power Sat. Length Gain Length Trans. Coh.
1.0 Å 1.5 GW 122 m 10.96 m 96 m
1.5 Å 2.9 GW 103 m 7.38 m 65 m
15 Å 8.3 GW 35 m 1.95 m 17 m
Wakefields included. Gain length determined by
linear fit to exponential growth of radiation
power. Transverse coherence obtained from
statistic of instantaneous power.
15 Å
1.5 Å
1.0 Å
8Wakefield Impact
- Reduction of up to 50
- 25 by gap in profile due to transient in wake
potential - 25 by slight energy loss of 30 keV/m at core
of bunch
1.0 Å
15 Å
1.5 Å
9Quantum Fluctuation
- Lower undulator parameter and beam energy reduce
impact of quantum fluctuation, although not a big
effect even for the old design.
Increase of Dsg of 0.9 over 80m for 1.0 Å case.
15 Å
1.5 Å
1.0 Å
10Profile and Spectrum at 1.0 Å
- Gap in profile and shift in resonant wavelength
due to wakefields.
11Profile and Spectrum at 1.5 Å
- Gap in profile and shift in resonant wavelength
due to wakefields.
12Profile and Spectrum at 15 Å
- Impact of wakefields strongly reduced.
- Strong sideband instability in deep saturation
regime.
13Bandwidth
- Growth of bandwidth for 15 Å case by factor of 3
in deep saturation regime.
15 Å
1.0 Å
1.5 Å
14Bunching
- New shot noise algorithm in Genesis
- Growth of bunching at higher harmonics does not
agree with theory at short wavelength (needs
investigation)
15 Å
1.5 Å
1.0 Å
15Bunching Statistic at 1.0 Å
16Bunching Statistic at 1.5 Å
17Bunching Statistic at 15 Å
18Taper
- Taper required to compensate for losses due to
the spontaneous radiation. - Additional taper can be applied to increase
performance.
SASE-run of 20 mm subsection of bunch at 1.5 Å
(wakefields excluded).
No SR no taper Taper compensating SR Additional
taper after 90 m
19Taper (cont)
Wavelength Taper Gradient Post Saturation
1.0 Å -1.15.10-5m-1 -
1.5 Å -9.27.10-6m-1 -9.76.10-5m-1
Taper for 1.5 Å SASE run
Steady-state model
Blue - 1.5 Å / Red - 1.0 Å Solid - taper
optimized Dot - optimized for other
wavelength.
20Emittance Dependence
- Most Sensitive Parameter!
- Saturation beyond LCLS undulator length of 120 m
for 1.0 mm.mrad at 1.0 Å and 1.4 mm.mrad at 1.5 Å.
1.0 Å
1.5 Å
15 Å
21Energy Spread Dependence
- Rather weak dependence (phase spread is dominated
by emittance effect). - 1.0 Å case does not saturate for any value of the
energy spread.
1.0 Å
1.5 Å
15 Å
22Field Errors and Related
- Field errors effects the FEL process by
- Degraded synchronizations between electron beam
and radiation field (phaseshake) - Exitation of trajectory distortion (overlap)
- Both effects are coupled by are differently
exited, depending on the cause (pole field
errors, quadrupole misalignment, undulator
misalignment, initial offsets and angle).
Overlap
Phaseshake
Initial Offsets
Correlated Errors
Uncorrelated Errors
Undulator Misalignment
Quad Misalignment
23Offset Tolerances at 1.5 Å
- Due to large period length of betatron
oscillation, an initial offset has almost no
impact on the longitudinal synchronization except
for a constant slow-down, which is compensated by
a higher energy (or self-adjustment for SASE FEL).
No Saturation
24Phaseshake
- Ponderomotive phase q(kku)bzt-wt depends
implicitly on the undulator field and residual
betatron motion. The collective change in the
phase is given by
Daw 1 rms Dxlt100 nm rms (correlated errors)
A linear change in Dq is compensated by a change
in the mean energy. After subtracting the linear
fit the phase shake is obtained.
25Phaseshake (cont)
- Saturation power and length difficult to estimate
for large field errors. Use integrated gain
length instead. - Results for correlated errors with a trajectory
distortion below 100 nm rms.
1
0.1
0.01
26Tolerance Summary
Values indicate a successful operation to reach
saturation within the 125 m of the LCLS
undulator.
Wavelength 1.0 Å 1.5 Å 15 Å
Emittance lt 1.1 mm.mrad 1.4 mm.mrad gt 2.1 mm.mrad
Energy Spread 0.02 0.04 gt 0.15
Orbit - 17 mm -
Phaseshake - 1.2 rad -
27Summery
- Saturation of SASE FEL at 15 and 1.5 Å, close to
saturation for 1 Å - Compared to old design saturation length
increases by 20m and power drops by 50 - Degradation of up to 50 by wakefields
- Additional tapers after saturation push output
power to 20 GW. Maximal change of field due to
extra taper is 0.3 - Tighter tolerances for emittance, energy spread,
but reduced for beam orbit - Start-end simulation not done yet.