ILC Curved Linac Simulation

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July 19-22, 2006, Vancouver KIRTI RANJAN 1 ILC Curved Linac Simulation Kirti Ranjan, Francois Ostiguy, Nikolay Solyak Fermilab + Peter Tenenbaum (PT) SLAC

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ILC Curved Linac Simulation. Kirti Ranjan, Francois Ostiguy, Nikolay Solyak Fermilab + Peter Tenenbaum (PT) SLAC. OVERVIEW. ILC BCD Curved LINAC Simulation : Dispersion Free Steering (DFS) DFS : Sensitivity studies Failure Mode Analysis in DFS: BPM / Corrector Failure - PowerPoint PPT Presentation

Transcript of ILC Curved Linac Simulation

Page 1: ILC  Curved Linac Simulation

July 19-22, 2006, Vancouver KIRTI RANJAN 1

ILC Curved Linac SimulationKirti Ranjan, Francois Ostiguy, Nikolay Solyak

Fermilab+

Peter Tenenbaum (PT)SLAC

Page 2: ILC  Curved Linac Simulation

July 19-22, 2006, Vancouver KIRTI RANJAN 2

OVERVIEW

ILC BCD Curved LINAC Simulation : Dispersion Free Steering (DFS)

DFS : Sensitivity studies

Failure Mode Analysis in DFS: BPM / Corrector Failure

Different No. of BPMs

Emittance Bumps

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July 19-22, 2006, Vancouver KIRTI RANJAN 3

Curved ILC-BCD LINAC

Length (m) : 10417.2m N_quad : 240 N_cavity : 7680N_bpms : 241N_Xcor : 240 N_Ycor : 241N_gkicks : 1920

A constant focusing lattice with a quadrupole spacing of 32 cavities and x/y phase advance of 75/60 per cell ( ILC BCD - 1Q / 4CM)

Modifications in LIAR code to simulate the earth curvature: The curvature is simulated by adding kinks between the cryo-modules - GKICK

“Design Dispersion (from earth curvature)” : The matched dispersion condition at the beginning of the linac is artificially introduced into the initial beam and is propagated through linac using transfer matrices

PT’s ILC BCD-like lattice distributed during ILC-LET workshop at CERN (Feb.2006)

Page 4: ILC  Curved Linac Simulation

July 19-22, 2006, Vancouver KIRTI RANJAN 4

LIAR Simulation: CURVED LINACO

rbit

at

the

YC

OR

s (

m)

Zoom

No

rmal

ized

Em

itta

nce

(n

m)

Design Y – dispersion (m)

Design Yp - dispersion

BPM index

BPM index

BPM index

• No misalignmentsOrbit at the Central CM b/w two “CM w/ Quads” ~ 35 m

Corrected: “Design y-Dispersion Corrected”

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Nominal Misalignment tolerances

Tolerance Vertical (y) plane

BPM Offset w.r.t. Cryomodule 300 μm

Quad offset w.r.t. Cryomodule 300 μm

Quad Rotation w.r.t. Cryomodule 300 μrad

Cavity Offset w.r.t. Cryomodule 300 μm

Cryostat Offset w.r.t. Survey Line 200 μm

Cavity Pitch w.r.t. Cryomodule 300 μrad

Cryostat Pitch w.r.t. Survey Line 20 μrad

BPM Resolution 1.0 μm

BPM transverse position is fixed, and the BPM offset is w.r.t. Cryostat Only Single bunch used Steering is performed using Dipole Correctors

1st 7 BPMs have 30 m RMS offset w.r.t. Cryostat

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July 19-22, 2006, Vancouver KIRTI RANJAN 6

Dispersion Free (or Matched) Steering

1:1 steering is performed - steer to obtain the nominal, design readings of the BPMs

DFS - Linac is divided into 18 segments (w/ 50% overlap) & 1st DF segment starts from 8th BPM Measure two orbits –

(i) y(0) : one for the nominal energy.

(ii) y() : other by switching off cavities upstream of the segment (maximum energy

change for a given segment is 20% of the nominal energy at the upstream end of the

segment, or 18 GeV, whichever is smaller.)

In both cases 3 BPMs upstream of each segment (used for fitting the incoming beam

trajectory) are included in the measurement.

Simultaneously minimize the Measured dispersion and RMS value of BPM readings

res = sqrt(2) * BPM resolution

BPM = BPM offset

Where

1m

300 m

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July 19-22, 2006, Vancouver KIRTI RANJAN 7

Dispersion Free Steering - Results

Misalign the beamline components and perform the DF steering

CURVED vs. STRAIGHT LINAC

Dispersion Free Steering : mean of 50 seeds

Straight

Curved

Co

rre

cte

d n

orm

aliz

ed e

mitt

anc

e (

nm)

DFS parameters not optimized for Curved Linac

Mean: 5.0 ± 0.4 nm

90%: 8.7 nm

Laser Straight

Mean: 5.3 ± 0.5 nm

90%: 9.5 nm

Curved

Distribution of emittance growth for 50 seeds

Nominal misalignments as mentioned in Page 4

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DFS: Sensitivity studiesC

orr

ect

ed

em

itta

nce

(n

m)

Quad offset sensitivity

Co

rre

cte

d e

mitt

an

ce (

nm

)

Cavity offset sensitivity Cavity pitch sensitivity

Co

rre

cte

d e

mitt

an

ce (

nm

)

BPM offset sensitivity BPM resolution sensitivity

CM offset sensitivityQuad roll sensitivity

CM pitch sensitivity

Vary one misalignment from its nominal value - keeping all other misalignments at their nominal values

90%Mean

Sensitive to Cavity pitch, BPM resolution, CM offset, Quad roll

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July 19-22, 2006, Vancouver KIRTI RANJAN 9

Beam and Quad Jitter Sensitivity

Quad strength error (dK)

Mean 90%

0.5 e-3 7.43±0.46 11.7

1e-3 7.44±0.46 11.5

2.5e-3 7.50±0.46 11.5

5e-3 7.70±0.46 11.9Beam jitter (sigma)

Quad Strength error

Cor

rect

ed e

mitt

ance

(nm

)

Beam Jitter sensitivity

Cor

rect

ed e

mitt

ance

(nm

)

90%Mean

Quad Jitter sensitivity

DFS: Sensitivity studies

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July 19-22, 2006, Vancouver KIRTI RANJAN 10

DFS: Contributions50 seeds mean 90%

Nominal 5.26 ± 0.38 9.47

Dispersion only 1.99 ± 0.24 4.22 Switch off wakes & quad roll

Wakes only 1.8 ± 0.17 3 Cavity offset & wakes only

Quad roll only 1.47 ± 0.13 2.83 quad roll only

Total 5.26 10.05

Individual misalignment (30 seeds) mean err 90%

CM pitch only 0.25 0.036 0.56

Cavity pitch only 2 0.35 4.3

Front bpm offset only 0.41 0.0493 0.77

Quadroll only 1.39 0.13 2.37

Cavity offset only 1.67 0.18 2.98

BPM resolution only 0.43 0.0548 0.76

BPM offset only 0.2 0.0107 0.28

Quad offset only 0.17 0.0026 0.19

Sum 6.52 12.2

A systematic contribution seems to add up in each case, which is added only once when we perform the nominal run

~ 0.2 nm

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Failure Mode Analysis (ILC BCD Curved Linac)10 seeds; Curved Linac; 1 BPM reading = 0 and is used in the DF steering

BPM # 50 BPM # 100

Dispersion corrected emittance growth (nm-rad) vs. BPM index

BPM # 50 BPM # 150

Case2: Faulty BPM and associated YCOR not used in steering

(1) If you know the position of faulty BPM and exclude it from the steering then the results are fine(2) However, if you use that faulty BPM in finding the corrector settings, then the emittance dilution is significant.

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Failure Mode Analysis (ILC BCD Curved Linac)Case 1: Perfectly straight Linac (1 Y - CORRECTOR NOT WORKING (kick =0) :# 49 )

Vertical Orbit at the Y-correctors (m)

Y – Dispersion (m)Dispersion corrected emittance growth (m-rad)

In a perfectly aligned Linac, if one YCOR doesn’t work according to it’s designed value – then both the trajectory and emittance dilution are significantly worse

Adjusted the adjacent two correctors (upstream and downstream) to guide the beam on to the designed orbit – we know which corrector is failed!

Vertical Orbit at the Y-correctors (m)

zoom

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Not corrected

Perfect Linac - vertical plane - Projected Normalized Emittance (m-rad)

5 - seeds 10 - seeds

Case 1: Failed Corrector used in finding the correction-settings; but correction is not applied to the failed corrector

Case 2: Failed Corrector NOT used in finding the correction-settings;

Nominal misalignment ; Dispersion Free Steering;

Dispersion corrected

Dispersion corrected –

emittance growth (nm-rad)

Failure Mode Analysis (ILC BCD Curved Linac)

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July 19-22, 2006, Vancouver KIRTI RANJAN 14

5 Y-CORRECTORS NOT WORKING – randomly chosen - CORRECTORS NO. 50,76,106,150,200(one corrector failure in one DF segment)

Vertical Orbit at the Y-correctors

Adjusted the adjacent two correctors to guide the beam on to the correct orbit

< 6 nmDispersion corrected – emittance growth (nm-rad)

Nominal misalignment ;

Dispersion Free Steering;

Failure Mode Analysis (ILC BCD Curved Linac)

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Using BPM in every CM or in every Cavity : Presently we are using BPM in only Quad package along w/ Corrector. (a) What if BPM is there at the centre of every CM? (b) what if each cavity can be read out as BPM – BPM in every cavity?

BPM in every CMBPM w/ YCORCURVED

Dispersion Corrected Emittance Growth vs. BPM index

50 seeds All the seeds have < 10 nm emittance growth

~4nm~5nm

No. of BPMs

BPM in every Cavity

~4nm~5nm

BPM in every alternate CM

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Emittance BumpsCurved ILC BCD Linac; 50 seeds One Bump:

Bump (starting at energy = 16.16 GeV) Cor1: Coeff= 3.3163e-07Cor2 (180 deg apart):Coeff=3.3163e-07*sqrt (energy2 / energy1)

Cor3 (90 deg from 1st Ycor): Coeff= 4.2299e-07Cor4:Coeff=4.2299e-07*sqrt (energy4 / energy3)

0

2

4

6

8

10

12

14

16

-600 -400 -200 0 200 400 600

Scan range (arbitrary units)

beam

siz

e ̂2

(um

^2)

Corrected Emittance Growth (nm) vs. BPM Index

Before Bumps

After Bumps

2% error on beam size measurement

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July 19-22, 2006, Vancouver KIRTI RANJAN 17

PLAN

Continue w/ dispersion + wake bumps in curved linac Perform the studies in the Final Main Linac Lattice

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July 19-22, 2006, Vancouver KIRTI RANJAN 18

Several Y-CORRECTORS NOT WORKING – randomly chosenCorrectors not used in the steering

Vertical Orbit at the Y-correctors (m)

Nominal misalignment; DMSDispersion corrected emittance dilution (nm-rad);

< 6 nm

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July 19-22, 2006, Vancouver KIRTI RANJAN 19

2 consecutive BPM/YCOR removed

15,16 40,41

WHAT IF Consecutive BPM / YCORs are not working and not used in finding the corrector settings?

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3 consecutive BPM/YCOR removed

15,16,17 40,41,42

100,101,102

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4 consecutive BPM/YCOR removed

15,16,17,18 40,41,42,43

100,101,102,103

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Straight Linac; 30nm RMS (white noise) Quad vibration (no other error); 50 seeds

Ybpm_readings at the end of the linac vs. seed no.

Y_beam_size at the end of the linac= 2.5 e -6 m

= 1.06e-6 m

Beam jitter at the end of the Linac for 30 nm RMS Quad vibration