Lessons learned from PEP-II LLRF and Longitudinal Feedback · 2008. 7. 17. · WEOBM02 EPAC June...
Transcript of Lessons learned from PEP-II LLRF and Longitudinal Feedback · 2008. 7. 17. · WEOBM02 EPAC June...
M02 EPAC June 2008
nal Feedback
Jiajing Xu
Wor -AC02-76SF00515
WEOB
Lessons learned from PEP-II LLRF and Longitudi
John D. Fox.
Themis Mastorides, Claudio Rivetta, Dan Van Winkle,
Stanford Linear Accelerator Center
Dmitry Teytelman
Dimtel, Inc.
k supported by the U.S. Department of Energy under contract #DE
M02 EPAC June 2008
ck
Wh
Ori
• L
• L
• D
Wh
• C
• M
• F
Wh
• L
• L
Imp
3 4 5 6ime, ns
ction from a timing sweep at ALS
28−Oct−96
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PEP-II LLRF and Broadband Feedba
at Was Expected?
ginal CDRGoals 1991/1993
LRF
ongitudinal Coupled-Bunch Feedback
esign and Methodology
at Happened?
ommissioning Experience
ajor Upgrades
inal PEP-II operations, performance
at wasn’t foreseen (via 2 examples)
FB - Impact of Noise in processing channel
LRF - Impact of Nonlinear Signal Processing
ortant Lessons Learned -Summary
0 1 2−1.5
−1
−0.5
0
0.5
1
1.5
T
Bea
m r
espo
nse,
au
Kicker response reconstru
M02 EPAC June 2008
Twocircuupd
• Gm
• e
• e
RF
• H
• Imfumin
• R ms
Inst planes
• H ies
• H MHz sampling rate)
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PEP-II
rings of 2.2 kmmference. CDR 1991,
ated 1993
oal of factory e+e- colliderachine L 3E33
- HER 1.5A (0.75/1A 1991)
+ LER 2.14 A (2.14 A 1991)
concerns
igh Beam Loading
pedance of cavityndamental, detuning - low-ode coupled bunchstabilities
eliability -extensive R&D effort in Vacuum, Feedback and RF syste
ability Concerns - operation well beyond stability thresholds in three
OM Impedances of cavities - HOM driven coupled-bunch instabilit
OM Dampers - Still the need for coupled-bunch fast feedback (238
M02 EPAC June 2008
d
Yea ER I LER L199 A 1.0A 1.2E33Run 3.0E33Run 1.7 4.4E33Run 1.9 6.3E33Run 2.5 9.0E33Run 3.0 1.0E34Run 2.9 1.2E34Run 3.0 1.2E34Run 1.2E34
HER tionsThe
HER
LOM damped!)
HOM sign)
The (3.213 A at 3 GeV).
Wer s easy and we overdesigned/ove
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Where we started, Where we finishe
r/run LER stations LER cavities HER stations HER cavities I H8 2 4 4(+1 parked) 16(+4 parked) 0.6 1 2 4 5 20 0.9 1.5 2 3 6 5 20 1.0 3 3 6 6 22 1.1 4 3 6 8 26 1.5 5a 4 8 9 26 1.7 5b 4 8 9 26 1.9 6 4 8 11 28 1.9 7 4 8 11 28 2.1A 3.2A
reconfigured 4 cavity -> two cavity station in Run 3, subsequently added 2 cavity staoperating configuration, gap voltages, tunes, etc. were constantly changing
current -2x design LER Current -1.8x design Luminosity4X design
Growth rates HER 1.2 ms-1 LER 3.0 ms-1 (design - simulation was
growth rates HER3x design LER growth rates 0.45 ms-1 (5.6x de
PEP-II collider holds the record for stored charge in a storage ring
e we successful in the feedback and LLRF areas because it warestimated things?
M02 EPAC June 2008
pology
Tun
Klys
• Rg
• K
Dire
• Cth
• E
• L
Com
• A the residual impedance
Gap
• R oid saturating the klystron ong
Lon des +/- 10
klystron
direct RF loop
comb filtersbeam
RF
BPMlongitudinal multi-bunch
Σ
feedback system
_
ripple loop
mod.
tunerloop
cavities
HVPSklys sat. loop
or
Loop technology
Klys sat -EPICSGap, (ripple) - digital,(Ripple) -analog
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PEP-II low-level RF feedback loops: To
er loops - standard tuning for minimum reflected power
tron operating point support
ipple loop adjusts a complex modulator to maintain constantain and phase shift through the klystron/modulator system.
lystron saturation loops maintain constant saturation headroom
ct feedback loop (analog)
auses the station to follow the RF reference adding regulation ofe cavity voltage
xtends the beam-loading Robinson stability limit
owers the effective fundamental impedance seen by the beam
b filter (digital)
dds narrow gain peaks at synchrotron sidebands to further reduce
feedback loop (digital)
emoves revolution harmonics from the feedback error signal to avap synchronous phase transients
gitudinal feedback uses RF as low-frequency “woofer” kicker for mo
RFreference
to widebandkicker
band limitedkick signal
+mod.
gap loop
stationreference
err
Tuner,Comb.Direct
M02 EPAC June 2008
ated?
LLR iver), Rich Tighe (SLAC)
• L
• C
LLR he, Rivetta, Mastorides)
• M n
• 1 s time windows
Des Dynamic range issues, I&Qmism
100
0.005
0.01
0.015
0.02
0.025
0.03
Mod
Pha
se (
deg)
Open LoopPole
g ∆ l xImpedance control
th
l
x
1/t
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How was required LLRF performance estim
F -Origin and design/modelling F. Pedersen, Stuart Craig (Chalk R
inear frequency domain models
oncerns about non-linear klystron, impact on impedance control
F station model, beam model -nonlinear time domain simulations (Tig
acro-bunch structure, low-mode dynamics with Non-Linear Klystro
994 model - Nocriteria for stability, robustness beyond trajectories in m
ign proceeded based on initial simulations. Little criteria for Noise,atches, other technical imperfections
0
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5
Time (ms)
LER ring − modal analysis
e number
−10 −5 0 5 10−2
−1
0
1
2
Gro
wth
rat
es (
ms−
1 )
−10 −5 0 5 103900
4100
4300
4500
Mode number
Osc
illat
ion
freq
uenc
ies
(Hz)
σ
ω
PoleClosed Loop
LGDW dampino
net damping d l
growl
o
rate
j
M02 EPAC June 2008
Eac
• 1
• V
• 2
• H
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PEP-II RF Station, LLRF
h Station
.2 MW 476 MHz Klystron
XI-based LLRF electronics
or 4 RF cavities, with HOM loads
V power supply, Interlocks, etc.
M02 EPAC June 2008
A D IIR Filters)Dev . Multi-crate VXI/VME
Det
Sca
Sam
Dow te to synchrotron oscillationfreq .
Hold
buffer,
DAC
Power
amplifier
×
Kicker oscillator
locked to 9/4×frf
1071 MHz
QPSK modulator
Low-pass filter
Kicker structure
To RF stations
Woofer link
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LFB Systems Design
SP based flexible, programmable system (can run arbitrary FIR oreloped for PEP-II, ALS, DAΦNE (later BESSY-II, PLS and SPEAR)
ection at , correction at 9/4 RF (options 11/4, 13/4)
lable VME processing array, up to MAC/sec.
pling, A/D and D/A at 500 MHz (238 MHz PEP-II)
nsampling to reduce computational load (match processing rauency). Original “woofer” taken at DSP farm D/A wideband output
Low-pass filter
AD
C,dow
nsa
mple
r
DSP
Beam
Phase servo
×
BPM
Comb generator
LNA
locked to 6×frf
Master oscillator
2856 MHz
Farm of digitalsignal processors
Timing and control
Low group-delay channel
DSP at 9.81 MHz
6 FRF×
3.2 109⋅
M02 EPAC June 2008
Ho
Line timates, with downsampledFIR
Thre
Bea
Res n)
Req lled power)
Dyn
Bea ate currents
Insu
6000 8000 10000 12000ency (Hz)
Kicker Σ
mb
BPM
−+
Beam
np
kv
|Re(
λ l)| (m
s1 )
WEOBw was required LFB performance estimated?
ar Growth Rates, GainandTime-domain Simulation(tracking, cavity HOM esfilter)
sholds, Growth Rates - from cavity HOM measurements/estimates
m tests - 1 bunch (SPEAR), ALS 4 processor “Quick Prototype”
olution offront end modelled and lab-tested(noise kept small for high DSP gai
uiredkicker power - estimated from injection error (amp expense,minimize insta
amics estimates from simulation. Filter completely programmable
m-LLRF Simulations predict stable Low-mode behavior - LER issue at ultim
rance policy - design in a low-mode “Woofer” channel
0 2000 4000−3
−2.5
−2
−1.5
−1
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0
Frequ
Am
plitu
de (d
B)
ε
XOscillatorMaster
Σ Filter
Co
Σns
−
+
+
+φ
0
vm vb
0 20 40 60 80 100 12010
−5
10−4
10−3
10−2
10−1
100
Frequency (MHz)
positive λl
negative λl
Synhrotron Radiation damping dr
M02 EPAC June 2008
d
LFB
prog
500
Gro
mon
Woo
LLR
Soft
Soft
Buil s)
Fau
Woo
The with VxWorks. GUI, etc.
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Features Anticipated and Implemente
rammable80 processor DSP reconfigurable array
MS/sec. A/D, D/A, Downsampler - table driven2 ns bucket spacing
w-dampdynamics measurements (via dual-port memory, codes)
itoring functions (Signal MUX, RMS detectors front and back-end)
fer output
F
ware controlled broadband (direct - analog) andcomb (IIR digital) loops
ware based low frequencydigital regulators via EPICS
t-in network analyzer (via time domain excitation, response function
lt files
ferinput
days of NIM Modules with Pots - are over.Software intensivesystems,
M02 EPAC June 2008
ALSprot
devmet
VXI
PEP
HOMmea
Thre300
Beafrom
ope
Woo
coopha
400 1600 1800 2000t (mA)
00 1800 1900 2000 2100t (mA)
May 31st 2007June 1st 2007Aug 13th 2007Feb 9th 2008
700 1750 1800 1850 1900nt (mA)
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Commissioning Experience LFB
- extensive experience with the “quickotype” made commissioning fast
eloped control filters, timing/synchronizationhods
system commissioned at ALS 1994
-II (1998)
Thresholds -consistent with cavity HOMsurements - damping rates per simulation
sholds -cavity fundamental driven low modes mA (Simulation had them damped!)
m hasRF power supply noise(very different ALS)
rational issues -
fer required for low mode control
rdination with operations on synchronousse, timing LFB
800 1000 1200 10.05
0.1
0.15
0.2
0.25
0.3
0.35
0.4
Curren
Gro
wth
Rat
es (
ms
−1)
Historical DataRun 4Run 5bRun 6Run 7
1300 1400 1500 1600 17−0.5
−0.4
−0.3
−0.2
−0.1
0
Curren
Dam
ping
Rat
es (
ms
−1)
1500 1550 1600 1650 16650
6700
6750
Curre
Fre
quen
cy (
Hz)
M02 EPAC June 2008
ver
UnaRF
ManLLR
Imp
Qua
4 5 6
.01;|H|var
= 1.0384; Gain ratio = 1
8 10 12
(28.1 at 6.595 kHz)
8 10 12
degrees at 6.595 kHz)
Hz)
1
1
Cou
nts
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Unexpected Impact of “noise” in Recei
nticipated- amount of “noise” on beam fromsystems (unlike ALS and SPEAR Experience)
y sources, predominantly klystron HVPS,F processing, phase distribution noise
act ofdriven motion vs. HOM instability
ntizing noise in A/D, Rcvr noise insignificant
0 1 2 3
−10
−5
0
5
10
Ratio = 0.58111; ∆Θ = 2.288; Θvar
= 44
0 2 4 6−50
0
50Magnitude of Filter TF
0 2 4 6−200
−100
0
100
200Phase of Filter TF (−90.6
deg
Freq. (k
0 2 4 6 8 10
0−1
00
HER LFB receiver noise (rms A/D counts)
HER 1700 mA − Red
HER A/D 50 Ohm Termination − Green
HER Receiver No Beam − Cyan
Freq (kHz)
M02 EPAC June 2008
Lo ay HOM control
At 1tran
Veryinfre
magsyststat
soluwoo
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w-Frequency Noise leads to saturation and runaw
900 mA - 2100 mA in HER, unexpectedsient saturation effects, loss of control
hard to diagnose, not a steady state situation,quent transient effects
nitude of 720 Hz constantly changing with RFem configurations, operating points, activeions, maintenance etc.
tions via better 720 Hz control in LLRF andfer ( more kicker amp power would help,too)
M02 EPAC June 2008
IssuSpuIniti inInstmantrad ch faster than anticipated
00
50
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150
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250
300
350
400
450
po
we
r −
kW
500 600 700 800 900kHz)
utput Forward PEP−II LLRF tutorial
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Commissioning Experience LLRF
es with configurations of direct and comb loops -stations oscillatingrious signals in RF output, klystron oscillationsal configuration method - network analyzer no beam,gain/phase margsabilities (Station and/or Beam) at currentual tweaking of the direct and comb loopse-off ofstation stability vs. beam stability -low mode growth rates mu
2 4 6 8 10 12
IQA Module #1 Fault File − LR45 Klystron Output Forward PEP−II LLRF tutorial
time − ms0 100 200 300 400
−40
−20
0
20
40
60
80
Frequency (
Mag
nitu
de (
dB)
IQA Module #1 Fault File − LR45 Klystron O
M02 EPAC June 2008
F
Mod nges with current)
Fau of operational problems
Low . Rapid low-mode growth
Klys ot with expected result
Exte ovedDriver Amplifier-add timal station configurations
−100
−20
−10
0
10
Gai
n (d
B)
Direct
−10−200
−100
0
100
200
Pha
se (
degr
ees)
Connectorboard
EPICS IOC
Parallel portdriver
ard
Linux PC
Ethernet
Front−panel status LEDs,trigger inputs
WEOB
Major Developments/upgrades - LLR
el based configuration - reconfigure loops at current. (Dynamics cha
lt file methodology, weekly reports and analysis- understand origins
Group delay Woofer - necessary above 1500 mA (HER), 2A (LER)
tron linearizer - effort to address fast low-mode growth rates - but n
nsive re-investment in LLRF-Beamsimulation models. Led to imprresses limits of impedance control, allows comb rotation, more op
0 −500 0 500 1000
: Fr = 475.9±0.1 MHz; G = 5.268±0.009; T
d = 430.8±0.6 ns; φ = 164.1±0.1 deg
Fit
Data
00 −500 0 500 1000
Frequency (kHz)
Comb: Gc = 0.2042±0.0009; Tc = 5590±2 ns; φ
c = 30.1±0.3 deg
ADC DACFPGA
XC4085XLA
ADC DACFPGA
XC4085XLA
SRAM64Kx16
SRAM64Kx16
Offset&filterboard #1 (HER)
GVA−200 FPGA bo
Offset&filterFro
m H
ER
and
LE
R L
FB
pha
se m
onito
rs
board #2 (LER)
To LER back−end module
To HER back−end module
M02 EPAC June 2008
Un
LLR
Non
Klys
We
very
Ima
Not 0 500 1000 (kHz)
(LR42 Ibeam=1900mA)
−
−
−
−
−
Out
put P
ower
(dB
m)
476 477 478 479 480 481ncy (MHz)
de Response
20W CarrierNo Carrier
WEOB
derstanding the impact of non-linear processing
F Signals - Dynamic range 90 dB!
-linear behavior in loop -imperfections
tron - obviously non-linear
missed - medium power amplifier
significant impact- SS vs. LS gain
ge frequency generation
realized for 7 years - understood via model −1000 −500−120
−100
−80
−60
−40
−20
0
freq
FFT klystron output
471 472 473 474 475 476 477 478 479 480 48150
40
30
20
10
0
10
20
30
40
50
freq (MHz)
Output Signal (single Sideband test)
471 472 473 474 4755
6
7
8
9
10
11
12
13
14
15
freque
Gai
n (d
B)
rela
tive
(+ a
ppro
x 30
dB
)
Amplitu
M02 EPAC June 2008
LER ew LLRF amplifier
Repof “c30%imp
RunLLR
Runrota
This
• N
• N
• Cse
Man(e.gopti
3000 3500
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Final PEP-II Run April 2008
LLRF and LOM control limit at 3100 mA without comb rotation, n
lacing Driver Amp, useomb rotation” provided
improvement inedance control
5B - old amps, originalF config
6/7 - new amps, combtion
was possible, with
ew Modelling
ew control technique
areful operating pointlection
y Accelerator issues. bunch length, heating,cs, choise of gap voltage, etc.)
1500 2000 25000
0.5
1
1.5
2
2.5
3
3.5
4
Beam Current (mA)
Gro
wth
Rat
es (
ms
−1)
Run 5b configurationRun 5b configurationNew LER42 AmpRun 6, low comb gainEnd of Run 6 configurationApril 2008Run 7 configuration
M02 EPAC June 2008
LLR
• N
With han they should be
Mod l techniques (comb rotation)
This
Fau
PEPjust
who
LFBund
Una
Flexapp
New30 40 50 60
tron Output Forward 14−Jul−2007 16:39:38
e − ms
WEOB
Lessons Learned
F Modelling - key to understanding non-linear effects
on-linear klystron was less significant than drive amplifier
out models - impossible to sort out effects, see if things were worse t
els - prediction of limits, identification of nonlinear amp, new contro
tookyears, but was invaluable
lt Files- so much information
-II Experience - needed a full-time RF expert to understand complexities of faults
is the customer for this information?
- transient domain measurements keytoerstanding dynamics
nticipated - saturation limit from RF system
ibility of DSP architecture key to unexpectedlications
Accelerator Diagnostics developed0 10 20
0
100
200
300
400
500
600IQA Module #1 Fault File − LR42 Klys
tim
pow
er −
kW
M02 EPAC June 2008
s
LFBkick
• k
• C
RF -
ope
• Inst
• In
Imp
com
R&Dpus
How
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What wasn’t foreseen -more lesson
- thermal problems with beam induced power iners
W power levels -SC/DIN/EIA connectors?
able fires (several systems)
rational task - management of so many stations
dividual station dynamics- unique station toation
dividually configured stations
act ofnon-linear Klystron/Preamp
plexity of fault file analysis
project - continual changes and performanceh in the machine
is this consistent with the operating machine?
M02 EPAC June 2008
Wer s easy and we overdesigned/ove
LLR
• C ompletelyunderestimated
• U dingnonlinear amp
• O s on/off, gap voltages)
• M upported
Bro
• E dous benefit to PEP-II
• V y of output power
Wha
• F ing/measurements
• M hysics/technology skills
• D
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Summary - Lessons learned
e we successful in the feedback and LLRF areas because it warestimated things?
F and RF dynamics
omplexity of RF system,stability of low modes, operational issues - c
nexpected low-mode instabilities ->2 woofers->klystron linearizer->fin
perational intensity, issues ofconstantly moving configurations (klystron
anpower/skill of operational support woefullyunderestimated/under s
adband (coupled-bunch) longitudinal feedback
ssential techniques developed at ALS and other facilities - tremen
ery lucky (wise?) design choices for detection frequency, scalabilit
t features wereessential for success
lexibility (reprogrammability, modular architecture), close ties tomodell
ost importantelement- Creative, highly curiousgroupwith concurrent p
iverse set of interesting challenges
M02 EPAC June 2008
Tha satko, M. Minty, P. McIntosh,C. L . Young, H. Hindi, I. Linscott(Sta arcellini, M. Serio (LNF-INF d, J. Corlett, G. Lambertson,G. S contributions.
The CERN) and developed by P.Cor rz, A. Hill (SLAC) and manyothe us, K. Krauter, K. Luchini andD. T r LHC-related collaboration.
The fully designed and developedby G are was designed and codedby R d D. Teytelman (SLAC)
The developed by F. Voelker andJ. C ni, A. Gallo, F. Marcellini,et.a
Spe ise and to the ALS, SPEAR,PEP consistent good humor andhelp 3-76SF0051
WEOB
Acknowledgments
nks to D. Andersen, L. Beckman, M. Browne, P. Corredoura, J. Duimborg, S. Prabhakar, W. Ross, J. Sebek, R. Tighe, U. Wienands, Anford), M. Tobiyama, E. Kikutani (KEK), A. Drago, A. Ghigo, F. MN), Shaukat Khan (BESSY), H. Kang ( POSTECH),W. Barry, J. Byrtover and M. Zisman (LBL) for numerous discussions, advice and
PEP-II LLRF Systems were inspired by Flemming Pedersen (redoura, R. Tighe, L. Sapozhnikov,B. Ross, J. Judkins, H. Schwars. System software was designed and coded by S. Allison, R. Claeytelman (SLAC). We thank P. Baudrenghien and J. Tuckmantel fo
PEP-II LFB digital processing architecture and modules were skill. Oxoby, J. Olsen, J. Hoeflich and B. Ross (SLAC) - System softw. Claus (SLAC), I. Linscott (Stanford), K. Krauter, S. Prabhakar an
wideband longitudinal kicker for ALS and PEP-II was designed andorlett (LBL). The kicker for DAFNE (PEP-II) was designed by R. Bol.
cial thanks to Boni Cordova-Grimaldi (SLAC) for fabrication expert-II, DAFNE, KEKB, PLS and BESSY-II operations groups for their. Work supported by U.S. Department of Energy contract DE-AC0
M02 EPAC June 2008
es
Mul EP-II/PLS/SPEARrequ ith up to 500 MHz samplingrate
• D
• V
• D
• H
• T
• F - 600 MHz IF bandwidth
• B ier (1125 MHz, 1071 MHz,1
• S with EPICS-based userin
• D
• L
WEOB
Longitudinal Feedback System Featur
tiprocessor architecture fully implements ALS/BESSY-II/DA NE/Pirements. Scalable, flexible architecture for up to 8192 bunches w
s.
SP processor -VME card,4 AT&T DSP 1610s
ME interface - Bus master for data distribution
ownsampler- 500 MHz A/D and VXI Sequencer
old Buffer -500 MHz D/A and VXI Ring Buffer
iming - VXI oscillators ( , , )
ront-end - Comb filter followed by (3 GHz) phase detector
ack-end - AM modulator transfers baseband kick to QPSK’ed carr196 MHz, 1375 MHz).
oftware - VxWorks operating system for configuration and control terface
ata analysis in Matlab, Automated diagnostics and setup tools
ink error checking, temperature monitoring
Φ
RF 6 RF× 9 4⁄ RF×
6 RF×
M02 EPAC June 2008
m PLS
A 30
AllTransimpin thmodeigetran
A sinstope
A veigecon
WEOB
Grow/damp measurement example fro
ms long data set with 15 ms open-loop section.
filled bunches participate in the modal motion.sformation to the even-fill eigenmode basislifies the picture - there are three strong eigenmodesis transient. Fitting complex exponentials to theal motion we extract estimates of the modalnvalues for both open and closed-loop parts of thesient.
ingle measurement like this only characterizes theabilities and the feedback at a single acceleratorrating point.
ery powerful techniqueis to measure modalnvalues as a function of beam current, RF system
figuration, etc.
M02 EPAC June 2008
trol
DAF
•
•
Wecon
•
•
•
ALS fetime) - unanticipated effectgian lay IIR Filter
80 100 120)
DualNotch
80 100 120)
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LFB Flexibility -Quadrupole instability con
NE e+/e-collider at LNF
increased operating currents
quadrupole mode longitudinalinstabilities have appeared (theinstalled system suppresses thedipole modes).
implemented a novel quadrupoletrol filter
software programmability ofthe DSP farm
two parallel control paths fordipole and quadrupole modes.
quadrupole control has beensuccessful, allowing a 20%increase in luminosity.
added passive harmonic cavities (to address Tousheck-limited lit tune change with current. Stability required a novelnegative group de
0 20 40 60
−40
−20
0
20
40
Frequency (kHz
Gai
n (d
B)
0 20 40 60−200
−100
0
100
200
Frequency (kHz
Pha
se (
deg)
M02 EPAC June 2008
trol
Las
Plan , optics changes
Lon
Gro z, etc. are a mystery
WEOB
Where We finished - LOM and HOM con
t year of Operations
to push from 1.2E34 to 2E34 - via current increase, bunch length
gitudinal stability- Data from LER 2900 mA
wth/Damping rate isn’t the issue.Strange interfering signals at 1100 H
M02 EPAC June 2008
trol
Wha edance)?
Sev
I). N m several stages -
Fron dynamic range, steady-stateoffs
Pro noise (broadband) is onesyst ntribute. Narrowband filtershelp sensitivity to machine tunes,ope
Pow n expensive way to increasegain
Out oscillation amplitude fromwhic complicated
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Ultimate/Practical Limits to Instability Con
t Limits theMaximum Gain(e.g. fastest growth rate, or allowed imp
eral Mechanism
oise in feedback filter bandwidth, limits on noise saturation. Gain is fro
t End(BPM to baseband signal) gain limited by required oscillationets (synchronous phase transients, orbit offsets)
cessing Block - gain limited by noise in filter bandwidth. Quantizing em limit - noise from RF system or front-end circuitry may also co with broadband noise. Broad filter bandwidths help with reduced rating point - or variations of dynamics with current
er stages- gain scales with kicker impedance, sqrt(output power). A (more kickers, more output power).
put power (actually maximum kicker voltage) determines maximumh linear (non-saturated) control is possible. Saturated behavior is
M02 EPAC June 2008
Ult
II) S n vs. control frequency)
Rela
For an pickup)
limit over control band
App
Neg ut for causal systems you paythe
WEOB
imate/Practical Limits to Instability Control
tability of the feedback loop itself, (e.g. limits on phase shift and gai
ted to time delay between pickup, processing, and actuator
circular machines (systems with kick signal applied on later turn th
set by revolution time, fastest growth rates, and filter phase slope
ropriate for optimal control theory applications
LQR
Robust Control
Uncertain Systems
ative group delay over a portion of the frequency band is possible, bprice in increased phase slope away from the negative region