proposal for low frequency damping system in tevatron
DESCRIPTION
Proposal for Low frequency damping system in Tevatron. Why do we need it? Maybe not? Can our current correctors handle the job? How should the system look? Problems or issues?. Horizontal Beam motion. Beam Signal while cycling T:HA49 correctors at 15 Hz. - PowerPoint PPT PresentationTRANSCRIPT
Proposal for Low frequency damping system in Tevatron
• Why do we need it? Maybe not?
• Can our current correctors handle the job?
• How should the system look?
• Problems or issues?
Horizontal Beam motion
0 200 400 600 800 1000 1200 1400 1600 1800 2000 2200400
200
0
200
400T:ORBACH position in microns
Time (4.898 msec)
posit
ion (m
icron
s)
233.417
220.503
Xi
2.027 1030 i
0 5 10 15 20 25 30 35 40 45 500
20
40FFT of T:ORBACH position data
Frequency (Hz)
mic
ro m
eter
s 2 XFi
N
i204
N
.
Beam Signal while cycling T:HA49 correctors at 15 Hz
0 200 400 600 800 1000 1200 1400 1600 1800 2000 2200500
0
500T:ORBACH position
Time (4.898 secs)
micro
mete
rs Xi
i
0 200 400 600 800 1000 1200 1400 1600 1800 2000 22002
1
0
1
2
Time (4.898 sec)
Curre
nt in
Corre
ctor (
Amps)
Ii
i
0 5 10 15 20 25 30 35 40 45 500
100
200FFT of T:ORBACH position data
Frequency (Hz)
micr
o m
eters 2 XFi
N
i204
N
.
0 5 10 15 20 25 30 35 40 45 500
0.5
1
1.5FFT of reference Current for Corrector
Frequency (Hz)
micr
o m
eters 2
IFi
N
i 207
N
Since at 15 Hz we can generate a 174 micron kick we shouldBe able to generate at least a 131 micron amplitude kick at 20 Hz which is much stronger than the strongest signal of 32 micronsobserved at 12 Hz. So the correctors are able to damp all oscillationsbelow 20 Hz if driven correctly.
How should the system look?
BPM 1
BPM 2
ProcessingCorrector 1
Corrector 2
CDF
D0D1
B1
Algorithm for orbit correction
0 5000 1 104
1.5 104
2 104
2.5 104
3 104
3.5 104
4 104
4.5 104
5 104
5.5 104
6 104
6.5 104
7 104
7.5 104
8 104
8.5 104
9 104
9.5 104
1 105
1 104
0
1 104
Z n 0
n
.
0 5 10 15 20 25 30 35 40 45 500
2 105
4 105
cxn2
N
n
N 21 106
Simulated beam response to applied kick 0.5 micro-rad kick of 20 Hz at D0 low beta quad as measured at A0 yield 30 micro-meter oscillations. Turn-by-turn (top) and frequency (bottom)
0 5000 1 104
1.5 104
2 104
2.5 104
3 104
3.5 104
4 104
4.5 104
5 104
5.5 104
6 104
6.5 104
7 104
7.5 104
8 104
8.5 104
9 104
9.5 104
1 105
0Z n 0
n
.
0 5 10 15 20 25 30 35 40 45 500
4 105
cxn2
N
n
N 21 106
Simulated beam response with damping feedback turned on. Now beam motion down to < 2E-20 meters at A0. Turn-by-turn (top) and frequency (bottom). The correctors are running < 0.8 micro-rad which would require cycling correctors at .324 Amps much less than the 1.2 Amps we were able to produce at 15Hz. If quad motion was located at B0 the optics are very similar and simulations produce similar results.
A detail schematic of a single orbit correction node
BPM 1HB11
BPM 2HB13
Corrector 1 HB19
Corrector 2 HB13
Sample And HoldCard
Sample And HoldCard
Op-amp x A
Op-amp x B
Op-amp x C
SUM
Beam sync trigger
1-200 Hz filter
1-200 Hz filter
Op-amp x D
SUM
A more detailed schematic of the damping system. Here Gains A,B and C are determined by the optics, voltage to position ratio of BPMs and voltage to Amp ratio for the correctors reference voltage. We have BPM transfer function of 12V/m, corrector transfer ratio of 2.54-rad/Amp and controlled by reference voltage transfer function 5 Amps/volt. This gives a total BPM voltage to reference voltage multiplicative factor as (1/12)x(1/2.54E-6)x(1/5) = 6561.67. The optics factor are Fa=1.88E-5, Fb= -0.021, Fc= -0.039, and Fd=-
2.371E-4. So a first estimate has A = 0.1233, B = -137.7, C = -255.9 and D = -1.555.
Issues to worry about? Phase shift?
Is this a real phase shift??? The snap shot time stamp says yes. But calculations from skin effect of stainless steel beam pipe say no.
0.61637 38.817
0.738 40.738
1.2 54.842
Current (Amps) Phase Diff. (degrees)
assuming the harmonic time dependence exp[iwt] and the spatial dependence of exp[ikx] for a simple slab geometry. Where our wave number k can be approximated with
k 1 1i( )
f f
With resistivity 75 106 cm
K become (1+i)*0.023√f . With a beam pipe thickness ~ .32 cm the phaseshift becomes
0.00736 f f
Or 1.63 degrees at 15 Hz.
Even if this does turn out to be a problem we can look to solutions used atThe APS where a simple phase and amplitude compensation circuit are used toCompensate phase shifts due to electronic and skin effects of aluminum beam Pipe yielding phase shifts in excess of 90 degrees.