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Optically Based Diagnostics for Optical Stochastic Cooling⇤ M

Optically Based Diagnostics for Optical Stochastic Cooling⇤ M

ISBN 978-3-95450-180-9 Proceedings of NAPAC2016, Chicago, IL, USA WEPOA38

OPTICALLY BASED DIAGNOSTICS FOR OPTICAL STOCHASTIC COOLING⇤ M. B. Andorf1, V. A. Lebedev2, P. Piot1,2, J. Ruan2 1 Department of Physics and Northern Illinois Center for Accelerator & Detector Development, Northern Illinois University DeKalb, IL, USA 2 Fermi National Accelerator Laboratory, Batavia, IL, USA

Abstract the two transverse phase spaces provides a path for cooling An Optical Stochastic Cooling (OSC) experiment with along all three degrees of freedom. electrons is planned in the Integrable Optics Test Accelera- Table 1: Parameters for the OSC in IOTA tor (IOTA) ring currently in construction at . OSC requires timing the arrival of an electron and its radiation parameter value unit generated from the upstream pickup undulator into the down- stream kicker undulator to a precision on the order of less Uo 100 MeV than a fs. The interference of the pickup and kicker radiation K 1.04 - suggests a way to diagnose the arrival time to the required period 11.06 cm precision. (at zero angle) 2.2 µm Total length 77.4 cm INTRODUCTION In IOTA, the OSC proof-of-principle experiment will be Fermilab is currently preparing a proof-of-principle of accomplished in two phases. In a first stage, we will not Optical Stochastic Cooling (OSC) using 100 MeV electrons have an amplifier and rely on passive cooling: the optical at the Integrable Optics Test Accelerator (IOTA). In OSC system will consists of a telescope composed of three lenses a particle emits radiation in a pickup undulator. The light chosen so that the optical transfer matrix between the pickup from the pickup is then transported, and in the presence of and kicker is I where I is identity matrix. The an optical amplifier, amplified, to a kicker undulator located telescope can transport 90% of the energy from the pickup downstream and identical to the pickup undulator. There- ⇠ to the kicker. Parameters for the undulators can be found fore the particle follows a curved path in a magnetic bypass in Table 1 and yield a value for the kick amplitude, ⇠ = chicane such that it arrives at the entrance of the kicker 0 8.5 10 10. Simulations show that the kick is further reduced just as the light from the pickup is also arriving [1,2]. For ⇥ by roughly 10 % due to dispersion in telescope [3]. In the the reference particle the arrival time of radiation and par- second stage, a 7-dB Cr:ZnSe optical amplifier (with an ticle in the kicker is such that it receives no kick. Parti- operating band from 2.2 2.9 µm) will be installed and is cles with a nonzero or betatron coordinate are expected to double the cooling rates over the passive cooling displaced relative to the reference particle by an amount scheme. s = M51 x + M52✓ + M56(p/p) and receive a longitudinal kick given as In this paper we explore how to measure the timing error p between the arrival of the pickup signal and the particle in = ⇠ sin(ks). (1) the kicker. The timing precision needs to be < 1 fs in order p 0 to fully optimize the cooling rates. We propose a technique In the above Mij are the elements of the 6 6 transfer matrix that uses optical interference between the pickup and kicker ⇥ from pickup to kicker, k 2⇡/ is the radiation wave- radiation signals. Before detailing the measurement tech- ⌘ number, and (p)/p is the relative momentum change of the nique we first consider in the impact of arbitrary timing error particle after a single pass through the cooling section. The on the OSC process. kick normalized amplitude is ⇠0 = 2E0pG/(pc) where E0 corresponds to, in the case of a suciently small undulator LONGITUDINAL TIMING parameter, the energy radiated in a single undulator, G is the gain in power from the optical amplifier (if present), p Cooling Rates and Transit Time Error the design momentum and c the velocity of light. When the The damping decrements i (i [x, s]) for small betatron 2 dispersion function is non vanishing at the kicker undulator and synchrotron amplitudes are given by [4] location a horizontal kick is also applied thereby resulting in horizontal cooling. Likewise, introducing coupling between x k⇠o M SP = 56 , (2) "s # 2 " SP # ⇤ Work supported by the by the US Department of Energy (DOE) contract

DE-SC0013761 to Northern Illinois University. Fermilab is operated 2016 CC-BY-3.0 and by the respective authors where Sp = M Dp + M D0 + M is the partial slip factor by the Fermi research alliance LLC under US DOE contract DE-AC02- 51 52 P 56 © 07CH11359. such that a particle with a momentum deviation p/p will be

3: Advanced Acceleration Techniques and Alternative Particle Sources 779 Copyright WEPOA38 Proceedings of NAPAC2016, Chicago, IL, USA ISBN 978-3-95450-180-9

damping and excitation

dp"˜ p"˜ = x (ax, ap ) dt ⌧s x,damp + (p"˜ p"o) ⌧s dp/p p/p = p (ax, ap ) dt ⌧s p,damp + (p/p p ), (5) ⌧s

Figure 1: Trajectories in ax,ap space. Top figures are for where ⌧s is the revolution period of the accelerator, x,damp, ksd = 0. The left shows trajectories from OSC without p,damp are the synchrotron cooling decrements in ampli- diusion from synchrotron damping, while the right figure tude per turn, "0 is the equilibrium beam emittance and p includes both. The bottom figure is set for ksd = ⇡ with is equilibrium momentum spread, both without OSC. again the left figure showing trajectories from OSC and the The above equations exclude fluctuations. Thus, they right including diusion from . describe an evolution of average amplitudes for an ensemble of particles having the same initial amplitudes. They do not imply, in the absence of OSC, that all particles are driven longitudinally displaced by the amount Spp/p while travel- to have the values "˜ = "0 and p/p = p, which is only ing from the pickup to kicker undulators (without accounting statistically true for the whole beam. In reality particles make the additional displacement due to betatron motion). The random walks about these values, reflecting the random 0 dDP quantities DP is the dispersion in the pickup and DP = ds . process of photon emission. Table 2 summarizes the OSC As can be seen from Eq. (1) the corrective kick becomes chicane and beam parameters used in this contribution. nonlinear for large particle amplitudes and so the damping decrements depend on amplitude. This is accounted for in [4] Table 2: OSC and Beam Parameters by averaging kicks over betatron and synchrotron oscillations. Here we follow what was done in the latter reference but parameter value unit delay 2 mm include an additional phase term in Eq. (1), ksd, where sd/c is the dierence between between the arrival times measured Sp 1.38 mm at the kicker between the reference particle and its radiation Sx 2.24 µm 4 p 1.1 10 - emitted (at a retarded time) from the pickup. Including this ⇥ additional term yields the damping decrements "o 9.1 nm 7 p,damp 1.2 10 - ⇥ 8 x (ax, ap ) Lp sd x,damp 7.2 10 - = | | cos(ksd ) ⇥ "p (ax, ap )# Lp 2J (a )J (a )/a Momentarily neglecting the synchrotron radiation terms x o p 1 x x , (3) ⇥ "p2Jo (ax )J1(ap )/ap # we look for the fixed points of Eq. (5). It is easily seen that such points occur only when both J0(ax ) and J0(ap ) are where the left most factor has been introduced to account for zero, or when J1(ax ) and J1(ap ) are zero. Computation the decrease in the kick amplitude due to the finite length of of the eigenvalues of the Jacobian reveals that the J0 fixed the undulator pulse, Lp Nund, and Nund is the number points correspond to saddle points while the J fixed points ⇡ 1 of undulator periods. The parameters ax and ap are the am- are either stable or unstable nodes. plitudes of longitudinal displacement from pickup to kicker, There are three particularly important fixed points expressed in units of the wave phase, respectively due to [0,µ, ], [µ , ,µ, ],and [µ , , 0] where µ , 2.405 is the 1 1 0 1 0 1 1 1 0 1 ⇡ betatron and synchrotron oscillations first zero of Jo and µ , 3.832 is the second zero for J . 1 1 ⇡ 1 These three points roughly map out the cooling boundary ax = k "˜Sx, and enclose most particles. When cos(ksd ) > 0 all three ap = kpSp (p/p), (4) points are unstable and all particles within this region are attracted to the stable node [0, 0],aJ1 = 0 fixed point. where "˜ is the particles Courant-Snyder invariant, Sx = When cos(ksd ) < 0 the stability of the nodes are switched 2 2 2 ( p M 2↵p M M + (1 + ↵ )M )), and ↵p and p are while the saddle points remain unstable. Thus all particles 51 51 52 p 52 the Courant-Snyder parameters in the pickup. within the cooling range are attracted to either [0,µ1,1] or We can now write a system of coupled rate equations for [µ1,1, 0] depending on their initial coordinate. Therefore 2016 CC-BY-3.0 and"˜ by the respectiveand authors p/p, where in addition to the eects of OSC we longitudinal timing errors correspond to only three modes © include a term to approximately describe both synchrotron of behavior, the two just described which are determined

Copyright 780 3: Advanced Acceleration Techniques and Alternative Particle Sources ISBN 978-3-95450-180-9 Proceedings of NAPAC2016, Chicago, IL, USA WEPOA38 only by the sign of cos(ksd ). And a 3rd intermediate case with cos(ksd ) = 0 where damping rates become zero. The two left plots of Fig. 1 show the trajectories of the [ax, ap] phase space when diusion due to synchrotron ra- diation is neglected. The plots on the right in Fig. 1 include diusion due to synchrotron radiation. They indicate the cooling boundary is expanded when cos(ksd ) > 0 and when cos(ksd ) < 0 particles are expelled out, as before, but to fixed points with smaller amplitudes with the exact location depending on the magnitude of cos(ksd ).

Method to Determine ksd Figure 2: Downstream light energy from the pickup and Here we demonstrate a simple method for measuring ksd, 4 and so the timing error, by observing the light intensity of kicker undulators with N=10 electrons as function in the the pickup and kicker downstream of the cooling insertion chicane delay achieved with changes of current in the chicane at the first harmonic. Note that the bunch length is much dipoles. longer than the wavelength and so the kicker and pickup pulses of dierent particles add incoherently. If we consider a bunch with N electrons the total loss of energy for the nth the interference we neglected their eect and considered that electron in the bunch is given as the sample lengthening results in a Gaussian distribution in the kicker undulator.

U(p/p, "˜)n = Uo⇠0 1 +  CONCLUSIONS Lp sd sin(ksn + ksd ) | | , (6) OSC requires timing of the arrival of the pickup signal Lp and its particle in the kicker to a precision of less than 1 fs. Any attempt to directly measure this arrival time is not prac- with sn Sp (p/p)n + pSx "n. Furthermore if the beam ⌘ tical since, in addition to the extreme precision needed, the has am rms relative momentum spread p and transverse signals from single electrons arrive in the form of a bunch emittance "0 (assumed to be independently Gaussian dis- with a length on the order of hundreds of picoseconds. The 2 tributed) then the rms longitudinal displacement is s = method that has been proposed here does not require a direct 2 (Spp ) + "0Sx. Integrating over all particles yields the measurement of the arrival time but rather takes advantage total loss in energy of the beam to be of the fact that in the cooling insertion particles receive kicks not just on their longitudinal displacement relative to a ref- Lp sd Ubeam = NUo⇠o 1 + | | sin(ksd ) erence particle, but also their phase relative to the pickup L  p signal. Thus timing information is derived from the light 2 2 exp( k s /2) (7) intensity variation with delay of electron bunch in the OSC ⇥ chicane. The variation originates from the interference of ra- diations coming from the pickup and kicker undulators. The The energy of the downstream radiation is Ubeam. Fig- ure 2 shows the radiation energy as a function of timing intereference between radiation produced by two undulators error recorded downstream of the kicker undulator. A InAs has been observed before in an optical setup [6] and photovoltaic detector can be used for the measurement. A used as a beam diagnostics [7]. single-staged thermally electric cooled detector has a NEP rating of 6 pw/Hz1/2. For an electron bunch with 104 parti- REFERENCES cles and rms bunch length of z = 20 cm this gives a signal [1] A. A. Mikhailichkenko and M.S. Zolotorev, Phys. Rev. Lett. to noise ratio of 4 when pickup and kicker signals interfere 71 (25), p. 4146, 1993. deconstructively at maximum amplitude. To observe a pat- [2] M. S. Zolotorev and A. A. Zholents, Phys. Rev. E 50 (4), tern like that shown in Fig. 2 the cooling and signal detection p. 3087, 1994. must be on for only a short time, on the order of ms, before [3] M. B. Andorf et al., in Proc. IPAC’16, Busan, Korea, p.3028, the beam becomes modified. This can be accomplished with 2016. two mechanical shutters. [4] V. A. Lebedev, "Optical Stochastic Cooling," ICFA Beam Dyn. In the above discussion we neglected non-linear contri- Newslett. 65 100, 2014. butions to longitudinal motion which mainly come from betatron motion. These nonlinearities are compensated by [5] V. Lebedev et al., presented at COOL’15, in press, 2015. sextupoles for the center of the distribution. However the [6] P. Elleaume, J. Phys. Coll. 44 (C1), 333, 1983. compensation is not perfect for the tails [5]. Taking into [7] R. Bakker et al., in Proc. EPAC1996, Barcelona, Spain, p. 667, 2016 CC-BY-3.0 and by the respective authors account that tails do not produce significant contributions to 1996. ©

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