Design Considerations for a Prototype Beam Position Monitor for the X-Ray Microscopy Beamline ID21 at the ESRF G. S. Dermody1, C. J. Buckley1, J. Susini2, R. Barrett2 1 Department of Physics, King's College London, WCR 2LS, United Kingdom 2 European Synchrotron Radiation Facility, Grenoble Cedex, France Abstract. The beam position monitor will be located after the focusing optics at the monochromator exit slit, 50 m from the undulator source and is intended to operate over the energy range 0.2–6.0 keV. Ray-tracing is used to evaluate the size, location and photon density of the monochromatic beam at the exit slits. This has been performed for the beamline in the two basic operation modes and at several undulator K values. The results of this work provides the information necessary to design detectors suitable for measuring the beam position and intensity. The results are provided in this paper together with an outline of prototype detection schemes. 1 Introduction The distance from the undulator to the monochromator to exit slit on the X-ray microscopy beamline at the ESRF is approximately 50 m. The undulator is constructed in three sections to provide both soft X-rays for imaging in the water window and harder X-rays up to 6 keV. This energy range is too large to be covered by a single monochromator, therefore the beamline has been designed to operate with either a double crystal monochromator (DCM) or a plane grating monochromator (PGM) without movement of the exit slit [1]. A beam position monitor (BPM) will be installed at the exit slit to ease the initial alignment of the optics and the interchange between imaging modes and to provide information on the temporal and spatial stability of the probe during image acquisition. Unlike second generation sources, the spatial and temporal stability of the probe cannot readily be achieved by overfilling the apertures, slits and zone-plates of the beamline [2]. Overfilling would result in the loss of photons exhibiting useful coherence properties because the undulator beams are highly collimated and have a much larger fraction of coherent flux within the central cone. The BPM will ensure the stability of the probe by providing real time correction with a feedback loop linked to a piezo-electric stage on the last mirror mount if needed. Various designs for beam position monitors, including the use of impinging and transmitting blades, have been described previously [3−8]. Here the detection scheme is limited by the non-uniformity of the beam at the exit slit and the microscope itself. The beamline layout is described briefly in section 2. The calculation of the flux available to the monitor is described in section 3 and in section 4 a number of detection schemes are outlined. I - 182 G. S. Dermody et al. 2 The Beamline Layout The beamline has been designed to enable the formation of a microprobe over the energy range 0.2−6 keV. The optical layout is shown in figure 1. In both imaging modes two horizontally deflecting plane mirrors stop bremsstrahlung radiation and act as a low pass filter. The X-ray beam is then collimated by three 5×5 mm apertures, the first two within the machine hutch and the third 27 m from the undulator to remove scattered and diverging photons. M od e 1 E x it S lit P lan vie w DCM M od e 2 E x it S lit P la n e m ir ro r PGM C ollim a to r A p e r tu re H o r iz o n ta l F o c u sin g M irro r V e r tic a l F o c u sin g M irr o r Fig. 1. Schematic diagram of the beamline optical layout. The beam is focused onto the monochromator exit slit by a two component Kirkpatric-Baez mirror system. In the harder X-ray region (1.6−6keV) both mirrors precede the monochromator, whereas in the softer X-ray region (0.2−1.6keV) the monochromator precedes the second focusing mirror. 3 The Beamline Simulation The beamline was modeled to calculate the flux available to a BPM immediately before the monochromator exit slit. The efficiency, geometrical transmission, bandpass and focusing properties of each optic were used to calculate the energy density distribution at the monochromator exit slit. The intensity reflectivities Rp and Rs of a plane wave reflected from a smooth surface were calculated from the Fresnel equations. The reflectivity from a coating with a residual r.m.s. surface roughness σrms is then given by [ Rσ = Rp exp −(4 πσ rms sin θ / λ ) 2 ] (3.1) with an analogous expression for s-polarised radiation. The beamline was simulated using the geometrical ray tracing software SHADOW [4]. Both beamline modes were traced at a number of wavelengths to obtain photon density distributions at the exit slit, figure 2a. By assuming 100% efficiency of all the optical surfaces the geometrical transmission factor, GTFλ , as a function of wavelength was calculated. The simulation was also used to give the Design Considerations for a Prototype Beam Position Monitor I - 183 transmission and DCM bandpass from the traced rocking curves. The transmission is given by the height of the curve after the second crystal and the bandpass BPDCM is calculated from the differential form of the Bragg equation ∆λ ∆E = = ∆θ cot θ B λ E where θB is the Bragg angle and ∆θ is the width of the rocking curve. The total flux at the exit slit for both imaging modes is then given by (3.2) Fmod e1 = U B × U N × GTFλ × Tλ × TSi(111) × BPDCM (3.3) Fmode2 = U B × U N × GTFλ × Tλ × ξ PGM (3.4) and 2 2 where UB [photons/sec/mrad /mm into 0.1% bandpass] is the undulator brilliance, UN normalises the fractional bandpass, Tλ is the combined transmission of the mirrors, TSi(111) is the transmission of the DCM and ξPGM is the efficiency into the PGM first order. From the flux curves, figure 2b and figure 2c), the photon density distribution and the energy density for any wavelength can be calculated, figure 2c. 4 Detection Schemes The monitor is required to measure accurately the position of the beam centroid with high short and long term repeatability and to act as an incident flux monitor. In the DCM mode the beam is small, has a clear centroid in both the horizontal 40 20 0 -20 -100 Flux [photons/sec into BPDCM banpass] Flux [photons/sec into 100% bandpass] 60 a) c) 7E+15 80 -50 0 50 100 Horizontal Position [µm] 1E+12 5E+15 4E+15 3E+15 2E+15 1E+15 0E+00 0 500 1000 1500 2000 Energy [eV] 60 1E+11 1E+10 1E+09 1E+08 1E+07 1E+06 2500 750 l/mm 1200 l/mm 1800 l/mm 6E+15 b) Vertical Position [µm] Vertical Position [µm] 100 50 40 30 20 10 34 47 0 20 17 7 40 27 -10 3500 4500 Energy [eV] 5500 6500 -40 d) -20 0 20 Horizontal Position [µm] 40 Fig. 2. a) The photon distribution at the exit slit with the DCM set at λ=0.3nm, b) the flux reaching the exit slit for PGM modes c) the flux at the exit slit for the DCM mode and d) the energy density [mW/mm2] with the DCM set at λ=0.3nm at the exit slit. I - 184 G. S. Dermody et al. and vertical directions and a highly non-uniform beam profile. The main problem in this imaging mode, therefore, is to use this profile to obtain the position of the beam centroid without degrading the imaging probe. The beam centroid can be located with a pinhole mounted on an X-y stage. By minimising the photoelectric signal from the foil around the pinhole the beam centroid can be located, figure 3a. A quadrant photon detector upstream of the pinhole will detect any changes in beam position. In the PGM mode the beam is focused into a vertical strip with continuously varying wavelength. If only a single wavelength is considered the profile is similar to that of the DCM mode. The location of the beam in this mode poses a more interesting problem. In the horizontal, the position can be obtained by a single pair of blades in the normal way. In the vertical direction, however, no simple solution to give the beam position exists because the beam lacks a vertical centroid. We are aiming to build a detector that will provide vertical position and intensity normalisation of the X-ray probe at specific wavelengths. Three detection schemes have been considered. The first consists of a slit mounted upon a linear feedthrough in front of two off axis coated blades, figure 3b. The difference between the photoelectron signal from the two blades would provide the horizontal position. By choosing a blade coating material with an absorption edge within the working energy range the vertical position could be found. As the slit is tracked across the blade a drop in intensity would be observed at the absorption edge hence providing the position and intensity of a specific wavelength from the grating. A number of interchangeable blades with a number of different coatings would provide vertical position and intensity normalisation at a number of wavelengths. The second solution is also based upon the utilisation of a spectral absorption feature. In this solution two slits are mounted upon a linear feedthrough in front two off axis coated detectors, figure 3c. The detector coating is chosen such that a NEXAFS resonance peak is within the working energy range. The vertical position would be obtained by tracking the slits and detectors across the off axis portion of the beam. As the slits move the resonance peak signal would be observed in the signal from first one then the other detector. By positioning the slits so that the energy exciting the resonance is obscured by the central stop any beam motion would result in a fluctuation of signal in one detector, indicating the direction of motion. When balanced the total signal can be used to normalise the probe at a specific wavelength. a) b) Signal Detector Slit Side elevation End elevation Signal Exit Aperture Coated Blades c) Slits Coated Detectors Exit Aperture Fig. 3. A schematic diagram of a) BPM using a range of pinholes, b) a BPM using an absorption edge for vertical position and c) a BPM using a ZANES peak for vertical position. Design Considerations for a Prototype Beam Position Monitor I - 185 Both solutions are only possible because a third generation undulator source is used to produce soft X-rays. In the energy range of interest, 0.2−1.6keV, the undulator will operate in near wiggler mode producing a broad spectrum. This will increase the number of possible coating materials with useful absorption features and allow the assumption that intensity across the absorption features is constant. The third solution, for the PGM mode, would combine one of the above PGM solutions with the use of a higher diffracted order. 5 Conclusion The beam parameters have been calculated at a number of undulator K values spanning the energy range of interest. This has enabled a number of prototype detection schemes to be evaluated. The prototypes will be constructed at King’s College London in the latter part of 1996 and tested in house in early 1997. Initially the beamline will operate in the hard X-ray region with the DCM. The first monitor scheme to be installed will be the pinhole BPM which will also act as the entrance aperture to the microscope. At a later date the addition of up to three PGMs will enable the microscope to cover the water window. By this time the inhouse testing will have been completed and the BPM will be ready for ESRF beamline testing. Acknowledgments G.D would like to thank the EPSRC for supporting this work and Oxford instruments for sponsorship. References 1 J. Susini and R. Barret The X-ray microscopy project at the ESRF, these proceedings. 2 J. Kirtz, H. Ade, C. Jacobsen, C.H. Ko, S. Lindaas, I. McNulty, D. Sayre, S. Williams, X. Zhang and M. Howells, Soft X-ray microscopy with coherent X-rays, Rev. Sci. Inst. 63 (1) 557 1992. 3 B.A. Karlin, P.L. Cowan and C. 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