<xml>
  <records>
    <record>
       <contributors>
          <authors>
             <author>Brajnik, G.</author>
             <author>Bassanese, S.</author>
             <author>Cautero, G.</author>
             <author>Cleva, S.</author>
             <author>De Monte, R.</author>
          </authors>
       </contributors>
       <titles>
          <title>
             Integration of a Pilot-Tone Based BPM System Within the Global Orbit Feedback Environment of Elettra
          </title>
       </titles>
		 <publisher>JACoW Publishing</publisher>
       <pub-location>Geneva, Switzerland</pub-location>
		 <isbn>978-3-95450-201-1</isbn>
		 <electronic-resource-num>10.18429/JACoW-IBIC2018-TUOC01</electronic-resource-num>
		 <language>English</language>
		 <pages>190-195</pages>
       <pages>TUOC01</pages>
       <keywords>
          <keyword>FPGA</keyword>
          <keyword>controls</keyword>
          <keyword>electron</keyword>
          <keyword>feedback</keyword>
          <keyword>Ethernet</keyword>
       </keywords>
       <work-type>Contribution to a conference proceedings</work-type>
       <dates>
          <year>2019</year>
          <pub-dates>
             <date>2019-01</date>
          </pub-dates>
       </dates>
       <urls>
          <related-urls>
              <url>https://doi.org/10.18429/JACoW-IBIC2018-TUOC01</url>
              <url>http://jacow.org/ibic2018/papers/tuoc01.pdf</url>
          </related-urls>
       </urls>
       <abstract>
          In this contribution, we describe the advantages of the pilot tone compensation technique that we implemented in a new BPM prototype for Elettra 2.0. Injecting a fixed reference tone upstream of cables allows for a continuous calibration of the system, compensating the different behaviour of every channel due to thermal drifts, variations of cable properties, mismatches and tolerances of components. The system ran successfully as a drop-in substitute for a Libera Electron not only during various machine shifts, but also during a user dedicated beamtime shift for more than 10 hours, behaving in a transparent way for all the control systems and users. The equivalent RMS noise (at 10 kHz data rate) for the pilot tone position was less than 200 nm on a 19 mm vacuum chamber radius, with a long-term stability better than 1 um in a 12-hour window. Two main steps led to this important result: firstly, the development of a novel RF front end that adds the pilot tone to the signals originated by the beam, secondly, the realisation of an FPGA-based double digital receiver that demodulates both beam and pilot amplitudes, calculating the compensated X and Y positions.
       </abstract>
    </record>
  </records>
</xml>
