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DOI:10.18429/JACoW-ICALEPCS2015-MOPGF177
Title Robust Stability Analysis of Orbit Feedback Controllers
Authors
  • S. Gayadeen, M.T. Heronpresenter, G. Rehm
    DLS, Oxfordshire, United Kingdom
Abstract Closed loop stability of electron orbit feedback controllers is affected by mismatches between the accelerator model and the real machine. In this paper, the small gain theorem is used to express analytical criteria for closed loop stability in the presence of spatial uncertainty. It is also demonstrated how the structure of the uncertainty models affects the conservativeness of the robust stability results. The robust stability criteria are applied to the Diamond Light Source electron orbit controller and bounds on the allowable size of spatial uncertainties which guarantee closed loop stability is determined.
Paper download MOPGF177.PDF [1.148 MB / 4 pages]
Poster download MOPGF177_POSTER.PDF [1.055 MB]
Conference ICALEPCS2015, Melbourne, Australia
Series International Conference on Accelerator and Large Experimental Physics Control Systems (15th)
Proceedings Link to full ICALEPCS2015 Proccedings
Session Poster session
Date 19-Oct-15   17:30–18:30
Main Classification Feedback Systems, Tuning
Keywords controls, feedback, electron
Publisher JACoW, Geneva, Switzerland
Editors Lou Corvetti (AS, Clayton, Australia); Kathleen Riches (SLSA, Clayton, Australia); Volker RW Schaa (GSI, Darmstadt, Germany)
ISBN 978-3-95450-148-9
Published December 2015
Copyright
Copyright © 2015 by JACoW, Geneva, Switzerland     CC-BY Creative Commons License
cc Creative Commons Attribution 3.0