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Pilot-Induced-Oscillations Alleviation Through Anti-windup Based Approach

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Book cover Space Engineering

Part of the book series: Springer Optimization and Its Applications ((SOIA,volume 114))

Abstract

The chapter is dedicated to the optimization of a well-known structure of compensators: the anti-windup scheme. This approach belongs to the saturation allowance control class which aims to exploit at the most the actuators capabilities. The objective of this chapter consists of adapting and developing the anti-windup compensator design to some particular classes of nonlinear actuators presenting both magnitude and rate saturations. It is illustrated on the lateral flying case for a civil aircraft in presence of aggressive maneuvering of the pilot. A complete methodology is then proposed comparing several approaches including given anti-PIO filters.

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Acknowledgement

This work was supported by COCKPIT project, convention ONERA F/20 334/DA PPUJ.

Author information

Authors and Affiliations

  1. LAAS-CNRS, Université de Toulouse, CNRS, Toulouse, France

    Sophie Tarbouriech & Isabelle Queinnec

  2. ONERA, System Control and Flight Dynamics Department, Toulouse, France

    Jean-Marc Biannic

  3. GIPSA-Lab, Department of Automatic Control, Grenoble Campus, Saint Martin d’Hères, France

    Christophe Prieur

Authors
  1. Sophie Tarbouriech
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  2. Isabelle Queinnec
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  3. Jean-Marc Biannic
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  4. Christophe Prieur
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Corresponding author

Correspondence to Sophie Tarbouriech .

Editor information

Editors and Affiliations

  1. Exploration and Science Thales Alenia Space, Turin, Italy

    Giorgio Fasano

  2. PCS Inc., Halifax, NS, Canada

    János D. Pintér

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Tarbouriech, S., Queinnec, I., Biannic, JM., Prieur, C. (2016). Pilot-Induced-Oscillations Alleviation Through Anti-windup Based Approach. In: Fasano, G., Pintér, J.D. (eds) Space Engineering. Springer Optimization and Its Applications, vol 114. Springer, Cham. https://doi.org/10.1007/978-3-319-41508-6_15

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