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

Sophie Tarbouriech (), Isabelle Queinnec (), Jean-Marc Biannic () and Christophe Prieur ()
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Sophie Tarbouriech: Université de Toulouse, CNRS
Isabelle Queinnec: Université de Toulouse, CNRS
Jean-Marc Biannic: System Control and Flight Dynamics Department
Christophe Prieur: Grenoble Campus

A chapter in Space Engineering, 2016, pp 401-423 from Springer

Abstract: 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.

Keywords: Magnitude and rate saturations; Anti-windup compensator; Convex optimization; PIO (search for similar items in EconPapers)
Date: 2016
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Persistent link: https://EconPapers.repec.org/RePEc:spr:spochp:978-3-319-41508-6_15

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DOI: 10.1007/978-3-319-41508-6_15

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