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Integrated Design and Control of a Flying Wing Using Nonsmooth Optimization Techniques

  • Yann DenieulEmail author
  • Joël Bordeneuve
  • Daniel Alazard
  • Clément Toussaint
  • Gilles Taquin

Abstract

In this paper we consider the problem of simultaneously stabilizing a civil flying wing aircraft and optimizing the control surfaces physical parameters, such as control surfaces sizes and actuators bandwidth. This flying wing configuration is characterized by unstable longitudinal modes, badly damped lateral modes, and a lack of control efficiency despite large movables. The question is then to determine the energy penalty associated to the control of these unstable modes, and more precisely to optimize the control surfaces architecture in order to minimize the control-associated energy. Our approach uses latest nonsmooth optimization techniques, which allows more possibilities on requirements specifications and controller structure compared to other approaches such as LMI-based optimizations. Results show a consistent behaviour for tuned parameters of the control surfaces.

Keywords

Linear Matrix Inequality Control Surface Autonomous Underwater Vehicle Integrate Design Manoeuvre Point 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Springer International Publishing Switzerland 2015

Authors and Affiliations

  • Yann Denieul
    • 1
    Email author
  • Joël Bordeneuve
    • 1
  • Daniel Alazard
    • 1
  • Clément Toussaint
    • 2
  • Gilles Taquin
    • 3
  1. 1.University of Toulouse-ISAEToulouseFrance
  2. 2.ONERAToulouseFrance
  3. 3.Airbus Operations SASToulouseFrance

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