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Stability of Gain Scheduling Control for Aircraft with Highly Nonlinear Behavior

Author

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  • Fany Mendez-Vergara
  • Ilse Cervantes
  • Angelica Mendoza-Torres

Abstract

The main goal of this work is to study the stability properties of an aircraft with nonlinear behavior, controlled using a gain scheduled approach. An output feedback is proposed which is able to guarantee asymptotical stability of the task-coordinates origin and safety of the operation in the entire flight envelope. The results are derived using theory of hybrid and singular perturbed systems. It is demonstrated that both body velocity and orientation asymptotic tracking can be obtained in spite of nonlinearities and uncertainty. The results are illustrated using numerical simulations in F16 jet.

Suggested Citation

  • Fany Mendez-Vergara & Ilse Cervantes & Angelica Mendoza-Torres, 2014. "Stability of Gain Scheduling Control for Aircraft with Highly Nonlinear Behavior," Mathematical Problems in Engineering, Hindawi, vol. 2014, pages 1-12, May.
    • Handle: RePEc:hin:jnlmpe:906367
    DOI: 10.1155/2014/906367
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