Differential Equations

, Volume 48, Issue 13, pp 1700–1720 | Cite as

Aircraft control with anti-windup compensation

  • G. A. Leonov
  • B. R. Andrievskii
  • N. V. Kuznetsov
  • A. Yu. Pogromskii
Control Theory


We consider an anti-windup compensation method ensuring the convergence of the closed-loop system for a class of reference signals. An application of the method to an aircraft flight control problem is shown.


Reference Signal Linear Matrix Inequality Harmonic Balance Method Aircraft Control Nyquist Curve 
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

© Pleiades Publishing, Ltd. 2012

Authors and Affiliations

  • G. A. Leonov
    • 1
    • 2
    • 3
    • 4
  • B. R. Andrievskii
    • 1
    • 2
    • 3
    • 4
  • N. V. Kuznetsov
    • 1
    • 2
    • 3
    • 4
  • A. Yu. Pogromskii
    • 1
    • 2
    • 3
    • 4
  1. 1.St. Petersburg State UniversitySt. PetersburgRussia
  2. 2.Institute of Problems of Mechanical EngineeringRussian Academy of SciencesSt. PetersburgRussia
  3. 3.University of JyväskyläJyväskyläFinland
  4. 4.Eindhoven University of TechnologyEindhovenThe Netherlands

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