The windup phenomenon is interpreted as a consequence of the convergent property absence for system with a saturation. This makes it possible to use the frequency-domain criterion for analysis of anti-windup augmentation in the case of stable and marginally stable plants. Based on this approach, robustness of the systems with respect to time delay in the anti-windup loop is examined and the approach for an optimal choice of the static anti-windup gain is proposed. An application of the convergence-based anti-windup control strategy to aircraft flight control for the case of time-delay in the anti-windup loop is described and studied by simulations.

Original languageEnglish
Pages (from-to)144-149
Number of pages6
JournalIFAC-PapersOnLine
Volume28
Issue number9
DOIs
StatePublished - 1 Jul 2015
Event1st IFAC Workshop on Advanced Control and Navigation for Autonomous Aerospace Vehicles, ACNAAV 2015 - Seville, Spain
Duration: 10 Jun 201512 Jun 2015

    Research areas

  • Anti-windup correction, Convergent systems, Flight control, Integrator windup

    Scopus subject areas

  • Control and Systems Engineering

ID: 41251412