Aircraft control with anti-windup compensation

Aircraft control with anti-windup compensation

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.

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Veröffentlicht in:Differential equations 2012-12, Vol.48 (13), p.1700-1720
Hauptverfasser: Leonov, G. A., Andrievskii, B. R., Kuznetsov, N. V., Pogromskii, A. Yu
Format: Artikel
Sprache:eng
Schlagworte:
Aircraft
Algebra
Closed loop systems
Compensation
Control algorithms
Control Theory
Controllers
Difference and Functional Equations
Differential equations
Mathematics
Mathematics and Statistics
Methods
Ordinary Differential Equations
Partial Differential Equations
Studies
Theorems
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Beschreibung
Zusammenfassung: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.
ISSN:0012-2661
1608-3083
DOI:10.1134/S0012266112130022