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.

Gespeichert in:

Bibliographische Detailangaben
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
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Schreiben Sie den ersten Kommentar!