Synthesis of Pitch Angle Control System with Angle of Attack Limiting Channel

The problem of synthesizing the pitch angle control system with the angle of attack limiting channel is considered. The problem of matching the trajectories of the system of the pitch angle control mode and the angle of attack limitation mode is discussed. An approach is proposed based on using a ge...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Russian aeronautics 2020, Vol.63 (1), p.25-32
Hauptverfasser: Abdullina, E. Yu, Efanov, V. N.
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:The problem of synthesizing the pitch angle control system with the angle of attack limiting channel is considered. The problem of matching the trajectories of the system of the pitch angle control mode and the angle of attack limitation mode is discussed. An approach is proposed based on using a generalized characteristic of the system, which ensures the matching the states at an arbitrary moment of change of its operation mode.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799820010043