Disturbance observer-based adaptive integral sliding mode control for rigid spacecraft attitude maneuvers

This article considers the attitude tracking problem of a rigid spacecraft involving inertia matrix uncertainty and external disturbance. The adaptive sliding mode control is utilized for the attitude controller design. The major concern is reducing the switching gain generated by current adaptive s...

Ausführliche Beschreibung

Bibliographische Detailangaben

Veröffentlicht in:	Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering Journal of aerospace engineering, 2013-10, Vol.227 (10), p.1660-1671
Hauptverfasser:	Cong, Binglong, Chen, Zhen, Liu, Xiangdong
Format:	Artikel
Sprache:	eng
Schlagworte:	Adaptive control systems Aerospace engineering Aircraft components Computer simulation Control systems Controllers Design Disturbances Gain Integrals Sliding mode control Spacecraft Switching Uncertainty
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!