Safety-Critical Attitude Tracking of Spacecraft With Data-Based Parameter Identification

This article proposes a safety-critical control strategy for the attitude tracking issue of a rigid spacecraft subject to orientation and angular velocity constraints. To compensate for the unknown inertial matrix parameters, an online identification algorithm with a data-based selection criteria is...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Veröffentlicht in:	IEEE transactions on aerospace and electronic systems Jg. 61; H. 2; S. 1353 - 1362
Hauptverfasser:	Xia, Kewei, Wang, Jianan, Liu, Fuxiang
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	New York IEEE 01.04.2025 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Schlagworte:	Algorithms Angular velocity Attitude control Closed loops Constraints Control barrier function (CBF) Feedback control Iron Logic programming Parameter identification Quadratic programming Quaternions Safety critical Simulation Space vehicles Spacecraft attitude control spacecraft attitude tracking Spacecraft tracking state constraints Torque Tracking control unwinding avoidance Vectors
ISSN:	0018-9251, 1557-9603
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Schreiben Sie den ersten Kommentar!