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...

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Vydané v:	IEEE transactions on aerospace and electronic systems Ročník 61; číslo 2; s. 1353 - 1362
Hlavní autori:	Xia, Kewei, Wang, Jianan, Liu, Fuxiang
Médium:	Journal Article
Jazyk:	English
Vydavateľské údaje:	New York IEEE 01.04.2025 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Predmet:	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
On-line prístup:	Získať plný text
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