Adaptive fault-tolerant attitude tracking control of rigid spacecraft on Lie group with fixed-time convergence

DOI10.1002/ASJC.1888MaRDI QIDQ6563349

Zhigang Zhou, Di Zhou, Xiao-Ning Shi

Publication date: 27 June 2024

Published in: Asian Journal of Control (Search for Journal in Brave)

zbMATH Keywords

sliding mode controlattitude trackingfinite-time stabilityrigid spacecraftexponential coordinates

Mathematics Subject Classification ID

Systems theory; control (93-XX)

Cites Work

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• Actuator failure compensation and attitude control for rigid satellite by adaptive control using quaternion feedback
• Robust controllers design with finite time convergence for rigid spacecraft attitude tracking control
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• A new class of finite-time nonlinear consensus protocols for multi-agent systems
• Quaternion-Based Hybrid Control for Robust Global Attitude Tracking
• Finite-Time Attitude Tracking Control of Spacecraft With Application to Attitude Synchronization
• Nonlinear Feedback Design for Fixed-Time Stabilization of Linear Control Systems
• Rigid-Body Attitude Control

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