Fault-tolerant control for full-state error constrained attitude tracking of uncertain spacecraft

DOI10.1016/j.automatica.2023.110907zbMath1520.93115OpenAlexW4321769938MaRDI QIDQ6109052

Qinglei Hu, Yang Shi, Youmin Zhang, Xiaodong Shao

Publication date: 30 June 2023

Published in: Automatica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.automatica.2023.110907

zbMATH Keywords

state constraintsspacecraftadaptive robust controlattitude controlfault-tolerant control

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Controllability (93B05) Control/observation systems with incomplete information (93C41) Adaptive control/observation systems (93C40) Orbital mechanics (70M20)

Related Items (1)

Balanced prescribed-distance guidance with impact angle constraint and input saturation

Cites Work

• Control of nonlinear systems with time-varying output constraints
• Eigenvalue bounds for AB+BA, with A, B positive definite matrices
• Control of nonlinear systems under dynamic constraints: a unified barrier function-based approach
• Flexible performance-based robust control for a class of nonlinear systems with input saturation
• Fault-tolerant output-constrained control of unknown Euler-Lagrange systems with prescribed tracking accuracy
• Adaptive attitude tracking control for rigid spacecraft with finite-time convergence
• Time-varying IBLFs-based adaptive control of uncertain nonlinear systems with full state constraints
• Robust Adaptive Control of Feedback Linearizable MIMO Nonlinear Systems With Prescribed Performance
• Attitude Tracking and Disturbance Rejection of Rigid Spacecraft by Adaptive Control
• Low-Complexity Tracking Control of Strict-Feedback Systems With Unknown Control Directions

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