Continuous appointed‐time prescribed performance attitude tracking control for rigid spacecraft with actuator faults on SO(3)

DOI10.1002/rnc.6991OpenAlexW4386850804MaRDI QIDQ6117459

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Publication date: 20 March 2024

Published in: International Journal of Robust and Nonlinear Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/rnc.6991

zbMATH Keywords

spacecraftattitude trackingfault-tolerant controlappointed-time prescribed performance control

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Perturbations in control/observation systems (93C73) Asymptotic stability in control theory (93D20) Orbital mechanics (70M20)

Cites Work

• Exponential stability of an attitude tracking control system on SO(3) for large-angle rotational maneuvers
• Coupled orbit-attitude dynamics and trajectory tracking control for spacecraft electromagnetic docking
• Prescribed performance finite-time tracking control for uncertain nonlinear systems
• Reaction wheel fault tolerant control for spacecraft attitude stabilization with finite-time convergence
• Fault‐tolerant spacecraft attitude control under actuator saturation and without angular velocity
• Adaptive fault‐tolerant spacecraft attitude control using a novel integral terminal sliding mode
• Robust Adaptive Control of Feedback Linearizable MIMO Nonlinear Systems With Prescribed Performance
• Fixed‐time attitude tracking control for spacecraft based on adding power integrator technique
• Reaction wheel fault‐tolerant finite‐time control for spacecraft attitude tracking without unwinding
• Anti-Unwinding Sliding Mode Attitude Maneuver Control for Rigid Spacecraft
• Rigid-Body Attitude Control

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