Adaptive variable structure maneuvering control and vibration reduction of three-axis stabilized flexible spacecraft

DOI10.3166/EJC.12.654-668zbMath1293.93157OpenAlexW1965628351MaRDI QIDQ2512081

Qinglei Hu, Guangfu Ma

Publication date: 7 August 2014

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

Full work available at URL: https://semanticscholar.org/paper/a8efd3f581f4a27f5b714dda7b9728c5aab6d40c

zbMATH Keywords

flexible spacecraftattitude controlvibration suppressioninput nonlinearitiesvariable structure output feedback control

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Feedback control (93B52) Nonlinear systems in control theory (93C10) Variable mass, rockets (70P05) Variable structure systems (93B12)

Related Items (4)

Coordinated control of path tracking and energy optimization for in-wheel motor drive electric buses with velocity estimation ⋮ Trajectory planning and robust tracking control for a class of active articulated tractor-trailer vehicle with on-axle structure ⋮ Neural network-based adaptive attitude tracking control for flexible spacecraft with unknown high-frequency gain ⋮ Robust adaptive backstepping attitude stabilization and vibration reduction of flexible spacecraft subject to actuator saturation

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