Robust output feedback attitude tracking control for rigid-flexible coupling spacecraft

DOI10.1016/J.JFRANKLIN.2017.02.031zbMath1404.93028OpenAlexW2592756796MaRDI QIDQ1634453

Y. Aharonov

Publication date: 18 December 2018

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2017.02.031

zbMATH Keywords

asymptotic stabilityfeedback attitude tracking controlrigid-flexible coupling spacecraftrobust attitude tracking control

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Feedback control (93B52) Application models in control theory (93C95) Asymptotic stability in control theory (93D20)

Related Items (3)

Agile attitude maneuver with active vibration-suppression for flexible spacecraft ⋮ Nonlinear stochastic position and attitude filter on the special Euclidean group 3 ⋮ Observer-based continuous finite-time attitude control for rigid–flexible coupling satellites

Cites Work

• T-S fuzzy-model-based piecewise \(\mathcal{H}_\infty\) output feedback controller design for networked nonlinear systems with medium access constraint
• Fault tolerant control using sliding modes with on-line control allocation
• Adaptive input shaping for maneuvering flexible structures
• Mode-dependent nonrational output feedback control for continuous-time semi-Markovian jump systems with time-varying delay
• Dynamics modeling for a rigid-flexible coupling system with nonlinear deformation field
• New results on H∞ dynamic output feedback control for Markovian jump systems with time-varying delay and defective mode information
• Smooth sliding-mode control for spacecraft attitude tracking maneuvers
• Adaptive robust attitude control of a flexible spacecraft

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