Robust \(H_\infty \) output feedback control for attitude stabilization of a flexible spacecraft

DOI10.1007/s11071-016-2624-5zbMath1354.93139OpenAlexW2299971817MaRDI QIDQ332763

Shenghui Wen, Shu-Nan Wu

Publication date: 9 November 2016

Published in: Nonlinear Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11071-016-2624-5

zbMATH Keywords

stabilizationrobust controloutput feedbackflexible spacecraftattitude dynamics

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Feedback control (93B52) (H^infty)-control (93B36) Automated systems (robots, etc.) in control theory (93C85) Adaptive or robust stabilization (93D21) Control of mechanical systems (70Q05)

Related Items (6)

Agile attitude maneuver with active vibration-suppression for flexible spacecraft ⋮ Observer‐based H_∞ control of a stochastic Korteweg–de Vries–Burgers equation ⋮ Robust finite-time non-fragile sampled-data control for T-S fuzzy flexible spacecraft model with stochastic actuator faults ⋮ Boundary control of linear stochastic reaction‐diffusion systems ⋮ Fuzzy logic based fault-tolerant attitude control for nonlinear flexible spacecraft with sampled-data input ⋮ Attitude dynamics of coupled spacecraft undergoing fuel transfer

Cites Work

• Robust adaptive sliding mode attitude maneuvering and vibration damping of three-axis-stabilized flexible spacecraft with actuator saturation limits
• Self-scheduled \({\mathcal H}_ \infty\) control of linear parameter-varying systems: A design example
• Robust attitude tracking control of flexible spacecraft for achieving globally asymptotic stability
• The attitude control problem
• Classical and robust H(infinity) control redesign for the Hubble Space Telescope
• A linear matrix inequality approach to H_∞ control
• On-Orbit Robust Control Experiment of Flexible Spacecraft ETS-VI
• H-infinity control of an Earth observation satellite
• Robust attitude and vibration control of a nonlinear flexible spacecraft
• Adaptive robust attitude control of a flexible spacecraft

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