Adaptive Variable Structure and Active Vibration Reduction for Flexible Spacecraft under Input Nonlinearity

DOI10.1177/1077546307078242zbMath1182.74091OpenAlexW1982021877MaRDI QIDQ5189482

Xie, Lihua, Huijun Gao, Qinglei Hu

Publication date: 16 March 2010

Published in: Journal of Vibration and Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1177/1077546307078242

zbMATH Keywords

vibration controlflexible spacecraftoutput feedback sliding mode control (OFSMC)suboptimal positive position feedback (SOPPF)

Mathematics Subject Classification ID

Adaptive control/observation systems (93C40) Vibrations in dynamical problems in solid mechanics (74H45)

Uses Software

• LMI toolbox

Cites Work

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• Static output feedback stabilization: An ILMI approach
• A sliding mode controller with improved adaptation laws for the upper bounds on the norm of uncertainties
• Variable structure control design for uncertain dynamic systems with sector nonlinearities
• Variable structure control of a class of uncertain systems.
• Parametric control of an axially moving string via fuzzy sliding-mode and fuzzy neural network methods
• Sliding mode control using modified Rodrigues parameters
• Variable-structure control of spacecraft large-angle maneuvers
• Variable-structure control of spacecraft attitude maneuvers
• On variable structure output feedback controllers for uncertain dynamic systems
• Decentralized variable-structure control design for uncertain large-scale systems with series nonlinearities
• Adaptive Control Design and Analysis
• Output feedback sliding mode control of base isolated structures