Stability analysis of a hypersonic vehicle controlled by the characteristic model based adaptive controller

DOI10.1007/S11432-011-4455-9zbMath1270.93064OpenAlexW2006259347MaRDI QIDQ362232

Mohammad Hasan, M. Dambrine

Publication date: 20 August 2013

Published in: Science China. Information Sciences (Search for Journal in Brave)

Full work available at URL: http://engine.scichina.com/doi/10.1007/s11432-011-4455-9

zbMATH Keywords

attitude controlstability testcharacteristic modelhypersonic vehicleinterval time-varying system

Mathematics Subject Classification ID

Application models in control theory (93C95) Adaptive control/observation systems (93C40)

Related Items (1)

On-line optimal autonomous reentry guidance based on improved Gauss pseudospectral method

Cites Work

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• Output feedback control of hypersonic vehicles based on neural network and high gain observer
• Prediction-based guidance algorithm for high-lift reentry vehicles
• Adaptive guidance law design based on characteristic model for reentry vehicles
• A necessary and sufficient condition for robust asymptotic stability of time-variant discrete systems

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