Fuzzy dynamic characteristic model based attitude control of hypersonic vehicle in gliding phase

DOI10.1007/S11432-011-4193-ZzbMath1227.93067OpenAlexW2038933015MaRDI QIDQ543237

Jiang Li, Xiong Luo

Publication date: 17 June 2011

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

Full work available at URL: http://engine.scichina.com/doi/10.1007/s11432-011-4193-z

zbMATH Keywords

hypersonic vehiclefuzzy dynamic characteristic modelinggliding attitude control

Mathematics Subject Classification ID

Fuzzy control/observation systems (93C42) Application models in control theory (93C95) Automated systems (robots, etc.) in control theory (93C85)

Related Items (5)

On-line optimal autonomous reentry guidance based on improved Gauss pseudospectral method ⋮ T-S fuzzy modelling and \(H_{\infty}\) attitude control for hypersonic gliding vehicles ⋮ Multiple characteristic model‐based golden‐section adaptive control: Stability and optimization ⋮ Characteristic model-based \(H_2/H_\infty\) robust adaptive control during the re-entry of hypersonic cruise vehicles ⋮ Direct parametric attitude tracking control for generic hypersonic vehicle

Cites Work

• Characteristic model based control of the X-34 reusable launch vehicle in its climbing phase
• Analysis and design for a class of complex control systems. I: Fuzzy modelling and identification
• Adaptive guidance law design based on characteristic model for reentry vehicles
• Characteristic modeling and the control of flexible structure

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