Robust adaptive neural control of flexible hypersonic flight vehicle with dead-zone input nonlinearity

DOI10.1007/s11071-015-1958-8zbMath1351.93102OpenAlexW2024612665MaRDI QIDQ2520649

Bin Xu

Publication date: 16 December 2016

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

Full work available at URL: https://doi.org/10.1007/s11071-015-1958-8

zbMATH Keywords

dynamic surface controldead-zone input nonlinearitydirect neural controlflexible hypersonic flight vehicleNussbaum function gain

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Adaptive control/observation systems (93C40) Automated systems (robots, etc.) in control theory (93C85)

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