Nonlinear adaptive tracking control of non-minimum phase hypersonic flight vehicles with unknown input nonlinearity

DOI10.1007/S11071-017-3716-6zbMath1390.93435OpenAlexW2748307726MaRDI QIDQ1637260

Bin Xu, Xiao-Sheng Si, Chang-Hua Hu, Xiaoxiang Hu

Publication date: 7 June 2018

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

Full work available at URL: https://doi.org/10.1007/s11071-017-3716-6

zbMATH Keywords

input nonlinearitynonlinear adaptive controlhypersonic flight vehicles (HFVs)

Mathematics Subject Classification ID

Nonlinear systems in control theory (93C10) Adaptive control/observation systems (93C40) Automated systems (robots, etc.) in control theory (93C85)

Related Items (1)

Robust fault accommodation strategy of the reentry vehicle: a disturbance estimate-triggered approach

Cites Work

• Precision preview-based stable-inversion for nonlinear nonminimum-phase systems: the VTOL example
• Nonlinear control systems.
• Adaptive output feedback fault-tolerant control design for hypersonic flight vehicles
• Fuzzy stable inversion-based output tracking for nonlinear non-minimum phase system and application to FAHVs
• Adaptive sliding mode tracking control for a flexible air-breathing hypersonic vehicle
• Robust adaptive neural control of flexible hypersonic flight vehicle with dead-zone input nonlinearity
• Adaptive discrete-time controller design with neural network for hypersonic flight vehicle via back-stepping
• Tracking nonlinear non-minimum phase systems using sliding control
• Dynamic Surface Control of Constrained Hypersonic Flight Models with Parameter Estimation and Actuator Compensation

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