Neural networks approximator based robust adaptive controller design of hypersonic flight vehicles systems coupled with stochastic disturbance and dynamic uncertainties

DOI10.1155/2017/7864375zbMath1426.93215OpenAlexW2755934258MaRDI QIDQ1993141

Xiu-yu Zhang, Lingfang Sun, Guo-Qiang Zhu

Publication date: 5 November 2018

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2017/7864375

Mathematics Subject Classification ID

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

Cites Work

• Passive fault-tolerant control design for near-space hypersonic vehicle dynamical system
• Composite antidisturbance control for a class of nonlinear stochastic systems via disturbance observer
• Adaptive backstepping controller design using stochastic small-gain theorem
• Adaptive control with guaranteed transient and steady state tracking error bounds for strict feedback systems
• Adaptive actuator failure compensation for parametric strict feedback systems and an aircraft application.
• Adaptive output feedback fault-tolerant control design for hypersonic flight vehicles
• Neural network-based adaptive backstepping control for hypersonic flight vehicles with prescribed tracking performance
• Dynamic surface control for a class of nonlinear systems
• Adaptive integral dynamic surface control of a hypersonic flight vehicle
• Adaptive NN output-feedback decentralized stabilization for a class of large-scale stochastic nonlinear strict-feedback systems
• Adaptive fuzzy dynamic surface control with prespecified tracking performance for a class of nonlinear systems
• Prescribed Performance Adaptive Control for Multi-Input Multi-Output Affine in the Control Nonlinear Systems
• Dynamic Surface Control of Constrained Hypersonic Flight Models with Parameter Estimation and Actuator Compensation

This page was built for publication: Neural networks approximator based robust adaptive controller design of hypersonic flight vehicles systems coupled with stochastic disturbance and dynamic uncertainties