Control of a time-varying hypersonic vehicle model subject to inlet un-start condition

DOI10.1016/j.jfranklin.2018.04.035zbMath1390.93241OpenAlexW2802311669WikidataQ129931958 ScholiaQ129931958MaRDI QIDQ1644276

Hao An, Hongwei Xia, Qian-Qian Wu, Chang-Hong Wang

Publication date: 21 June 2018

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2018.04.035

zbMATH Keywords

barrier functionsfault-tolerant controllerair-breathing hypersonic vehicles (AHVs)time-varying uncertain parametersvelocity-dependent constraint on angle-of-attack

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Control/observation systems with incomplete information (93C41) Application models in control theory (93C95)

Related Items

Input-and-measurement event-triggered control for flexible air-breathing hypersonic vehicles with asymmetric partial-state constraints ⋮ Simplified fault-tolerant adaptive control of air-breathing hypersonic vehicles ⋮ Adaptive fault tolerant control for hypersonic flight vehicle system with state constraints ⋮ Multiple Lyapunov function-based longitudinal maneuver control of air-breathing hypersonic vehicles ⋮ Hypersonic flight control considering parametric variations and VGI effects

Cites Work

• Exponential sliding mode tracking control via back-stepping approach for a hypersonic vehicle with mismatched uncertainty
• Reference command tracking control for an air-breathing hypersonic vehicle with parametric uncertainties
• Adaptive restricted trajectory tracking for a non-minimum phase hypersonic vehicle model
• Decentralized adaptive tracking control for a class of interconnected nonlinear time-varying systems
• Robust exact differentiation via sliding mode technique
• Adaptive nonlinear control without overparametrization
• Barrier Lyapunov function-based adaptive control for hypersonic flight vehicles
• Robust adaptive neural control of flexible hypersonic flight vehicle with dead-zone input nonlinearity
• Uncertainty modeling and robust minimax LQR control of multivariable nonlinear systems with application to hypersonic flight
• Reference governor for constrained nonlinear systems
• Command Filtered Backstepping
• Prescribed-performance fault-tolerant control for feedback linearisable systems with an aircraft application
• Dynamic Surface Control of Constrained Hypersonic Flight Models with Parameter Estimation and Actuator Compensation

This page was built for publication: Control of a time-varying hypersonic vehicle model subject to inlet un-start condition