Robust Parameter Dependent Receding HorizonH∞Control of Flexible Air-Breathing Hypersonic Vehicles with Input Constraints

DOI10.1002/asjc.1084zbMath1332.93111OpenAlexW1552205257MaRDI QIDQ2789952

Li-Xin Wang, Jieyu Liu, Gang Liu, Bing He, Wei-Wei Qin

Publication date: 2 March 2016

Published in: Asian Journal of Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/asjc.1084

zbMATH Keywords

linear matrix inequalitieslinear parameter varyingtensor product model transformationair-breathing hypersonic vehicle (ABHSV)parameter dependent receding horizon \(H_{\infty}\) control

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Application models in control theory (93C95) (H^infty)-control (93B36)

Related Items

Mixed‐Objective Robust Dynamic Output Feedback Controller Synthesis for Continuous‐Time Polytopic Lpv Systems ⋮ Robust model predictive tracking control of hypersonic vehicles in the presence of actuator constraints and input delays ⋮ Active Vibration Control for a Flexible‐Link Manipulator with Input Constraint Based on a Disturbance Observer ⋮ Influence of the Tensor Product Model Representation Of QLPV Models on The Feasibility of Linear Matrix Inequality

Cites Work

• TP-Model Transformation-Based-Control Design Frameworks
• Design of Robust Control Systems for a Hypersonic Aircraft
• Optimum Mission Performance and Multivariable Flight Guidance for Airbreathing Launch Vehicles
• Co‐ordination and control of distributed spacecraft systems using convex optimization techniques
• Analytical aeropropulsive-aeroelastic hypersonic-vehicle model with dynamic analysis