Static \(\mathcal H_{\infty}\) loop shaping control of a fly-by-wire helicopter

DOI10.1016/j.automatica.2005.04.001zbMath1093.93512OpenAlexW2100419780MaRDI QIDQ2576104

Emmanuel Prempain, Ian Postlethwaite

Publication date: 8 December 2005

Published in: Automatica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.automatica.2005.04.001

zbMATH Keywords

Linear matrix inequalitiesStatic output feedback\(\mathcal H_{\infty}\) loop shapingHelicopter control

Mathematics Subject Classification ID

Design techniques (robust design, computer-aided design, etc.) (93B51) (H^infty)-control (93B36) Automated systems (robots, etc.) in control theory (93C85) Synthesis problems (93B50)

Related Items (17)

Improved nonlinear trajectory tracking using RBFNN for a robotic helicopter ⋮ Robust hierarchical control for uncertain multivariable hexarotor systems ⋮ Design of low order robust controllers for a VSC HVDC power plant terminal ⋮ Output Feedback $\mathcal{H}_\infty$ Loop-Shaping Controller Synthesis ⋮ Trajectory tracking anti-disturbance control for unmanned aerial helicopter based on disturbance characterization index ⋮ Sufficient dilated LMI conditions for \(H_\infty\) static output feedback robust stabilization of linear continuous-time systems ⋮ \(\mathcal L_2\) optimal decentralised static output feedback stabilisation of a network of dynamical systems ⋮ Design of static \(H_\infty\) loop shaping controller in four-block framework using LMI approach ⋮ A linear matrix inequality approach to parametric \(H_{\infty }\) loop shaping control ⋮ Autonomous Control of Micro Flying Robot ⋮ Decoupled Robust Velocity Control for Uncertain Quadrotors ⋮ Discrete-time static \(H_\infty\) loop shaping control via LMIs ⋮ Robust Flight Control Using Nonsmooth Optimization for a Tandem Ducted Fan Vehicle ⋮ Robust output tracking control of a laboratory helicopter for automatic landing ⋮ Robust attitude tracking control of small-scale unmanned helicopter ⋮ Model-based control of thermoacoustic instabilities in partially premixed lean combustion – a design case study ⋮ Robust trajectory tracking control for a laboratory helicopter

Uses Software

• LMI toolbox

Cites Work

• Unnamed Item
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