A robust guidance and control scheme of an autonomous scale helicopter in presence of wind gusts

DOI10.1080/00207170902948043zbMath1178.93042OpenAlexW2023440297MaRDI QIDQ3654558

Thibault Cheviron, Abdelhamid Chriette, Franck Plestan

Publication date: 6 January 2010

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

Full work available at URL: https://doi.org/10.1080/00207170902948043

zbMATH Keywords

autonomous helicopterhigh-gain unknown input observerrobust non-linear control

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Design techniques (robust design, computer-aided design, etc.) (93B51) Automated systems (robots, etc.) in control theory (93C85) Observability (93B07)

Related Items (2)

On Trajectory Tracking Model Predictive Control of an Unmanned Quadrotor Helicopter Subject to Aerodynamic Disturbances ⋮ Output feedback control design using extended high-gain observers and dynamic inversion with projection for a small scaled helicopter

Cites Work

• Nonlinear control design for slightly non-minimum phase systems: Application to V/STOL aircraft
• State and input estimation for a class of uncertain systems
• Nonlinear modelling and control of helicopters
• Observer design for a class of MIMO nonlinear systems.
• Output feedback stabilization of fully linearizable systems
• Higher-order sliding modes, differentiation and output-feedback control

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