Robust output tracking control of a class of non-minimum phase systems and application to VTOL aircraft

DOI10.1080/00207179.2011.627596zbMath1236.93048OpenAlexW2112693234MaRDI QIDQ3119135

Yan Lin, Shanwei Su

Publication date: 7 March 2012

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

Full work available at URL: https://doi.org/10.1080/00207179.2011.627596

zbMATH Keywords

robust controlnonlinear systemoutput trackingnon-minimum phaseVTOL aircraftuncertainty and disturbance estimator (UDE

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Nonlinear systems in control theory (93C10) Application models in control theory (93C95) Estimation and detection in stochastic control theory (93E10)

Related Items (8)

Approximate stable system centre approach to output tracking of non-minimum phase nonlinear systems ⋮ Design of \(\alpha\)-filter-based UDE controllers considering finite control bandwidth ⋮ Exponentially stable observer-based controller for VTOL-UAVs without velocity measurements ⋮ A novel approach to stable zero dynamics of sampled-data models for nonlinear systems in backward triangle sample and hold case ⋮ Finite-time observer-based output-feedback control for the global stabilisation of the PVTOL aircraft with bounded inputs ⋮ GD-aided IOL (input–output linearisation) controller for handling affine-form nonlinear system with loose condition on relative degree ⋮ Tracking with prescribed performance for linear non-minimum phase systems ⋮ Singularity-conquering ZG controllers of z2g1 type for tracking control of the IPC system

Cites Work

• Nonlinear control design for slightly non-minimum phase systems: Application to V/STOL aircraft
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• Output regulation of nonlinear systems
• Robust input–output linearisation using uncertainty and disturbance estimation
• Global stabilization of a PVTOL aircraft model with bounded inputs
• Tracking nonlinear non-minimum phase systems using sliding control
• Nonlinear inversion-based output tracking
• Global configuration stabilization for the VTOL aircraft with strong input coupling
• An Alternative Nonlinear Control Law for the Global Stabilization of the PVTOL Vehicle
• A prediction‐based nonlinear controller for stabilization of a non‐minimum phase PVTOL aircraft
• Output tracking for nonlinear non-minimum phase systems and application to PVTOL aircraft

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