A constrained error-based MPC for path following of quadrotor with stability analysis

DOI10.1007/S11071-019-04859-0zbMath1459.93069OpenAlexW2939815894WikidataQ128042746 ScholiaQ128042746MaRDI QIDQ2023075

Abolfazl Eskandarpour, Inna Sharf

Publication date: 3 May 2021

Published in: Nonlinear Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11071-019-04859-0

zbMATH Keywords

constrained model predictive controlLaguerre functionprescribed stabilityquadrotor dynamics

Mathematics Subject Classification ID

Linear systems in control theory (93C05) Automated systems (robots, etc.) in control theory (93C85) Asymptotic stability in control theory (93D20) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (6)

Compound tracking control based on MPC for quadrotors with disturbances ⋮ A multi-rate hierarchical fault-tolerant adaptive model predictive control framework: theory and design for quadrotors ⋮ Mu-based trajectory tracking control for a quad-rotor UAV ⋮ Trajectory tracking of a quadrotor using extend state observer based U-model enhanced double sliding mode control ⋮ Prescribed chattering reduction control for quadrotors using aperiodic signal updating ⋮ Fractional-order global sliding mode controller for an uncertain quadrotor UAVs subjected to external disturbances

Cites Work

• Nonlinear robust output feedback tracking control of a quadrotor UAV using quaternion representation
• An integral predictive/nonlinear \(\mathcal H_{\infty}\) control structure for a quadrotor helicopter
• Model predictive control system design and implementation using \texttt{MATLAB}
• Adaptive and robust control of quadrotor aircrafts with input saturation
• Constrained model predictive control: Stability and optimality
• Robust trajectory tracking control for a laboratory helicopter
• Nonlinear adaptive control for quadrotor flying vehicle
• System identification using Laguerre models
• On Trajectory Tracking Model Predictive Control of an Unmanned Quadrotor Helicopter Subject to Aerodynamic Disturbances

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