A backstepping-based procedure with saturation functions to control the PVTOL system

DOI10.1007/s11071-015-2400-yzbMath1351.93120OpenAlexW2097406618MaRDI QIDQ335462

J. Humberto Sossa-Azuela, Miguel S. Suarez-Castanon, Carlos Fernando Aguilar-Ibáñez

Publication date: 2 November 2016

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

Full work available at URL: https://doi.org/10.1007/s11071-015-2400-y

zbMATH Keywords

feedback linearizationsaturation functionbackstepping procedurePVTOL system

Mathematics Subject Classification ID

Feedback control (93B52) Lyapunov and other classical stabilities (Lagrange, Poisson, (L^p, l^p), etc.) in control theory (93D05) Linearizations (93B18) Asymptotic stability in control theory (93D20)

Related Items (4)

Robust Stabilization of Nonlinear PVTOL Aircraft with Parameter Uncertainties ⋮ Stabilization of the planar vertical take‐off and landing using nonlinear feedback control ⋮ A robust control scheme for a PVTOL system subject to wind disturbances ⋮ Robust constrained trajectory tracking control for a PVTOL aircraft subject to external disturbances

Cites Work

• Unnamed Item
• Unnamed Item
• PVTOL maneuvers guided by a high-level nonlinear controller applied to a rotorcraft machine
• Nonlinear robust output feedback tracking control of a quadrotor UAV using quaternion representation
• Path following for the PVTOL aircraft
• Nonlinear control design for slightly non-minimum phase systems: Application to V/STOL aircraft
• A different look at output tracking: Control of a VTOL aircraft
• Multiple time scale analysis of aircraft longitudinal dynamics with aerodynamic vectoring
• Longitudinal-lateral velocity control design and implementation for a model-scaled unmanned helicopter
• Output tracking of a non-linear non-minimum phase PVTOL aircraft based on non-linear state feedback control
• Global Stabilization of the PVTOL: Real-Time Application to A Mini-Aircraft
• Global stabilization of a PVTOL aircraft model with bounded inputs
• A nonlinear small gain theorem for the analysis of control systems with saturation
• Global configuration stabilization for the VTOL aircraft with strong input coupling
• Interconnection and damping assignment passivity-based control of mechanical systems with underactuation degree one
• An Alternative Nonlinear Control Law for the Global Stabilization of the PVTOL Vehicle
• On Output Tracking Using Dynamic Output Feedback Discrete-Time Sliding-Mode Controllers

This page was built for publication: A backstepping-based procedure with saturation functions to control the PVTOL system