Output sliding mode-based stabilization of underactuated 3-DOF helicopter prototype and its experimental verification

DOI10.1016/J.JFRANKLIN.2015.01.010zbMath1395.93155OpenAlexW2057649002MaRDI QIDQ1660413

Marlen Meza-Sánchez, Luis T. Aguilar, Yury V. Orlov

Publication date: 16 August 2018

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2015.01.010

zbMATH Keywords

feedback designhelicopter prototypeoutput sliding mode-based stabilizationsliding mode control synthesis

Mathematics Subject Classification ID

Feedback control (93B52) Stabilization of systems by feedback (93D15) Application models in control theory (93C95) Design techniques (robust design, computer-aided design, etc.) (93B51) Asymptotic stability in control theory (93D20) Variable structure systems (93B12) Synthesis problems (93B50)

Related Items (2)

Adaptive sensor-fault tolerant control for a class of MIMO uncertain nonlinear systems: adaptive nonlinear filter-based dynamic surface control ⋮ Dual terminal sliding mode control design for rigid robotic manipulator

Cites Work

• Unnamed Item
• Discontinuous systems. Lyapunov analysis and robust synthesis under uncertainty conditions
• Sliding modes in control and optimization. Transl. from the Russian
• Nonlinear output-feedback tracking using high-gain observer and variable structure control
• Nonlinear modelling and control of helicopters
• Robust regulation for a 3-DOF helicopter via sliding-mode observation and identification
• State-space solutions to standard H/sub 2/ and H/sub infinity / control problems
• Lyapunov-based settling time estimate and tuning for twisting controller
• Performance Recovery of Feedback-Linearization-Based Designs
• Robust nonlinear motion control of a helicopter
• Second-order sliding-mode observer for mechanical systems
• Super twisting algorithm-based step-by-step sliding mode observers for nonlinear systems with unknown inputs

This page was built for publication: Output sliding mode-based stabilization of underactuated 3-DOF helicopter prototype and its experimental verification