Fault tolerant control based on continuous twisting algorithms of a 3-DoF helicopter prototype-Reference-Cited by-同舟云学术

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Fault tolerant control based on continuous twisting algorithms of a 3-DoF helicopter prototype

Published:2020-08 Issue: Volume:101 Page:104486
ISSN:0967-0661
Container-title:Control Engineering Practice
language:en
Short-container-title:Control Engineering Practice

Author:

Pérez-Ventura U.,Fridman L.,Capello E.,Punta E.

Funder

CONACyT (Consejo Nacional de Ciencia y Tecnología), Mexico

PAPIIT-UNAM

Bilateral cooperation Italy-Mexico

Publisher

Elsevier BV

Subject

Applied Mathematics,Electrical and Electronic Engineering,Computer Science Applications,Control and Systems Engineering

Reference40 articles.

1. Approximate back-stepping fault-tolerant control of the flexible air-breathing hypersonic vehicle;An;IEEE/ASME Transactions on Mechatronics,2015

2. Optimal gain for the super-twisting differentiator in the presence of measurement noise;Angulo,2012

3. The differentiation error of noisy signals using the generalized super-twisting differentiator;Angulo,2012

4. Laboratory guide 3 DOF helicopter experiment for MATLAB/Simulink users;Apkarian,2012

5. Generalized reasoning about faults based on the diagnostic matrix;Bartyś;International Journal of Applied Mathematics and Computer Science,2013

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2. Disturbance-Observer-Based Second-Order Sliding-Mode Position Control for Permanent-Magnet Synchronous Motors: A Continuous Twisting Algorithm-Based Approach;Energies;2024-06-17

3. Design, Mathematical Modeling, and Control of an Underactuated 3-DOF Experimental Helicopter;IEEE Access;2024

4. Active fault-tolerant control of quadrotor UAVs with nonlinear observer-based sliding mode control validated through hardware in the loop experiments;Control Engineering Practice;2023-08

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