Robust Control Design Techniques Using Differential Evolution Algorithms Applied to the PVTOL-Reference-Cited by-同舟云学术

Robust Control Design Techniques Using Differential Evolution Algorithms Applied to the PVTOL

Published:2014-04-10 Issue:3 Volume:20 Page:451-466
ISSN:1079-8587
Container-title:Intelligent Automation & Soft Computing
language:en
Short-container-title:Intelligent Automation & Soft Computing

Author:

Lara David,Panduro Marco,Romero Gerardo,Alcorta Efrain,Betancourt Romeo

Publisher

Computers, Materials and Continua (Tech Science Press)

Subject

Artificial Intelligence,Computational Theory and Mathematics,Theoretical Computer Science,Software

Reference30 articles.

1. Advances in Unmanned Aerial Vehicles

2. Fantoni, I., Lozano, R. & Castillo, P. (2002). A simple stabilization algorithm for the PVTOL aircraft. Proceedings of the 15th IFAC World Congress. Barcelona, Spain.

3. Nonlinear control design for slightly non-minimum phase systems: Application to V/STOL aircraft

4. Al-hiddabi, S., Shen, J. & McClamroch, N. H. (June 1999). A study of flight maneuvers for the PVTOL aircraft model. Proceedings of the American Control Conference. San Diego, California, USA.

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Adaptive Hybrid Control Scheme for Controlling the Position of Coaxial Tri-rotor UAS;Intelligent Automation and Soft Computing;2018

2. Stabilization of the PVTOL aircraft based on a sliding mode and a saturation function;International Journal of Robust and Nonlinear Control;2016-11-17

3. An Actuator Fault Detection and Isolation method design for Planar Vertical Take-off and Landing Unmanned Aerial Vehicle modelled as a qLPV system**This work was supported by the National Council of Science and Technology (Consejo Nacional de Ciencia y Tecnología - CONACYT) of Mexico. The supports is gratefully acknowledged.;IFAC-PapersOnLine;2016

4. A backstepping-based procedure with saturation functions to control the PVTOL system;Nonlinear Dynamics;2015-09-30