Attitude Control of Unmanned Aerial Vehicle Based on Sliding Mode Technique with Parameter Estimation

An adaptive robust controller for nonlinear and coupling dynamic of aerial vehicle has been presented. In this paper an adaptive sliding mode controller (ASMC) is integrated to design the attitude control for the inner loops of nonlinear coupling dynamic of Unmanned Aerial Vehicle (UAV) in the prese...

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Bibliographic Details
Main Authors: A. A. Akbari*, S. Amini
Format: Article
Language:English
Published: Islamic Azad University-Isfahan (Khorasgan) Branch 2017-08-01
Series:International Journal of Advanced Design and Manufacturing Technology
Subjects:
Online Access:https://admt.isfahan.iau.ir/article_535013_7f87649058823d8c256d24ad4bbdbd05.pdf