Disturbance Rejection Attitude Control for a Quadrotor: Theory and Experiment

In this article, an attitude tracking controller is designed for a quadrotor unmanned aerial vehicle (UAV) subject to lumped disturbances. Firstly, the attitude dynamical model of the quadrotor under external disturbances is established. Subsequently, an improved sliding mode control (SMC) strategy...

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Bibliographic Details
Published in:International Journal of Aerospace Engineering
Main Authors: Li Ding, Qing He, Chengjun Wang, Rongzhi Qi
Format: Article
Language:English
Published: Wiley 2021-01-01
Online Access:http://dx.doi.org/10.1155/2021/8850071