Agile flight control under multiple disturbances for quadrotor: algorithms and evaluation

In this article, a scheme of anti-disturbance agile flight control is developed for a maneuverable quadrotor unmanned aerial vehicle, subject to the aerodynamic drag, dynamic shift of center of gravity (CoG), and motor dynamics. A cascaded control framework is adopted. In the translational loop, an...

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Bibliographic Details
Main Authors: Jia, Jindou, Guo, Kexin, Yu, Xiang, Guo, Lei, Xie, Lihua
Other Authors: School of Electrical and Electronic Engineering
Format: Article
Language:English
Published: 2022
Subjects:
Online Access:https://hdl.handle.net/10356/163762
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Institution: Nanyang Technological University
Language: English