Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/163762
Title: Agile flight control under multiple disturbances for quadrotor: algorithms and evaluation
Authors: Jia, Jindou
Guo, Kexin
Yu, Xiang
Guo, Lei
Xie, Lihua
Keywords: Engineering::Electrical and electronic engineering
Issue Date: 2022
Source: Jia, J., Guo, K., Yu, X., Guo, L. & Xie, L. (2022). Agile flight control under multiple disturbances for quadrotor: algorithms and evaluation. IEEE Transactions On Aerospace and Electronic Systems, 58(4), 3049-3062. https://dx.doi.org/10.1109/TAES.2022.3143781
Journal: IEEE Transactions on Aerospace and Electronic Systems
Abstract: 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 aerodynamic drag model that considers the drag surface change is developed, containing the deep coupling information between the aerodynamic drag and the system states. A disturbance observer based on the aerodynamic drag model is subsequently designed for suppressing the aerodynamic drag force. In the rotational loop, a full quaternion-based backstepping control is adopted and a nonlinear disturbance observer with consideration of motor dynamics is designed, which can handle the dynamic CoG shift and aerodynamic drag torque. Comparative studies on both simulations and experiments manifest that the agile ability can be ensured by the proposed control framework, especially in the presence of multiple disturbances.
URI: https://hdl.handle.net/10356/163762
ISSN: 0018-9251
DOI: 10.1109/TAES.2022.3143781
Schools: School of Electrical and Electronic Engineering 
Rights: © 2022 IEEE. All rights reserved.
Fulltext Permission: none
Fulltext Availability: No Fulltext
Appears in Collections:EEE Journal Articles

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