Nonlinear Modeling the Quadcopter Considering the Aerodynamic Interaction

Nonlinear Modeling the Quadcopter Considering the Aerodynamic Interaction

This paper presents a nonlinear model of the quadcopter to simulate the actual motion. An aerodynamic model of the rotor is obtained through wind-tunnel tests, which consider the variations in the rotor&#x2019;s angular velocity, incoming flow speed, and angle of attack of the rotor (<inline-...

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Bibliographic Details
Main Authors: Jianchuan Ye, Jiang Wang, Tao Song, Zeliang Wu, Pan Tang
Format: Article
Language:English
Published: IEEE 2021-01-01
Series:IEEE Access
Subjects:
Quadcopter
aerodynamic interaction
rotor model
wind-tunnel tests
Online Access:https://ieeexplore.ieee.org/document/9552918/

Internet

https://ieeexplore.ieee.org/document/9552918/

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