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Aerodynamic modeling and parameter estimation of a quadrotor helicopter
Date
2014-01-01
Author
Kaya, Derya
Kutay, Ali Türker
Metadata
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This study focuses on aerodynamic modeling of a quadrotor helicopter and the estimation of the model parameters in wind tunnel tests for hover, vertical climb, and forward flight conditions. The motion of a quadrotor is mainly affected by the aerodynamic forces and moments generated by rotors. Accurate calculation of rotor loads is essential for high fidelity simulation of a quadrotor. Momentum and blade element theories are used to obtain expressions for rotor forces and moments for a traveling vehicle. The parameters of the models are then identified through wind tunnel tests where the forces and moments created under various wind conditions and rotor speeds are measured with a six axes balance system.
Subject Keywords
Measuring
,
Testing and validation of aerospace systems
URI
https://hdl.handle.net/11511/57803
DOI
https://doi.org/10.2514/6.2014-2558
Conference Name
AIAA Atmospheric Flight Mechanics Conference
Collections
Department of Aerospace Engineering, Conference / Seminar
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D. Kaya and A. T. Kutay, “Aerodynamic modeling and parameter estimation of a quadrotor helicopter,” presented at the AIAA Atmospheric Flight Mechanics Conference, Atlanta, GA, 2014, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/57803.
