AIAA SCITECH 2024 Forum 2024
DOI: 10.2514/6.2024-2875
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Dynamics Modeling of Multirotor type UAV with the Blade Element Momentum Theory and Nonlinear Controller Design for a Wind Environment

On Park,
Hyo-Sang Shin

Abstract: This paper presents an aerodynamics modeling of a rotary type Vertical Take-Off and Landing (VTOL) aircraft using the Blade Element Momentum Theory (BEMT). The BEMT is incorporated into the rigid body dynamics to describe main force and its reactive torque by rotor of the multirotor UAV. The dynamics modeling can demonstrate the motion of the multirotor UAV in the presence of gust or wind in an unsteady environment effectively. In order to operate the multirotor UAV, a robust nonlinear control technique is des… Show more

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