ICUAS'22 Paper Abstract

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Paper ThB3.4

Huang, Jing (Xi'an University of Technology), Wang, Ban (Northwestern Polytechnical University), Deng, Yangping (Northwestern Polytechnical University), ning, Kaikai (Xi'an University of Technology), Zhang, Youmin (Concordia University)

Aerodynamic Design of Fixed-Wing Mode for a Ducted-fan Tiltrotor UAV by Digital DATCOM

Scheduled for presentation during the Regular Session "Multirotor Design and Control II" (ThB3), Thursday, June 23, 2022, 16:30−16:50, Divona-1

2022 International Conference on Unmanned Aircraft Systems (ICUAS), June 21-24, 2022, Dubrovnik, Croatia

This information is tentative and subject to change. Compiled on March 28, 2024

Keywords Multirotor Design and Control, Simulation, UAS Testbeds

Abstract

This paper proposes a novel ducted-fan tiltrotor unmanned aerial vehicle (UAV) with vertical takeoff and landing capability. Firstly, the geometry of the UAV with three views is given. The proposed UAV has three flight modes: helicopter mode, transitional mode and fixed-wing mode. Then, to guarantee that the overall design meets the system specifications, the Digital DATCOM program is utilized to calculate both the stability and control derivatives of the UAV under fixed-wing mode. Finally, numerical simulation results are given to demonstrate the changes of the stability and control derivatives with respect to different cruise speeds and angle of attacks.

 

 

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