Performance and Stability of Ducted-Fan Uninhabited Aerial Vehicle Model

Author:

Avanzini Giulio1,D’Angelo Salvatore1,de Matteis Guido2

Affiliation:

1. Politecnico di Torino, 10129 Turin, Italy

2. University of Rome “La Sapienza”, 00184 Rome, Italy

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 13 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Validating and Analyzing the Kinematics of a Highly-Gyroscopic VTOL MAV;55th AIAA Aerospace Sciences Meeting;2017-01-05

2. Aerodynamic Analysis of the Ducted Fan for a VTOL UAV in Crosswinds;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2016

3. Nondimensional Modeling of Ducted-Fan Aerodynamics;Journal of Aircraft;2012-01

4. A Compact Method for Modeling the Aerodynamics of Ducted Fan Vehicles;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04

5. Simulation Analysis of the Controllability of a Tandem Ducted Fan Aircraft;AIAA Atmospheric Flight Mechanics Conference and Exhibit;2008-06-15

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