학술논문
Mini airplane: Design, aerodynamic modeling and stability
Document Type
Conference
Author
Source
2014 11th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE) Electrical Engineering, Computing Science and Automatic Control (CCE), 2014 11th International Conference on. :1-6 Sep, 2014
Subject
Language
Abstract
This paper presents the development of a mini airplane UAV, focusing on the aerodynamic design, modeling and stability. Mathematical model of the vehicle is obtained using the Euler-Lagrange formulation and includes aerodynamic parameters of the design. For the stability, a classic control law is proposed taking in account the aerodynamic parameters and the sensors bandwidth implemented in the aircraft. Simulation results are shown for the closed-loop system of the vehicle. Finally, aerodynamic design and avionics are based on flying and handling qualities for having a mini airplane that performs a reliable and stable flight.