Abstract
This article presents the math modeling of a fixed wing Unmanned Aerial Vehicle (UAV) for a flight simulator, using a numerical method. The UAV is controlled through radio control or mission plan. The mathematical model contains a numerical approximation considering multiple Single Input Single Output (SISO) systems that related altitude, pitch, roll and yaw angle as an input parameters and yaw speed, x, y, z axis speed as output parameters.
The signal analysis shows unpredictable behavior during manual controlled flight, but an acceptable stable group of data in controlled mission.
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Acknowledgement
This work is part of the research project 2016-PIC-024 from Universidad de las Fuerzas Armadas ESPE, directed by Dr. Wilbert G. Aguilar.
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Orbea, D., Moposita, J., Aguilar, W.G., Paredes, M., León, G., Jara-Olmedo, A. (2017). Math Model of UAV Multi Rotor Prototype with Fixed Wing Aerodynamic Structure for a Flight Simulator. In: De Paolis, L., Bourdot, P., Mongelli, A. (eds) Augmented Reality, Virtual Reality, and Computer Graphics. AVR 2017. Lecture Notes in Computer Science(), vol 10324. Springer, Cham. https://doi.org/10.1007/978-3-319-60922-5_15
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DOI: https://doi.org/10.1007/978-3-319-60922-5_15
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