System Identification of a Nonlinear Flight Dynamics Model for a Small, Fixed-Wing UAV

System Identification of a Nonlinear Flight Dynamics Model for a Small, Fixed-Wing UAV

This thesis describes the development of a nonlinear flight dynamics model for a small, fixed-wing unmanned aerial vehicle (UAV). Models developed for UAVs can be used for many applications including risk analysis, controls system design and flight simulators. Several challenges exist for system ide...

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Bibliographic Details
Main Author: Simmons, Benjamin Mason
Other Authors: Aerospace and Ocean Engineering
Format: Others
Published: Virginia Tech 2019
Subjects:
Output Error Method
Unmanned Aerial Vehicle
Vortex Lattice Method
Flight Testing
Aerodynamic Modeling
Parameter Estimation
Online Access:http://hdl.handle.net/10919/95324

Internet

http://hdl.handle.net/10919/95324

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