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Development of a Data Acquisition System for Unmanned Aerial Vehicle (UAV) System Identification
2017
Aircraft system identification techniques are developed for fixed wing Unmanned Aerial Vehicles (UAV). The use of a designed flight experiment with measured system inputs/outputs can be used to derive aircraft stability derivatives. This project set out to develop a methodology to support an experiment to model pitch damping in the longitudinal short-period mode of a UAV. A Central Composite Response Surface Design was formed using angle of attack and power levels as factors to test for the
doi:10.25777/xqe7-gs03
fatcat:23fggyqzyfghlcdgm2qmwu7u7a