AIAA Atmospheric Flight Mechanics Conference, 2016, California, Amerika Birleşik Devletleri, 4 - 08 Ocak 2016
System identification of an unmanned aerial vehicle (UAV) called Pelikan, which is a fixed wing UAV developed by the Turkish Aerospace Industries, is presented. Time domain identification and frequency domain identification, are used to obtain a linear model of Pelikan. Inputs and outputs of two identification methods are compared and verified with the test results.