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Non-Linear Modeling and Control of Unmanned Air Vehicle
The aim of this thesis is to design and simulate a Dynamic Inversion based autopilot for a fixed wing aircraft. The autopilot provides the aircraft motion stability by commanding the different aircraft control surfaces and ...
Mazari UAV Adaptive Autopilot System Design and Implementation
Autonomous unmanned aerial vehicle (UAV) research started at AUS in 2005. Linear and nonlinear aircraft models and system identification of the aircraft system were developed to design flight control laws. Proportional-i ...