Abstract
The guidance law is required for the aircraft to autopilot along the fixed path. The LOS(Line-of-Sight) guidance law is mainly used to follow the path. In this paper, we propose aircraft guidance systems that consist of LOS guidance law and the fuzzy self-tuning PID controller to follow the path more precisely. In addition, we compared the path following performance and feasibility of various existing research of LOS guidacne law using Matlab/Simulink simulation.
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