A complete fixed-wing autopilot system built in MATLAB/Simulink, covering aircraft dynamics, control system design, and real-time flight simulation via FlightGear. This repository presents a ...
This project designs and analyzes pitch and roll control loops for a small aircraft using classical (PD, Root Locus, Bode) and modern (State-Space, LQR) control methods. It demonstrates how feedback ...
The conceptual design stage is a key step in aircraft development, laying the foundation for performance, efficiency and innovation. Traditionally, this process relies heavily on experienced designers ...
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