This project consists of the design, production and validation of the physical vehicle and the flight controller (hardware and software).
A quadcopter is chosen given the simplicity and flexibility in order to implement newer control strategies.
Currently, the project is at its third iteration, where the flight controller has been validated on altitudes up to 1000m and lateral winds of 8m/s, with a stable control of the attitude. The payload (except from the systems needed for basic operation) are an FPV system (camera plus transmitter) and high definition compact camera.
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