Small unmanned aircraft are typically defined as UAVs with a maximum takeoff weight of less than 55 pounds (25 kg). These aircraft can be classified into several categories, including fixed-wing, rotary-wing, and hybrid configurations. The design and operation of small UAVs rely heavily on the principles of aerodynamics, flight mechanics, and control systems.
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Small unmanned aircraft, commonly known as drones, are defined by their ability to operate without an onboard human pilot. While they may appear simple, their operation relies on a complex synergy of aerodynamics, control theory, and autonomous navigation. I. The Theoretical Foundation of sUAS Small unmanned aircraft are typically defined as UAVs