Design readings | Design and performance of drones

UAV short drone (Unmanned Aerial Vehicle), it is not manned aircraft using the program control apparatus and radio remote control equipment owned, including helicopter, fixed wing aircraft, multi-rotor, unmanned airship Unmanned parachute wing.

Broadly speaking, it also includes adjacent space vehicles (20-100 km airspace), such as stratospheric airships, high air balls, solar drones, and so on. From a certain point of view, the drone can complete complex air missions and various load tasks under unmanned conditions, and can be regarded as an "airborne robot."

The flight control subsystem is the core system of the whole flight process of the drone to complete take-off, air flight, mission execution and return-to-field recovery. The flight control is equivalent to the driver's role for the manned aircraft. One of the most core technologies. The flight control generally includes three parts: the sensor, the onboard computer and the servo actuating device. The functions realized mainly include the three types of unmanned aircraft attitude stabilization and control, drone mission equipment management and emergency control.

Aiwe concept cargo drone design