Abbreviation: drone

Air-powered aircraft managed by a remote control station and not carrying an operator

Use aerodynamics to provide the required lift for the aircraft and be able to guide it remotely

Able to carry payload

Can be used once or recycled and used again

No cockpit, no driver

Installed with automatic pilot, program control device and other equipment

Personnel on the ground, on the ship or at the mother aircraft remote control station

Tracking, positioning, remote control, telemetry and digital transmission through radar

Flight mode: It can take off like an ordinary airplane under radio control or be launched into the sky with a booster rocket, or it can be taken into the air by the mother aircraft.

During recovery: it can land automatically in the same way as an ordinary aircraft landing process, or it can be intercepted by remote control with a parachute or blocker.

UAV body

Related remote control stations

required instructions

control data link

Approved model design provisions

Other supporting parts

composition:

UAV airborne equipment

The body is an aerial platform, its function depends on what airborne equipment is carried

military drone

Civilian drone

fixed wing

rotor

Other types

military

Civilian

Features:

Fly forward using thrust generated by propellers and turbine engines

Lift comes from the relative motion of the wing and the air

Common wings

System composition

advantage:

shortcoming:

single rotor

Multi-rotor

umbrella wing

flapping wings