Coaxial six-propeller unmanned aerial vehicle

The invention discloses a coaxial six-propeller unmanned aerial vehicle which comprises a vehicle body, a positive power driving system, a negative power driving system and an attitude control system. The fuselage is composed of a fuselage structure and an energy supply system. The positive power driving system drives a positive propeller through a first motor; according to the reverse power driving system, a reverse lift paddle is driven by a second motor; the motor base structural member is mechanically connected with the positive power driving system and the negative power driving system; the attitude control system is installed between the positive power driving system and the negative power driving system or above or below the positive power driving system and the negative power driving system, an attitude motor base structural part is mechanically coupled with a third motor, a fourth motor, a fifth motor and a sixth motor, the third motor drives a first attitude paddle, and the fourth motor drives a sec