Abstract: This invention discloses an aerial device (AD) for manned or unmanned flight, comprising a fuselage main body coupled with two or more aerodynamic units via bearings. Each aerodynamic unit is independently moveable and controllable, and thus able to create their own unique aerodynamic vectors, all of which are combined in varying manners to control the flight of the AD. Each unit comprises a structural part, a thruster with a propeller, and a servo wing positioned behind the propeller. More aerodynamic units may be combined with the main body in order to create more control. The units may be programmed or controlled manually to offset or otherwise account for varying environmental conditions such as slope, wind, and turbulence. The apparatus may further be coupled with a PID controller with a multidimensional field of input and output parameters.