There is rope direct current multiaxis aircraft, characterized by include fuselage, a plurality of electronic rotor, state of flight computer control system, remote controller and DC power supply, and DC power supply passes through the power transmission line externally to be introduced. Divide into groups the motor, make the stator winding of motor establish ties into the branch road and be connected with the power, to the stator winding of each motor or stator winding's partly parallelly connected multifunctional module, multifunctional module includes flight control circuit, direct current reduction voltage circuit, rechargeable battery, with electric loading and fictitious load, state through changing multifunctional module changes control the state of each motor. The utility model provides a being applicable to speed governing / the operation control strategy of multiaxis rotor craft, need not complicated algorithm, only need a switch between motor and the power, the reliability is high, a small amount of electric energy that the state control consumes is also utilized high -efficiently.