Rotor wing operating system of coaxial double-rotor-wing helicopter

The invention relates to the field of aviation, and discloses a coaxial dual-rotor helicopter rotor wing operation system, which comprises a rotor wing control module used for controlling the rotating speed of a helicopter rotor wing and the propeller pitch of a propeller; the swash plate module is used for controlling the inclination angle of the helicopter rotor; the automatic flight module is used for realizing automatic flight control of the helicopter; the electrical system module is used for providing required electric power for the rotor wing operation system; and the electric system module is used for providing power for the rotor wings and controlling the rotor wings to incline. The working state of the rotor control module is detected in real time through the fault maintenance unit, detected fault information is transmitted to the module protection unit, the fault information is analyzed, a standby control system is switched in time, emergency response protection measures are taken, whether the stan