The utility model relates to a kind of unmanned aerial vehicle structure of front and rear wing coordinated control, including bearing shaft, bearing shaft is equipped with installation slot, installation slot is equipped with installation shell, installation shell is fixed with mounting plate, full-actuated steering gear is installed on mounting plate, installation shell is fixedly connected with baffle, baffle is equipped with wing movable link key, wing movable link key is externally rotatably equipped with
rudder connecting piece,
rudder connecting piece is fixedly connected with extension plate, extension plate is rotatably connected with eccentric wheel connecting rod, and pull rod is arranged between full-actuated steering gear and eccentric wheel connecting rod;By starting full-actuated steering gear, drive pull rod relative movement, to indirectly drive
rudder connecting piece rotation, to realize the deflection of different angles of front and rear wing surface, realize the adjustment wing surface aerodynamic distribution of unmanned aerial vehicle, so that unmanned aerial vehicle can respond in time when low-altitude flight, hovering or big maneuvering attitude adjustment, improve the maneuverability and control performance of unmanned aerial vehicle.