A variable aerodynamic configuration of the aircraft

The present invention discloses an aircraft aerodynamic layout for a variable, including full-motion canard steering gear, with telescopic mechanism, the first to sixth machine module, the body, resistance of two rudders, two vertical tail folded, electronic speed , a propeller, a receiver and a remote controller, a telescopic mechanism driven by the motor module may be implemented full-motion canard extendable and retractable, while the folded fin deployment with a respective flattened, thus achieving canard and tailless conversion between the flying wing. The present invention can realize the conversion between the flying wing tailless and canard in the air, both stealthy flying wing tailless and canard relatively high mobility, and a large load STOL performance.