Resonance-frequency-variable electromagnetic driven type double-drive micro flapping wing aircraft

The invention provides a resonance-frequency-variable electromagnetic driven type double-drive micro flapping wing aircraft, which comprises two DC (Direct current) motors, two current torsion-variable materials, DC motor fixing elements, two wing fixing elements and two wings comprising passive torsion hinges. During the flapping of the wings driven by the DC motors, the current torsion-variable materials have different torsion rigidities under different incidental charges or potentials, so as to obtain different resonance frequencies. The aircraft is high in controllability; the goal that the aircraft resonates to obtain a maximum flapping angle when flapping at different frequencies becomes possible; meanwhile, as each DC motor controls one wing independently, the flying attitude is diversified and the aircraft can be adaptive to various environments.