Separated type inverted-V-shaped tail wing control mechanism of miniature flapping-wing aircraft

The invention discloses a separated type inverted-V-shaped tail wing control mechanism of a miniature flapping-wing aircraft. The separated type inverted-V-shaped tail wing control mechanism comprises a body frame, a right tail vane engine, a right tail vane engine rocking arm, a right connecting rod, a right hinge, a right tail vane, a right tail vane rocking arm, a left tail vane, a left tail vane rocking arm, a left connecting rod, a left hinge, a left tail vane engine rocking arm, a left tail vane engine, a left inverted-V-shaped bracket and a right inverted-V-shaped bracket, wherein two sides on the body frame are respectively provided with the left inverted-V-shaped bracket and the right inverted-V-shaped bracket and are respectively connected with the left tail vane and the right tail vane by the left hinge and the right hinge; the left inverted-V-shaped bracket is provided with the left tail vane engine; one end of the left tail vane engine rocking arm is connected with the left tail vane engine, and the other end of the left tail vane engine rocking arm is connected with the left connecting rod; the other end of the left connecting rod is connected with the left tail vane rocking arm; the right inverted-V-shaped bracket is provided with the right tail vane engine; one end of the right tail vane engine rocking arm is connected with the right tail vane engine, and the other end of the right tail vane engine rocking arm is connected with the right connecting rod; and the other end of the right connecting rod is connected with the right tail vane rocking arm. The separated type inverted-V-shaped tail wing control mechanism disclosed by the invention has the advantages of simple structure, strong reliability, high control efficiency and the like.