Real-time collection system for three-dimensional ice type of icing on surface of aircraft wing

The invention relates to the field of aircraft safety monitoring. The invention provides a real-time collection system for a three-dimensional ice type of icing on the surface of an aircraft wing. The system is characterized by comprising a CCD camera group installed on the inner side of an aircraft porthole; a light source system comprises a detection light source mounted on the inner side of an aircraft porthole and an auxiliary light source mounted on the inner side of a winglet; a plurality of marks are arranged on the surface of the wing to form a three-dimensional reconstructed spatial position reference; a delay pulse generator is mounted in the aircraft; a computer; the delay pulse generator is connected with the CCD camera group and sends out a pulse control signal, so that the CCD camera group can shoot synchronously; the computer is connected with the CCD camera, the delay pulse generator and the light source system, and is used for controlling on-off of the light source and operation of the delay