Electromagnetic hole guiding method and device for assembling aircraft skin and framework

The invention discloses an electromagnetic hole guiding method and device for assembling an aircraft skin and a framework. The problems that due to the fact that an existing hole guiding method and device are poor in universality, inconvenient to operate and multiple subjective judgment factors, hole guiding position calibration is not accurate, positioning deviation is likely to be generated, hole manufacturing cannot be effectively implemented in the working environment with poor openness, the hole manufacturing precision and efficiency are low, 8-shaped holes are extremely likely to be generated, the holes are out of tolerance, and the hole manufacturing cost is low are solved. And finally, the riveting quality of the airplane is seriously influenced, and the productivity is reduced. Under the condition that components of an aircraft are not damaged, the aircraft can penetrate through the properties of an aircraft framework and a skin within a certain range, and when two coils which are connected with curr