The invention provides a satellite navigation regenerative deception generation method based on correlation peak dynamic dragging, and belongs to the field of satellite navigation. According to the method, on the basis of traditional regenerative deception simulation, complete coherence of deception interference with real signals in technical indexes such as signal power, signal Doppler, arrival time delay and the like is achieved by receiving space real signals, a traditional anti-deception method cannot recognize the technical indexes, and the deception success rate is high; in the whole regenerative deception generation process, a navigation receiver is switched to a deception signal in a non-inductive mode through a correlation peak dragging mode from a space real signal, the deception belongs to dexterous deception, and the deception efficiency is high; the deception method does not need additional environment support and external auxiliary information, and deception is realized only in a smart control mode on deception interference generation; and the method is low in transmitting power, high in concealment, simple in engineering implementation and wide in application range, and has good popularization and application values.