This invention belongs to the technical field of
aviation transponder pulse overlap
signal separation methods, specifically relating to a
separation method applicable to Mode A / C
aviation transponder pulse collision conditions. By analyzing the differential characteristics of the Mode A / C
aviation transponder signal waveform in the time and energy domains, the pulse collision
signal is effectively split. Based on the waveform definition characteristics of the Mode A / C aviation transponder signal, the pulse frame is accurately recovered from the separated signal, ultimately completing the
separation process of the Mode A / C collision pulse signal. This invention requires only a single-channel
receiver to achieve signal separation, reducing
system implementation costs and
engineering difficulty, effectively improving the
system monitoring capability in densely overlapping electromagnetic environments, and providing an efficient and engineered solution for transponder pulse signal separation tasks in scenarios such as air traffic surveillance and low-altitude airspace management.