The invention relates to the technical field of
aviation safety, and provides a
laser radar trailing vortex inversion method,
system and device, a product and a medium. The method comprises the following steps: acquiring meteorological parameters,
model parameters and ADS-B data, and calculating trailing vortex circular rector; constructing an axial scanning coordinate
system; constructing a first radial speed
algorithm; background
wind speed is calculated through a first radial speed
algorithm; constructing a second radial speed
algorithm through the background
wind speed and the first radial speed algorithm; determining a
range gate, obtaining a corresponding detection point coordinate pair, and traversing gradient absolute values of the detection point coordinate pair in the detection
point set to obtain a relative vortex core position; and obtaining a first real vortex core position, a second real vortex core position and a distance between the two positions in an area where the relative vortex core position is located, and iterating to the distance convergence between the two positions to determine a real vortex core position. According to the method, interference of background wind is effectively eliminated, and
airplane wake flow axial scanning based on the
laser radar is realized by calculating the real vortex core position.