The invention provides an anti-detection
camouflage method based on
missile-borne
tail end guidance features, and relates to the technical field of anti-detection
camouflage, and the method comprises the steps: constructing a
feature data set through the reflection feature parameters of
radar transmission
waves with different transmission features under different environment data, transmission angles and distances, and building a reflection feature calculation model; the method comprises the following steps: acquiring guided
missile tail end guidance features, performing preprocessing according to the emission angle, distance and
environmental data of guided
missile radar, predicting reflection feature parameters through a model, modulating
radar interference
waves with the same reflection feature parameters as the reflection feature parameters to generate an interference blind area with reflection
waves, and controlling the position and size of the interference blind area. Blind
area coverage is conducted on the position where the missile is located, the blinding index of the missile in the time period is calculated by calculating the moving trajectory fluctuation coefficient of the missile after interference and the change coefficient of a landing area, whether an
attack target is lost or not is judged, and whether a tempting
signal is released or not is selected.