Satellite navigation regenerative deception generation method based on correlation peak dynamic dragging
A technology of satellite navigation and generation method, which is applied in the field of satellite navigation to achieve the effects of low transmission power, low environmental dependence, and simple engineering implementation.
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[0024] The technical solutions of the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.
[0025] A method for generating satellite navigation regenerative deception based on dynamic dragging of correlation peaks, comprising the following steps:
[0026] (1) On the basis of traditional spoofing interference generation methods, the function of receiving space satellite navigation signals is added to obtain satellite signal information in the spoofing interference area, including the visible satellite number, spatial position, signal power, and signal Doppler in the spoofing area Observation parameters of space visible satellites such as pseudo-code phase and message parameters;
[0027] (2) By receiving the space navigation satellites in the deception area, extract the signal feature monitoring two-dimensional matrix of the real space navigation satellites in the current deceitful airspace, coverin...
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