A quasi-generative UAV induction method and system
A UAV, generative technology, applied in the field of satellite navigation, can solve the problems of UAV navigation deception, inability to achieve, etc., and achieve the effect of good decoy effect and fast deception speed.
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Embodiment 1
[0058] A specific embodiment of the present invention discloses a quasi-generative unmanned aerial vehicle inducing system. The schematic structural diagram is as follows: figure 1 As shown, the system includes: a signal receiving unit, a target tracking unit, a strategy generating unit, and an inducing signal generating unit; wherein,
[0059] The signal receiving unit is used to receive and analyze the real satellite navigation signals of all visible satellites, and obtain the ephemeris information and timing information of all visible satellites; The real navigation signals of satellites can be seen, and the acquisition, tracking, ephemeris reception, positioning calculation, navigation information storage / output, and timing information acquisition of real satellite navigation signals are completed. Exemplarily, the signal receiving unit can choose BDS / GPS / GLONASS / Galieo high-performance multi-mode combined receiver, which needs to have the function of outputting raw observ...
Embodiment 2
[0096] In Embodiment 2 of the present invention, a quasi-generative UAV induction method is also provided, and the flowchart is as follows figure 2 As shown, the method includes the following steps:
[0097] Step S1: receiving and analyzing real satellite navigation signals of all visible satellites in real time, obtaining ephemeris information and timing information of all visible satellites; also obtaining the current position of the target UAV in real time;
[0098] Step S2: generating a pseudo-range delay based on the ephemeris information of all visible satellites, the current position of the target drone and the expected position of the target drone at the next moment;
[0099] Step S3: selecting the real satellite navigation signals of the visible satellites to be delayed, and generating radio frequency signals based on the selected real satellite navigation signals of the visible satellites that are delayed;
[0100] Step S4: delay the radio frequency signal by using...
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