Quasi-generative unmanned aerial vehicle induction method and system
A drone and generative technology, applied in the field of satellite navigation, can solve problems such as unrealizable, drone navigation deception, etc., and achieve the effect of fast deception and good deception effect
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Embodiment 1
[0058] A specific embodiment of the present invention discloses a quasi-generated unmanned aerial vehicle guidance system, the 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 induced 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; for example, in this process, a high-performance satellite navigation receiver can be used to receive all satellite navigation signals in real time. The real navigation signal of the satellite can be seen, and the capture, tracking, ephemeris reception, positioning calculation, navigation information storage / output, and timing information acquisition of the real satellite navigation signal can be completed. Exemplarily, the signal receiving uni...
Embodiment 2
[0096] In Embodiment 2 of the present invention, a quasi-generated UAV induction method is also provided, the flow chart is as follows figure 2 As shown, the method includes the following steps:
[0097] Step S1: Receive and analyze the real satellite navigation signals of all visible satellites in real time, obtain the ephemeris information and timing information of all visible satellites; also obtain the current position of the target UAV in real time;
[0098] Step S2: Generate 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: Select the real satellite navigation signal of the visible satellite for delay, and generate a radio frequency signal based on the real satellite navigation signal of the selected visible satellite for delay;
[0100] Step S4: Use the pseudo-range delay to delay the radio frequency signal, and...
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