A method and system for UAV induction based on location spoofing
A UAV, current location technology, applied in the field of satellite navigation, can solve problems such as unrealization and UAV navigation deception, and achieve the effect of fast induction speed and good induction effect.
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Embodiment 1
[0072] A specific embodiment of the present invention discloses a position spoofing-based UAV induction system. The schematic diagram is as follows: figure 1 As shown, the system includes: a satellite navigation signal real-time receiving unit, a target tracking unit, a strategy generating unit, and an inducing signal generating unit; wherein,
[0073] The satellite navigation signal real-time receiving unit is used to receive and analyze the real satellite navigation signals of all visible satellites, and obtain the ephemeris information of all visible satellites; exemplarily, in this process, a high-performance satellite navigation receiver can be used to receive all the satellite navigation signals in real time. The real navigation signal of the satellite can be seen, and the acquisition, tracking, ephemeris reception, positioning calculation and navigation information storage / output of the real satellite navigation signal are completed. Exemplarily, the satellite navigatio...
Embodiment 2
[0122] In Embodiment 2 of the present invention, a method for inducing drones based on location spoofing is also provided. The flowchart is as follows: figure 2 As shown, the method includes the following steps:
[0123] Step S1: Receive and analyze the real satellite navigation signals of all visible satellites in real time, and obtain the ephemeris information of all visible satellites; also obtain the current position of the target UAV in real time;
[0124] 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;
[0125] Step S3: selecting and separating the real satellite navigation signals of the visible satellites that are delayed;
[0126] Step S4: delaying the separated real satellite navigation signal by using the pseudorange delay, and enhancing the power of the delayed real navigation satellite signal to generate ...
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