Infrared vision based automatic landing guidance method and system applied to fixed-wing UAV (unmanned aerial vehicle)
A technology for automatic landing and unmanned aerial vehicles, which is applied in the direction of aircraft automatic landing aids, aircraft landers, traffic control systems, etc., can solve the problem of insufficient performance of image processors, fast speed of fixed-wing unmanned aerial vehicles, and increased weight of unmanned aerial vehicles and other problems, to achieve the effects of eliminating the influence of visible light, good real-time performance, and reducing the difficulty of recognition
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[0036] Embodiments of the present invention are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention.
[0037] The automatic landing guidance system of the present invention is made up of two identical image tracking modules, an image processing module, a control module, and a wireless transmission module, wherein the image tracking module is composed of a camera and a high-precision two-axis pan-tilt (PTU) and is placed on the runway respectively On both sides, the camera is installed on the top of the two-axis gimbal, such as figure 1 As shown, the UAV is detected, identified and tracked in the image using image tracking technology, and the...
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