Space target identification method based on main focus large-field-of-view photoelectric telescope
A technology for optoelectronic telescopes and space targets, used in scene recognition, character and pattern recognition, image data processing, etc., can solve problems such as difficulty in closed-loop tracking, large real-time data volume, and inability to observe space targets, and achieve the goal of improving the degree of observation automation. Effect
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specific Embodiment approach 1
[0045] Specific implementation mode 1. Combination Figure 1 to Figure 3 In this embodiment, the space target recognition method based on the main focus large-field photoelectric telescope is described, and the method includes the extrapolation of the servo state of the telescope and image processing and analysis. Achieved by the following steps:
[0046] 1. Extrapolation of the servo state of the telescope;
[0047] Since the catalog information of the angle and time when the space target transits is predicted, the program tracking method (that is, the open-loop tracking method) can be used to guide the telescope to observe.
[0048] The so-called program tracking party first uses the two-line root number to calculate the azimuth and altitude angle data required for the telescope to align with the space target, and then these data are loaded on the servo platform of the telescope to drive the telescope to move.
[0049] For space targets in low-Earth orbit, the time interval ...
specific Embodiment approach 2
[0099] Specific embodiment two, combine Figure 4 Describe this embodiment, this embodiment is the embodiment of the space object recognition method based on the main focus large field of view photoelectric telescope described in the specific embodiment one:
[0100] Telescope platform: 1.2m main focus large field of view photoelectric telescope;
[0101] Target number: 33105;
[0102]Observation time: January 17, 2019;
[0103] Data composition: a total of 24 frames of data;
[0104] Calculation results: All 24 frames of images have recognized space targets.
[0105] In this embodiment, the target number 33105 is the JASON2 satellite, which is a marine terrain satellite jointly developed by CNES and NASA, with a perigee altitude of 1305km, an apogee altitude of 1317km, and an orbital inclination of 66.04°. Since this satellite is a laser star, the astronomical positioning of the identified space target can be carried out, and the data and the data of the CPF (consolidated...
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