Embedded guiding star processing system

A processing system and embedded technology, applied in image data processing, general control system, control/adjustment system, etc., can solve problems such as the difficulty of guiding stars and the inability to observe space targets in the main field of view, and achieve good universality and strong Image processing and computational analysis capabilities, the effect of improving stability and accuracy

Active Publication Date: 2019-07-09
中国科学院国家天文台长春人造卫星观测站
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Problems solved by technology

[0007] The present invention provides an embedded guide star processing system to solve the problems that the existing image acquisition and processing system is difficult to cope with the huge amount of real-time data, the guide star is difficult, and the main field of view cannot observe the space target for a long time.

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  • Embedded guiding star processing system

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specific Embodiment approach 1

[0040] Specific implementation mode 1. Combination Figure 1 to Figure 5 Description of this embodiment, the embedded guide star processing system includes an image acquisition module and a guide star calculation module. The guide star calculation module adopts a guide star processing system with FPGA and DSP heterogeneous processor architecture. The camera video signal is collected in real time and stored in DDR3 SDRAM, and then the image data in DDR3 SDRAM is transmitted to the guide star calculation module;

[0041] In the present embodiment, described image acquisition module has image acquisition and transmission function, and it is based on FPGA as platform, adopts Kintex-7 XC7K325T of Xilinx company as control core, based on PCI Express bus architecture, can realize the high-speed transmission of optical fiber network image data collection function. The function of image acquisition and transmission uses optical fiber to complete the acquisition and transmission of sCM...

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Abstract

The invention discloses an embedded guiding star processing system, relates to a space target guiding star-oriented embedded processing system, and aims at solving the problem that the existing imageacquisition and processing systems are difficult to answer huge real-time data size and difficult to guide stars so that the main visual fields cannot observe space targets for a long time. The systemcomprises an image acquisition module and a guiding star calculation module, wherein the guiding star calculation module adopts a guiding star processing system constructed by FPGA and DSP heterogeneous processors; the image acquisition module acquires video signals of an sCMOS camera in real time and stores the video signals to a DDR3 SDRAM; and the image data in the DDR3 SDRAM is transmitted tothe guiding star calculation module. According to the system, strong image processing and calculation analysis abilities are provided, space targets can be recognized and accurate mass center positions of the space targets can be obtained, the calculated error vectors are converted into practical miss distances of telescopes, and the practical miss distances are fed back to pointing control systems of the astronomical telescopes. The embedded guiding star processing system is capable of improving the stability and accuracy of the guiding stars and achieving the long-time observation for the targets.

Description

technical field [0001] The invention relates to an embedded processing system for space target guide stars. Background technique [0002] For the precise observation of space targets, if the main field of view of the telescope is relatively small, and the space target prediction error is large, the target cannot enter and stabilize in the main field of view. At this time, a large field of view guide star telescope is needed to image a large range of airspace, search for targets, and guide the targets into the main field of view. [0003] Therefore, the guide mirror is a telescope attached to the main telescope barrel to monitor space targets. It plays the role of the main telescope to accurately track the space target. Once the space target in the field of view deviates from the correct position, it can be corrected by the driving device of the telescope. [0004] According to the target forecast file, the program tracking method is adopted to guide the telescope to track ...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B19/042G06T7/11G06T7/136G06T7/194H04N5/374H04N7/22H04N5/765
CPCG05B19/0423G06T7/11G06T7/136G06T7/194H04N7/22H04N5/765G05B2219/24215H04N25/76
Inventor 杨文波康喆吕游
Owner 中国科学院国家天文台长春人造卫星观测站
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