Image data transmission circuit of satellite-borne high-resolution CCD (Charge Coupled Device) camera

A high-resolution, image data technology, applied in the field of aerospace optical remote sensing imaging, can solve the problems of large phase deviation of output signals of multiple differential driver integrated circuits, inaccurate positioning of data clocks, and performance degradation of data transmission circuits. The effect of miniaturization, prevention of influence, and volume reduction

Inactive Publication Date: 2011-08-17
CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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Problems solved by technology

[0003] The invention solves the problem that the single-channel image data transmission of the existing space-borne CCD remote sensing camera requires the cooperation of multiple differential driver integrated circuits, resulting in large phase deviations in the output signals of the multi-chip di

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  • Image data transmission circuit of satellite-borne high-resolution CCD (Charge Coupled Device) camera
  • Image data transmission circuit of satellite-borne high-resolution CCD (Charge Coupled Device) camera
  • Image data transmission circuit of satellite-borne high-resolution CCD (Charge Coupled Device) camera

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Example Embodiment

[0011] Specific implementation mode one, combination figure 2 with image 3 To explain this embodiment, the image data transmission circuit of a satellite-borne high-resolution CCD camera includes a high-speed serial differential transmission circuit and a high-speed serial differential receiving circuit; it is characterized in that the high-speed serial differential transmission circuit receives the satellite-borne high-resolution The parallel image data, line synchronization signal, and data clock signal output by the CCD camera, the parallel image data and line synchronization signal are converted into three sets of data LVDS signal streams in one clock cycle by a high-speed serial differential transmission circuit; the data clock signal The LVDS signal stream is converted into a clock by the high-speed serial differential transmission circuit and sent in the fourth group of LVDS signal streams, and the four groups of LVDS signal streams are transmitted to the high-speed seri...

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Abstract

The invention provides an image data transmission circuit of a satellite-borne high-resolution CCD (Charge Coupled Device) camera, relating to the technical field of aerospace optical remotely-sensed imaging technology and solving the problem that the performance of the data transmission circuit is reduced after data transmission because the transmission of image data of a single channel of the traditional satellite-borne CCD remote sensing camera needs coordination of a plurality of differential driver integrated circuits. The image data transmission circuit comprises a high-speed serial differential transmitting circuit at a transmitting end and a high-speed serial differential receiving circuit at a receiving end. The high-speed serial differential transmitting circuit receives image data, line synthesizing signals and data clock output by a satellite-borne high-resolution CCD; the image data, the line synthesizing signals and the data clock are subjected to parallel-serial conversion and differential driving through a high-speed LVDS (Low Voltage Differential Signaling) serializer to output four groups of high-speed serial LVDS signals; and the four groups of LVDS signal flows are transmitted to the high-speed serial differential receiving circuit through an LVDS transmission cable. By means of the image data transmission circuit provided by the invention, the size, the weight and the power consumption of a data transmission link of the satellite-borne high-resolution CCD camera are reduced, and the quality of image transmission is effectively ensured.

Description

technical field [0001] The invention relates to the technical field of aerospace optical remote sensing imaging, in particular to an image data transmission circuit of a spaceborne high-resolution CCD camera. Background technique [0002] With the development of aerospace optical remote sensing imaging technology, the requirements for the ground pixel resolution and width of space-borne CCD remote sensing cameras are constantly increasing. In order to meet the requirements, most space-borne high-resolution CCD remote sensing cameras use high-speed multi-channel parallel output structure. "High speed" is due to the high readout frequency of CCD pixels due to high resolution, resulting in high data rate image data; "multi-channel" contains two meanings: one is to use multiple CCDs to meet the ground width of the camera Splicing; the second is to ensure the complete transfer and output of the signal charge, the CCD uses multiple taps to output in parallel. This will inevitabl...

Claims

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Application Information

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IPC IPC(8): H04N5/372H04N5/357
Inventor 张贵祥金光
Owner CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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