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Satellite-borne TDI CMOS camera imaging simulation method and apparatus

A technology of camera imaging and simulation method, applied in the field of satellite imaging simulation, can solve the problem of less research on TDICMOS camera imaging simulation

Active Publication Date: 2017-12-08
自然资源部国土卫星遥感应用中心
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0008] In view of this, the embodiment of the present invention provides a method and device for imaging simulation of a spaceborne TDI CMOS camera, to solve the limitations of existing surveying and mapping remote sensing satellites using TDI CCD cameras, and there are few researches on imaging simulation of TDI CMOS cameras. question

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  • Satellite-borne TDI CMOS camera imaging simulation method and apparatus
  • Satellite-borne TDI CMOS camera imaging simulation method and apparatus
  • Satellite-borne TDI CMOS camera imaging simulation method and apparatus

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Embodiment 1

[0036] In this embodiment, a method for imaging simulation of a spaceborne TDI CMOS camera is provided, figure 1 It is a flow chart of the imaging simulation method for a spaceborne TDI CMOS camera according to an embodiment of the present invention, such as figure 1 As shown, the process includes the following steps:

[0037] S101: Simulate satellite orbit data and satellite attitude data; the satellite orbit data includes the scanning time, position, and velocity data of the satellite in the earth reference coordinate system, and describe the satellite orbit through the orbit six parameters in the celestial reference coordinate system: orbit height, orbit inclination , orbit eccentricity, argument of perigee, true anomaly, right ascension of ascending node, and satellite attitude data include pitch angle, roll angle and yaw angle of the satellite platform.

[0038] S102: According to the geometric parameters of the CMOS camera, satellite orbit data and satellite attitude da...

Embodiment 2

[0161] image 3 It is a schematic diagram of the hardware structure of the computer equipment of the satellite-borne TDI CMOS camera imaging simulation method according to the embodiment of the present invention, as image 3 As shown, the device includes one or more processors 310 and memory 320, image 3 A processor 310 is taken as an example.

[0162] The device for executing the imaging simulation method of the spaceborne TDI CMOS camera may also include: an input device 330 and an output device 340 .

[0163] The processor 310, the memory 320, the input device 330 and the output device 340 may be connected via a bus or in other ways, image 3 Take connection via bus as an example.

[0164] The processor 310 may be a central processing unit (Central Processing Unit, CPU). The processor 310 may also be other general-purpose processors, digital signal processors (Digital Signal Processor, DSP), application-specific integrated circuits (Application Specific Integrated Circ...

Embodiment 3

[0171] The embodiment of the present invention also provides a computer-readable storage medium, the computer-executable instruction is stored in the computer-executable instruction, and the computer-executable instruction can execute the imaging simulation method of the spaceborne TDI CMOS camera in any of the above method embodiments. Wherein, the storage medium may be a magnetic disk, an optical disk, a read-only memory (Read-Only Memory, ROM), a random access memory (Random Access Memory, RAM), a flash memory (Flash Memory), a hard disk (Hard Disk) Disk Drive, abbreviation: HDD) or solid-state drive (Solid-State Drive, SSD), etc.; the storage medium may also include a combination of the above-mentioned types of memory.

[0172] Those skilled in the art should understand that the embodiments of the present invention may be provided as methods, systems, or computer program products. Accordingly, the present invention can take the form of an entirely hardware embodiment, an e...

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Abstract

The present invention provides a satellite-borne TDI CMOS camera imaging simulation method and an apparatus. The method comprises the following steps that: the data source range of a CMOS instantaneous focal plane imaging area is obtained according to the geometric parameters of a CMOS camera and satellite attitude and orbit data; the surface reflectance of the imaging area and atmospheric transmission simulation parameters are obtained; an integration time interval is obtained according to image ground resolution, satellite orbit data and attitude data of each integration time point are obtained; a CMOS pixel is uniformly divided into a plurality of sub-pixels; the entrance pupil radiance images of the CMOS camera at each integration time point are obtained according to the above parameters; the entrance pupil radiance images of the CMOS camera are filtered, so that CMOS focal plane radiance images at each integration time point are obtained; the CMOS focal plane radiance images are converted into charge number images, and the charge number images at each integration time point are obtained; and integration delay accumulation is performed on the charge number images, and analog-to-digital conversion is performed, and therefore, a gray value image is obtained. With the satellite-borne TDI CMOS camera imaging simulation method and the apparatus of the invention adopted, limitations caused by a condition that an existing surveying and mapping remote sensing satellite adopts a TDI CCD camera can be eliminated; and the problem of few researches on the imaging simulation of the TDI CMOS camera can be solved.

Description

technical field [0001] The invention relates to the technical field of satellite imaging simulation, in particular to an imaging simulation method and equipment for a satellite-borne TDI CMOS camera. Background technique [0002] With the development of aerospace remote sensing technology, people have higher and higher requirements for the update frequency of remote sensing data. The temporal resolution of remote sensing images must reach one day or even several hours. However, large-platform satellites like Ziyuan-3 are not only costly, but also have limited maneuverability, making it difficult to meet the increasing image acquisition speed. Due to the low cost of small satellites equipped with CMOS imaging sensors, they can form satellite constellations and obtain images with hour-level time resolution, which is becoming a new trend in the field of space remote sensing. [0003] Compared with traditional CCD imaging sensors, CMOS sensors have the advantages of low power ...

Claims

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Application Information

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IPC IPC(8): G06T3/60G06T5/00G06F17/50
CPCG06T3/604G06F30/20G06T5/70
Inventor 高小明李国元陈继溢袁小棋刘诏陈乾福赵严铭
Owner 自然资源部国土卫星遥感应用中心
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