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Ultrafast recovery method and system for twin image of pneumatic optical effect target

An aero-optics and image technology, applied in image enhancement, image data processing, instruments, etc., can solve the problems of large amount of calculation, complexity, time-consuming, etc., and achieve the effect of ensuring accuracy

Active Publication Date: 2021-12-14
WUHAN INSTITUTE OF TECHNOLOGY
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Problems solved by technology

However, due to the complexity of its algorithm design, large amount of calculation, and long time consumption, it is difficult to meet the requirements of fast processing, especially for high-speed aircraft, real-time performance is very important

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  • Ultrafast recovery method and system for twin image of pneumatic optical effect target
  • Ultrafast recovery method and system for twin image of pneumatic optical effect target
  • Ultrafast recovery method and system for twin image of pneumatic optical effect target

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Embodiment Construction

[0042] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0043] The ultra-fast restoration method of the twin image of the aero-optical effect target in the embodiment of the present invention adopts C++ and MFC to build the system on the windows10 platform. It can be understood that the algorithm of the present invention can also be transplanted to other programming languages ​​or hardware devices.

[0044] Such as figure 1 , 2 As shown, the ultrafast recovery method of the aero-optical effect target twin image in the embodiment of the present invention includes the following steps:

[0045] S1. In the high-speed flow field, quickly generate two fram...

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Abstract

The invention discloses an ultrafast restoration method for a target twin image based on an aerodynamic optical effect, and the method comprises the following steps: S1, rapidly generating two frames of target twin images through a camera in a high-speed flow field; S2, carrying out fast discrete Fourier transform on the two frames of target twin images, and establishing image turbulence fuzzy degradation models respectively; S3, merging and calculating the two image turbulence fuzzy degradation models, eliminating the same noise item and the same item in the degradation model, adding a non-negative constraint item and a spatial correlation constraint item, and solving to obtain a fuzzy kernel of each frame of target twin image; S4, respectively carrying out differential continuous continuation on the boundaries of the two frames of target twin images, and inhibiting a boundary ringing effect; S5, according to the solved blurring kernel, carrying out the restoration of two frames of target twin images through a fast non-blind deconvolution method of super-Laplacian prior; and S6, normalizing the restored images to obtain clear images. According to the method, ultrafast restoration can be carried out on the aerodynamic optical effect degraded image with the target twin image.

Description

technical field [0001] The invention belongs to the fields of aero-optical effect correction and image processing, and in particular relates to an ultra-fast recovery method for a twin image of an aero-optic effect target. Background technique [0002] When a high-speed aircraft flies in the atmosphere at high speed, due to the relative motion and interaction with the surrounding air, the aerodynamic flow field is generated, which seriously degrades the function of the aircraft's optical imaging detection system. The physical process and phenomenon is called the aero-optical effect. Due to the complexity of the environment, the imaging system will be disturbed by the aero-optic effect, resulting in turbulent degradation of the acquired image, which will affect the recognition and tracking of the target. The high-speed movement of the aircraft leaves a shorter time interval for the completion of detection processing, which poses a severe challenge to the limited processing ca...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06T5/00
CPCG06T5/73
Inventor 洪汉玉雷金磊张耀宗章秀华吴锦梦张天序
Owner WUHAN INSTITUTE OF TECHNOLOGY
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