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Satellite-borne ultra-miniature monitoring camera

An ultra-miniature, camera technology, applied in the direction of TV, color TV, color TV components, etc., can solve the problems of high cost, high power consumption, large size of surveillance cameras, etc., to reduce power consumption, reduce size, improve The effect of reliability

Active Publication Date: 2021-11-16
CHANGCHUN UNIV OF SCI & TECH +2
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Due to technical reasons, most of the existing spaceborne surveillance cameras use fixed-focus lenses and large area array CMOS image sensors. This type of surveillance camera is large in size, high in power consumption, and high in cost, and is not suitable for use on micro-nano satellites and pico-satellites. However, the miniature cameras used on the ground have poor environmental, mechanical and anti-radiation performance, and are not suitable for use on spaceborne cameras.

Method used

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  • Satellite-borne ultra-miniature monitoring camera
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  • Satellite-borne ultra-miniature monitoring camera

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Embodiment Construction

[0022] The present invention will be described in further detail below in conjunction with the accompanying drawings.

[0023] combined with figure 1 , a space-borne ultra-miniature surveillance camera, including anti-radiation glass assembly, auto-focus voice coil motor lens 4, focal plane module, signal processing module, interface circuit module, special rigid-flexible integrated circuit board and camera structure 10.

[0024] The special rigid-flex circuit board consists of 6 parts: rigid board 1, rigid board 2, rigid board 3, flexible connection 1 and flexible connection 2. The focal plane circuit board is designed on the rigid board 1 , the signal processing module is designed on the rigid board 2 , and the interface circuit module is designed on the rigid board 3 . The flexible connection 1 is used to connect the rigid board 1 and the rigid board 2, and transmit the data output by the image sensor to the signal processing circuit on the rigid board 2. The flexible con...

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Abstract

The invention discloses a satellite-borne ultra-miniature monitoring camera, and the camera comprises a camera shell; a camera structural member is installed in the camera shell, a specially-made rigid-flexible integrated circuit board is installed and fixed in the camera structural member through a second screw, and a focal plane module, a signal processing module and an interface circuit module are installed on the specially-made rigid-flexible integrated circuit board; an automatic focusing voice coil motor lens is installed at one end of the special rigid-flexible integrated circuit board, and the automatic focusing voice coil motor lens is covered with an anti-radiation glass assembly. The invention has the advantages of simple structure, small volume, low power consumption, low cost and short production period, and has a certain anti-radiation function.

Description

technical field [0001] The invention relates to the technical field of surveillance cameras, in particular to a space-borne ultra-miniature surveillance camera. Background technique [0002] In recent years, with the development of the commercial aerospace industry, the launch of ultra-small satellites such as micro-nano satellites and pico-satellites has sprung up. On-board surveillance cameras put forward new technical requirements. [0003] Due to technical reasons, most of the existing spaceborne surveillance cameras use fixed-focus lenses and large area array CMOS image sensors. This type of surveillance camera is large in size, high in power consumption, and high in cost, and is not suitable for use on micro-nano satellites and pico-satellites. However, the miniature cameras used on the ground have poor environmental, mechanical and anti-radiation performance, and are not suitable for use on spaceborne cameras. Contents of the invention [0004] In order to solve t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H04N5/225
CPCH04N23/52H04N23/50H04N23/55Y02E30/30
Inventor 陈磊刘颖邹昕胡永富赵爽张保贵韩承志张原野吴建福
Owner CHANGCHUN UNIV OF SCI & TECH
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