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Satellite space selfie device

A Selfie device and satellite technology, applied in radio transmission systems, closed-circuit television systems, electrical components, etc., can solve the problems of low display screen utilization rate and single screen form, and achieve the effect of improving screen utilization rate and enriching content

Inactive Publication Date: 2018-05-18
CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Based on this, it is necessary to provide a satellite space Selfie device for the problems of single image form and low utilization rate of the display screen in the ground control center when using an external camera to take selfies of rockets or spacecraft.

Method used

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Embodiment Construction

[0016] The technical solutions of the present invention will be described in detail below in conjunction with the accompanying drawings and preferred embodiments.

[0017] In one of the examples, as Figure 1-3 As shown, the satellite space selfie device includes a folding bracket 3, a high-definition camera unit and an image display unit 2, one end of the folding bracket 3 is fixedly connected to the satellite 1, and the other end is fixedly connected to the high-definition camera unit; the image display unit 2 is used to display the satellite 1 The image data recorded by the external camera or the image data stored in advance, the image display unit 2 is fixedly connected to the satellite 1, and the image display unit 2 and the high-definition camera unit are located on the same side of the satellite 1; when the satellite 1 enters orbit, the satellite 1 Control the folding bracket 3 to expand from the folded state, and control the high-definition camera unit to take self-por...

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Abstract

The invention relates to a satellite space selfie device, and belongs to the technical field of photoelectronic imaging. The satellite space selfie device comprises a folding bracket, a high-definition image pickup unit and an image display unit; one end of the folding bracket is fixedly connected with a satellite, and the other end of the folding bracket is fixedly connected with the high-definition image pickup unit; the image display unit is used for displaying image data shot and recorded by an external camera of the satellite or pre-stored image data, the image display unit is fixedly connected with the satellite, and the image display unit and the high-definition image pickup unit are positioned on the same side of the satellite; and when the satellite enters an orbit, the satellitecontrols the folding bracket to be expanded from a folding state and controls the high-definition image pickup unit to carry out selfie image pickup on the satellite and the image display unit to obtain a satellite selfie image comprising an image displayed by the image display unit. According to the satellite space selfie device disclosed by the invention, contents of the satellite selfie image are further enriched, and when a display is utilized to carry out observation on a ground control center, an image utilization rate of the display is improved.

Description

technical field [0001] The invention relates to the technical field of photoelectric imaging, in particular to a satellite space selfie device. Background technique [0002] At present, there are external cameras installed on rockets and spacecraft to take selfies. This external camera is mostly used to monitor the status of the rocket and the docking of the spacecraft and other activities. The pictures it takes are fixed and only for special tasks. The ground control center can only observe the picture of a certain fixed position through an external camera, and the form is single, and the utilization rate of the display screen of the ground control center is not high. Contents of the invention [0003] Based on this, it is necessary to provide a satellite space Selfie device for the problem that the self-portrait of a rocket or spacecraft by an external camera is single and the utilization rate of the display screen of the ground control center is not high. [0004] In o...

Claims

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Application Information

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IPC IPC(8): H04N7/18H04B7/185F16M11/26F16M13/02
Inventor 谢晓光王旻徐伟常琳杨秀彬金光
Owner CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI