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Rocket-borne image acquisition and compression system suitable for sounding rocket

A technology for image acquisition and sounding rockets, which is applied in image communication, closed-circuit television systems, electrical components, etc. It can solve problems such as power supply and thermal control effects of rocket-borne systems, reduce design complexity, reduce costs, and enhance applicability Effect

Active Publication Date: 2014-01-15
NAT SPACE SCI CENT CAS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In addition, the power consumption of some space cameras reaches 10W or more, which has a certain impact on the power supply and thermal control of the entire rocket system.

Method used

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  • Rocket-borne image acquisition and compression system suitable for sounding rocket
  • Rocket-borne image acquisition and compression system suitable for sounding rocket
  • Rocket-borne image acquisition and compression system suitable for sounding rocket

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Embodiment Construction

[0037] In order to make the objectives, technical solutions, and advantages of the present invention clearer, the following further describes the present invention in detail with reference to the accompanying drawings and embodiments.

[0038] The purpose of the present invention is achieved as follows:

[0039] The sounding rocket image acquisition and compression system provided by the present invention includes:

[0040] Power management module 1, to provide power for each module in the entire system, through DC-DC conversion, output voltage of 3.3V, 2.5V, 1.8V, 1.2V, to supply power to other unit modules;

[0041] The arrow-mounted analog camera 2 is used to acquire images and generate analog image signals;

[0042] The image and video decoding unit 3 is used to digitize the image data of the analog camera and output 8-bit image data to the image compression unit;

[0043] The image compression unit 4 is used to perform wavelet transformation and compression on the digitized image da...

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PUM

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Abstract

The invention relates to a rocket-borne image acquisition and compression method and a system which are suitable for a sounding rocket. The system comprises a power supply management module, several rocket-borne simulation cameras, an image video decoding unit, an image compression unit, a central control unit, a data transmission unit and a watchdog unit, wherein the power supply management module provides power for the whole system; the image video decoding unit is used to carry out digitization on image data of the simulation cameras; the image compression unit is used to carry out wavelet transformation and compression on the image data; the central control unit is used to control the image compression unit and the image video decoding unit, switch among the plurality of cameras and pack and output the image data; the data transmission unit is used to complete buffer and transmission of the image data and convert parallel bus data into synchronous 422 bus data; the watchdog unit is used to monitor software of the whole system. The system is used for realizing image acquisition on the sounding rocket. The system possesses the characteristics that cost is low; power consumption is low; temperature adaptability is good and reliability is high.

Description

Technical field [0001] The invention relates to a rocket-borne image acquisition and compression system, in particular to a rocket-borne image acquisition and compression method and system suitable for sounding rockets. Background technique [0002] Sounding rocket is a kind of rocket for detection and scientific experiment in near-Earth space. Its flying altitude is between the sounding balloon and artificial satellite. It is also the only field detection method in the adjacent space (40~200 kilometers). It is other aircraft. Beyond reach. [0003] Sounding rockets are generally uncontrolled rockets, which have the advantages of simple structure, low cost, short development period, and flexible and convenient launch. It can not only detect the structure, composition and parameters of each layer of the atmosphere in the height direction, and realize the three-dimensional profile detection of the middle and upper atmosphere; it is more suitable for temporary observation of special ...

Claims

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Application Information

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IPC IPC(8): H04N19/63H04N7/18
Inventor 陈萍王林林姜秀杰陈志敏刘建斌李婷婷满峰刘成
Owner NAT SPACE SCI CENT CAS
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