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Remote data management system based on carrier rocket

A carrier rocket and remote data technology, applied in the field of remote data management system, to achieve efficient data query and analysis and comparison, and improve utilization

Pending Publication Date: 2021-08-10
SHANGHAI AEROSPACE SYST ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, there is no unified platform or system that can realize big data management of remote data of launch vehicles in terms of remote data access, unified data storage, data retrieval and query, and analysis applications.

Method used

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  • Remote data management system based on carrier rocket
  • Remote data management system based on carrier rocket
  • Remote data management system based on carrier rocket

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Experimental program
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Embodiment Construction

[0026] The present invention will be further elaborated below in conjunction with embodiment.

[0027] The invention provides a remote data management system based on a launch vehicle, which is realized by using big data computing and storage technology, adopts a distributed architecture design, follows the principle of layered and modular design, and has background service functions such as collection, analysis, calculation, and query etc. are designed with a micro-service architecture, and the visualization module is also designed in a componentized manner to support linear expansion and subsequent capacity expansion.

[0028] Remote data management methods based on launch vehicles, such as figure 1 As shown, it specifically includes a data collection and processing module, a structured data storage module, a multimedia data storage module and a client;

[0029] Data acquisition and processing module: receive the test data of the launch vehicle; send the test data with time...

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Abstract

The invention relates to a remote data management system based on a carrier rocket, and belongs to the field of data management design. The system includes a data acquisition and processing module, a structured data storage module, a multimedia data storage module and a user side, wherein the data acquisition and processing module is used for sending the test data with the time scale to the structured data storage module, sending the test data without the time scale to a multimedia data storage module; the structured data storage module and the multimedia data storage module are used for compressing and storing the test data with the time scale and marking an ID (Identity), encrypting the storage data packet corresponding to the ID, and sending the encrypted storage data packet to the user side; the user side sends a calling instruction, receives the encrypted storage data packet, and checks the data after decryption and decompression. According to the system, the difficult problems of massive heterogeneous time sequence carrier rocket remote data in the aspects of storage, retrieval, comparison, analysis, data service and the like are solved, and the utilization rate of the carrier rocket remote data is greatly improved.

Description

technical field [0001] The invention belongs to the field of data management design and relates to a remote data management system based on a carrier rocket. Background technique [0002] The structure of the launch vehicle is complex, and a large amount of high-dimensional and diverse heterogeneous data with time-series characteristics will be generated in the stages of development, testing, and flight. These data are very valuable. Launch vehicle developers can use these data to conduct various data research and judgment to find launch vehicle problems and defects, optimize launch vehicle design schemes, and improve launch vehicle manufacturing processes. However, due to the huge amount of data, large differences in data structure, and high real-time data, general database and data management methods cannot effectively manage and rationally utilize these data. [0003] Remote testing of launch vehicles often comes from different subsystems, monitoring systems or manual in...

Claims

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Application Information

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IPC IPC(8): G06F16/22G06F16/41G06F21/60
CPCG06F16/22G06F16/41G06F21/602
Inventor 颜晓明张元明黄兴朱亚明王良军姚迪
Owner SHANGHAI AEROSPACE SYST ENG INST