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Spaceborne radar data processing and controlling device based on VPX bus

A control device and data processing technology, which is applied in electrical digital data processing, architecture with a single central processing unit, digital computer components, etc. Harsh, spaceborne radar data processing point track processing capability is high

Active Publication Date: 2017-03-15
CHINA ELECTRONIC TECH GRP CORP NO 38 RES INST
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AI Technical Summary

Problems solved by technology

[0004] Aiming at the current spaceborne radar data processing requirements, the present invention proposes a spaceborne radar data processing and control device based on the VPX bus to solve the problem of high track processing capability of spaceborne radar data processing points, coordinate transformation and point trace of radar intelligence data. Coarse correlation with track, point track and temporary track correlation, track correlation, point track fusion and track filtering and prediction processing time are short, and the aerospace environment is harsh

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  • Spaceborne radar data processing and controlling device based on VPX bus
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  • Spaceborne radar data processing and controlling device based on VPX bus

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Embodiment Construction

[0023] 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.

[0024] The spaceborne radar data processing and control device based on the VPX bus of the present invention belongs to a configurable spaceborne radar data processing and control system device, which can solve the problem of high track processing capabilities of spaceborne radar data processing points and harsh aerospace use environments. requirements. The present invention will be described in further detail below in conjunction with the accompanying drawings and embodiments.

[0025] like figure 1 As shown, the spaceborne radar data processing and control device adopts the standard VPX chassis...

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Abstract

The invention discloses a spaceborne radar data processing and controlling device based on a VPX bus. Two identical processing computers are adopted for a data processing system and a controlling system, and each processing computer comprises two isomorphic PowerPC 440 cores. The two systems form two working modes through the four isomorphic PowerPC 440 cores. According to the parallel mode, the four isomorphic PowerPC 440 cores independently work, but interconnection channels are formed between the four isomorphic PowerPC 440 cores through interconnection communication buses. According to the fault-tolerance mode, the four isomorphic PowerPC 440 cores carry out fault tolerance in a four-mode redundancy mode. The device aims at achieving the purposes of high spaceborne radar data processing point flight path processing capacity, coordinate transformation of radar information data, trace point and flight path rough correlation, trace point and temporary flight path correlation, flight path correlation, trace point fusion and flight path filtering, and short prediction processing time and solving the problem that the spaceflight use environment is severe.

Description

technical field [0001] The invention relates to a data processing and control device in the field of spaceborne radar, in particular to a data processing and control device for spaceborne radar based on a VPX bus. Background technique [0002] The functions of the radar data processing and control system mainly include: (1) data processing, including target point track preprocessing, target automatic start, track correlation and tracking processing, track state maintenance, etc.; (2) system control, including Radar beam resource planning and scheduling control, radar working mode management, communication between radar and satellite digital control computer or ground system, whole machine BIT and other tasks. [0003] According to the requirements of data processing performance analysis and the needs of radar control, the domestically produced BM3803FMGRH with the highest performance and aerospace experience does not meet the needs of this stand-alone machine. The hardware ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F15/173G06F15/78
Inventor 宣浩李琳陈之涛段晓超肖文光张宏财许大进李化雷
Owner CHINA ELECTRONIC TECH GRP CORP NO 38 RES INST
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