Universal inertial data processing system based on uniform interface

A data processing system and processing system technology, applied in the field of inertial group test equipment, can solve the problems of incomplete function, poor versatility of pulse test equipment, inconvenient portability, etc., and achieve configurable sampling time, fast read and write speed, and high security Effect

Active Publication Date: 2017-05-10
HUBEI SANJIANG AEROSPACE HONGFENG CONTROL
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  • Abstract
  • Description
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  • Application Information

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Problems solved by technology

[0011] In view of the above defects or improvement needs of the prior art, the present invention provides an inertial group data processing system based on a unified interface, by integrating the data processing unit, measurement

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  • Universal inertial data processing system based on uniform interface
  • Universal inertial data processing system based on uniform interface
  • Universal inertial data processing system based on uniform interface

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[0041] 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. It should be understood that the specific embodiments described herein are only used to explain the present invention, but not to limit the present invention. In addition, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not conflict with each other.

[0042] The scheme adopted by the present invention is: a common data acquisition system based on a unified interface. The core circuit adopts dual-core STM32 control circuit, and the peripheral interface circuit includes pulse acquisition circuit, synchronous serial communication interface circuit, 1553B bus communication interface circuit, platinum resistance temperature measurement circuit, RS422 bus...

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Abstract

The invention discloses a universal inertial data processing system based on a uniform interface. The universal inertial data treatment system based on the uniform interface is characterized in that the data processing system comprises a pulse collection circuit, a communication interface circuit, a main control chip set, a data processing unit and a power source board, wherein the pulse collection circuit is used for collecting inertial positive and negative channel pulse output; the communication interface circuit achieves inertial data collection which is output by the inertial unit in a bus communication mode; a platinum resistance temperature measuring circuit measures compensating parameters which are needed when inertial precision is calculated, the main control chip set comprises a main processor and a subsidiary processor, communication interfaces with multiple types are extended through the main control chip set, and protocol conversion is conducted in software; the data treatment unit receives data transmitted by the main control chip set and achieves and conducts treatment. According to the universal inertial data processing system based on the uniform interface, multiple inertial test interfaces are integrated, multi-interface inertial data is unified into Ethernet output, multiple communication protocols are compatible, and multiple types of inertial test requirements are met.

Description

technical field [0001] The invention belongs to the field of inertial group test equipment, and more specifically relates to a general-purpose inertial group data processing system based on a unified interface, which is suitable for direct pulse output, general synchronous output, asynchronous serial port output, CAN bus output, 1553B bus output, etc. Data acquisition and processing of most inertial groups. Background technique [0002] The inertial measurement combination (hereinafter referred to as "inertial group") is the core component of the missile control system. After the inertial group is loaded, it is fastened in the instrument compartment of the missile with screws, and is directly sensitive to the flight attitude and running speed of the missile body. Therefore, the inertial group Accuracy and stability directly affect the flight accuracy of the missile. [0003] The inertial group tester is an important part of the inertial group test system. The function of t...

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Application Information

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IPC IPC(8): G06F13/38G06F13/42H04L29/06H04Q1/02
CPCG06F13/382G06F13/42H04L69/08H04Q1/028
Inventor 刘江龙邹力邓世恒刘文军李正睿张梦竹
Owner HUBEI SANJIANG AEROSPACE HONGFENG CONTROL
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