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Test-launch-control remote data transmission system

A data transmission system and long-distance technology, which is applied in the field of aerospace measurement, launch and control, can solve the problems of various types of equipment and complex transmission links of the data transmission system, and achieve the effect of reducing purchase costs and multiple protocol conversion links

Active Publication Date: 2014-12-17
BEIJING AEROSPACE AUTOMATIC CONTROL RES INST +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Since the existing long-distance measurement, launch and control system data transmission system has shortcomings such as complex transmission links and many types of equipment, it is necessary to improve it to reduce the cost of additional software and hardware design while achieving reliable and efficient data transmission.

Method used

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Embodiment Construction

[0023] Specific embodiments of the present invention will be further described in detail below in conjunction with the accompanying drawings.

[0024] Such as figure 1 As shown, the present invention provides a long-distance data transmission system for measuring, sending and controlling, including: a back-end PLC combination, a central computer, a virtual display computer, an instruction input module, a front-end PLC combination, a front-end power supply and a relay module;

[0025] Such as figure 2 As shown, the back-end PLC combination includes a back-end CPU module, a back-end power supply module, a switch module, an Ethernet communication module, a first Controller Link module and a second Controller Link module;

[0026] As the control core of the back-end PLC combination, the back-end CPU module processes the data of the switch module, the Ethernet communication module, the first Controller Link module and the second Controller Link module;

[0027] The back-end powe...

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PUM

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Abstract

A test-launch-control remote data transmission system is used for remote data communication in an aerospace test-launch-control system. The test-launch-control remote data transmission system comprises a front end and a rear end connected through optical fibers. The rear end is composed of a rear-end PLC (programmable logic controller) set, a central computer, a virtual display computer and a command input module. The rear-end PLC set allows remote communication with the front end, which is a test-launch-control front end, receives switching signals from the central computer and the command input module and feeds status information acquired by the rear-end PLC set back to the virtual display computer for displaying. The front end is composed of a front-end PLC set; on one hand, the front end is used for receiving control commands from the rear-end PLC set and controlling a test object to correspondingly run, on the other hand, the front end transmits the status information of the front-end PLC set to the rear-end PLC set. The front-end and rear-end PLC sets allow front-end and rear-end data transmission through establishing a controller link network.

Description

technical field [0001] The invention provides a long-distance data transmission system for measurement, launch and control, which belongs to the field of spaceflight measurement, launch and control. Background technique [0002] At present, in the field of aerospace measurement, launch and control, the measurement, launch and control system based on long-distance data transmission is widely used. This kind of measurement, launch and control system is divided into two parts, the front end and the back end, according to the location of the equipment. The front-end equipment of the measurement and control system is placed near the launch tower, which is used to convey the control instructions issued by the back-end of the measurement and control system to the object under test; the back-end equipment of the measurement and control system is placed in the remote control test room as the entire measurement and control system operations, command and control center. Usually, the f...

Claims

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Application Information

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IPC IPC(8): G05B19/418
CPCY02P90/02
Inventor 梁海波刘志华司文杰李浩梁婕吕章刚许昊
Owner BEIJING AEROSPACE AUTOMATIC CONTROL RES INST
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