Information control platform used for informationized rocket launching

A rocket launch platform and information control technology, applied in the general control system, control/regulation system, test/monitoring control system, etc., can solve the problems of unsatisfactory rapid mobile launch, lack of essential changes, long test cycle, etc., and achieve simplification The scale of the ground system and the number of equipment, the effect of meeting the needs of rapid mobile launch and short test period

Active Publication Date: 2019-04-09
BEIJING INST OF ASTRONAUTICAL SYST ENG +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] b) It cannot meet the needs of rapid mobile launch, and can only be used in the remote test launch mode at a fixed location;
[0005] c) The operating efficiency is low and the test cycle is long, which

Method used

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  • Information control platform used for informationized rocket launching
  • Information control platform used for informationized rocket launching
  • Information control platform used for informationized rocket launching

Examples

Experimental program
Comparison scheme
Effect test

Embodiment

[0074] The information control platform is mainly composed of a chassis, a backplane, a power management module, a main control management module and other common modules.

[0075] (1) Chassis and Backplane

[0076] The chassis adopts an all-aluminum reinforced design to realize quick plug-in and pull-out of various functional modules and facilitate maintenance; it adopts conduction cooling + air-cooling heat dissipation mode, which has good environmental adaptability.

[0077] The backplane is the carrier of all modules in the chassis, providing bus interconnection and power interconnection for all modules inside the information control platform.

[0078] The filter in the power management module is installed inside the chassis. The external input power is filtered by the filter first, and the filtered power supplies +12V and +3.3V working voltages for each functional module through the power management module. Other power supplies required by the module Generated by the mod...

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Abstract

The invention discloses an information control platform used for informationized rocket launching. The information control platform platform comprises a back plate arranged in a case, and a power supply management module, a master control management module, a calculation resource module, a data storage module, a communication management module and a network switching module inserted on the back plate. The power management module supplies power to all the modules of the information control platform; the master control management module is used for realizing centralized management and control ofall the modules; the calculation resource module is used for completing a ground test process, a launching control process and a command process; the data storage module provides a shared space of data storage for the information control platform; the communication management module is used for achieving various wired and/or wireless communication between the front end and the rear end of a rocket launching platform; and the network switching module realizes interconnection and intercommunication of all the modules inside the information control platform. Equipment is highly integrated; the network management and maintenance are convenient; the requirement of fast flexible launching can be met; interfaces are simple; the testing efficiency is high; and the launching period of a commercialrocket can be obviously shortened.

Description

technical field [0001] The invention relates to an integrated and intelligent information control platform for launching an information rocket, which belongs to the field of information application. Background technique [0002] In the past, commercial rocket launch platforms consisted of multiple systems such as launch towers, ground measurement and launch control systems, ground measurement systems, and test and launch network systems. . Through the establishment of a measurement and control network, the information transmission of each system is realized, and the comprehensive utilization of rocket control, measurement, utilization, power system and launch site C 3 I system test information, command and monitor rocket test and launch. Generally, the liquid rocket test and launch control system in the remote control state is divided into front-end and back-end. The measurement and control network builds a measurement and control network information exchange platform for ...

Claims

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Application Information

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IPC IPC(8): G05B23/02
CPCG05B23/0224
Inventor 管洪仁李婧张利彬郑小刚王大敏王芳沈超鹏易航廖友萍施清平阎小涛马宏伟任卉康健邵旭东宋永生
Owner BEIJING INST OF ASTRONAUTICAL SYST ENG
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