Information control platform used for informationized rocket launching

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 ...

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 leads to the long launch cycle of the entire commercial rocket. Only artificial means can be used to optimize the cycle, and there is a lack of essential changes from the design source and technical means.

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