Ground integrated measurement and control system for carrier rocket

Abstract

The invention discloses a carrier rocket ground integrated measurement and control system which comprises a network communication module, an instruction analysis module, a heartbeat detection module, a bus communication module, a function module, a fault diagnosis module and a master-slave switching module. Wherein after the network communication module receives an instruction of an upper computer, the received instruction is sent to the instruction analysis module; the instruction analysis module compares the instruction with a preset configuration file, the configuration file contains a mapping table of the instruction and specific content, the specific instruction content is obtained through comparison, and the module corresponding to the instruction content in the function module is called according to the instruction content. Different functions correspond to different modules, different functions are achieved through different modules, the modules are mutually independent, and function expansion and tailoring are facilitated.

Description

technical field [0001] The invention belongs to the technical field of aerospace electronic system design, and in particular relates to a launch vehicle ground integrated measurement and control system. Background technique [0002] With the development of launch vehicle ground measurement and control equipment equipment, the general-purpose front-end measurement and control equipment of "internal bus + modular board" will be the future trend. Due to the different processors and operating systems used in this type of measurement and control equipment, and the different types and quantities of internal modular boards, there is currently no general software architecture. On the other hand, even for the same device, there are often some differences in requirements due to different users, which brings relatively high requirements for the scalability and scalability of the software architecture. Contents of the invention [0003] The technical problem solved by the present inv...

AI Technical Summary

Problems solved by technology

Due to the different processors and operating systems used in this type of measurement and control equipment, the types and quantities of internal modular boards are different, so there is currently no general software architecture.

On the other hand, even for the same device, there are often some differences in requirements due to different users, which brings relatively high requirements for the scalability and scalability of the software architecture.

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