Design system and fault information quick positioning method for intellectualizing satellite measurement and control information stream based on model

Abstract

The invention relates to a design system and fault information quick positioning method for intellectualizing a satellite measurement and control information stream based on a model. Satellite remotemeasurement and remote control information is extracted from the satellite remote measurement and remote control information stream. The information comprises remote measurement and remote control source terminal equipment information, remote measurement and remote control type information and remote measurement and remote control target equipment information; remote measurement and remote controlnumber information is counted by using a satellite remote measurement and remote control information counting module; then remote measurement and remote control information is classified and graded through a satellite remote measurement and remote control information classification and grading module; a standard model and standard linear information in a satellite remote measurement and remote control information dictionary standard module are called, and the modelling pattern design work of the satellite remote measurement and remote control information stream is completed in a model establishment and line connection operation module; different versions are stored in a version control module; finally, a module output design result is output by using an information stream result. The whole process of intellectualized seamless design of the spacecraft information stream is achieved, the design process is standardized, and the total design capacity is improved.

Description

technical field [0001] The invention relates to a model-based intelligent design system for satellite measurement and control information flow and a fast positioning method for fault information, which can be popularized and applied in the overall design of all satellite information. Background technique [0002] The design of measurement and control information flow is the embodiment of the flow direction of satellite telemetry and remote control information, and meets the needs of spaceborne equipment layout. Its rationality and correctness determine the layout of onboard instruments and the allocation capability of satellite information resources. The quality of the measurement and control information flow design will directly affect the utilization rate of on-board resource allocation and the timeliness and correctness of the implementation of failure plans. For the design of measurement and control information flow, it is necessary to formulate the direction of informat...

AI Technical Summary

Problems solved by technology

[0004] The diversification of user needs and the variety of satellite models lead to heavy satellite design tasks, a huge amount of information flow data, and the complexity of the information flow data structure, which requires a lot of manpower and material resources to process, but the time allowed for the task is limited, so in the current manpower, time and other factors There are many limitations; the satellite information flow design work has problems such as long time-consuming, repetitive and mechanical workload, low work efficiency, high number of iterations, many uncontrollable versions of design results, and poor standardization of design results.

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