Telemetry Configuration Management Method for Satellite-Ground Integration

A configuration management and satellite telemetry technology, applied in the field of satellite-ground integration telemetry configuration management, can solve the problems of satellite telemetry configuration satellite-ground integration management, etc. Effect

Active Publication Date: 2022-03-29
SHANGHAI SATELLITE ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, the prior art does not solve the specific problem of how to realize the integrated management of satellite telemetry configuration and satellite ground proposed by the present invention.

Method used

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  • Telemetry Configuration Management Method for Satellite-Ground Integration
  • Telemetry Configuration Management Method for Satellite-Ground Integration
  • Telemetry Configuration Management Method for Satellite-Ground Integration

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Embodiment

[0068] In order to solve the problem of satellite-terrestrial integrated management of satellite telemetry configuration, the present invention provides a satellite-terrestrial integrated telemetry configuration management method, which includes the following steps: automatic generation of satellite-terrestrial integrated frame table configuration files, hierarchical analysis of satellite telemetry, and layer-based Closed-loop comparison of star-earth telemetry equivalently generated by simplified telemetry.

[0069] The preferred embodiments of the present invention are given below in conjunction with the accompanying drawings to describe the technical solution of the present invention in detail.

[0070] The invention proposes a brand-new method in order to solve the problem of satellite-ground integrated management of satellite telemetry configuration. The present invention provides a method for integrated generation and management of star affairs frame table, ground teleme...

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Abstract

The present invention relates to a satellite-terrestrial integrated telemetry configuration management method in the field of satellite development process and on-orbit telemetry programming technology; Closed-loop comparison of star-earth telemetry equivalently generated by hierarchical telemetry; the present invention adopts the design of hierarchical telemetry table, which can automatically generate large table of ground telemetry analysis, configuration file of star mission grouping and on-orbit programming of telemetry, which is well adapted to The requirement of frequent change of telemetry organization in the satellite development stage reduces the workload of framing arrangement and telemetry analysis and configuration of comprehensive measurement, measurement and control, and star affairs; Programming modification ability; the present invention adopts three-dimensional telemetry configuration, improves telemetry traceability, enhances telemetry tracking and positioning capabilities, quickly locates telemetry points and transmission paths, and facilitates troubleshooting.

Description

technical field [0001] The invention relates to the technical field of satellite development process and on-orbit telemetry programming, in particular to a satellite-ground integrated telemetry configuration management method. Background technique [0002] as attached Figure 7 As shown, there are multiple telemetry modes in satellite telemetry, and each telemetry mode has a corresponding frame table configuration. During the satellite development process, the telemetry frame table arrangement scheme has been changed many times, which consumes a lot of energy of the measurement and control and satellite affairs subsystems. The TT&C and satellite sub-system personnel first communicate with each satellite sub-system to coordinate the number and size of the telemetry packets, and the frequency of downloading the information in the packets, and distribute the telemetry packets to the corresponding sections of the telemetry frame according to the required frequency. Insufficient ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F9/445G06F40/18
CPCG06F9/44505
Inventor 杨同智阎珺刘廷玉曾齐盛开明
Owner SHANGHAI SATELLITE ENG INST
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