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Satellite power supply controller, testability verification method and testability verification platform

A technology of satellite power supply and verification method, applied in electrical testing/monitoring, general control system, control/regulation system, etc., can solve the lack of design defects, lack of testing resources and testing methods, difficult to detect and locate specific components, etc. problems, to achieve the effect of increasing testability, improving self-diagnosis and external diagnostic capabilities, ensuring coverage and diagnostic efficiency

Inactive Publication Date: 2019-10-01
SHENZHEN ACAD OF AEROSPACE TECH +2
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This mode of operation utilizing ground-based comprehensive test coverage to ensure mission reliability and safety results in an overall lack of focus on product design flaws in inherent testability
At the same time, due to the lack of effective testing resources and testing methods during operation, it is difficult to directly detect and locate specific components when a fault occurs

Method used

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  • Satellite power supply controller, testability verification method and testability verification platform
  • Satellite power supply controller, testability verification method and testability verification platform
  • Satellite power supply controller, testability verification method and testability verification platform

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Embodiment Construction

[0028] The present invention will be further described below in conjunction with the description of the drawings and specific embodiments.

[0029] Such as Figure 1 to Figure 4 As shown, a satellite power controller (PCU) includes a satellite power controller body 1 and a health management module 2 , and the satellite power controller body 1 is connected to the health management module 2 . Health management module 2 is the PHM module.

[0030] Such as Figure 1 to Figure 4 As shown, the health management module 2 includes a core board 21, n simulation boards 22 and an interconnection backplane 23, for example, three simulation boards 22 can be preferably set, and the core board 21 and the simulation board 22 are respectively connected to the The interconnection backplane 23 is connected, and the interconnection backplane 23 is the adjustment backplane. The core board 21 is mainly used to run fault diagnosis algorithms and communicate. The simulation board 22 is mainly respo...

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Abstract

The invention provides a satellite power supply controller. The satellite power supply controller comprises a satellite power supply controller body and a health management module; and the satellite power supply controller body is connected with the health management module. The invention further provides a testability verification method. The invention further provides a testability verificationplatform. The verification platform provided by the invention has the advantages that the testability of the satellite power supply controller is increased by adding a modular-designed health management module; the fault diagnosis coverage rate and diagnostic efficiency of the satellite power supply controller are guaranteed, and the self-diagnosis and external diagnosis capacity are improved.

Description

technical field [0001] The invention relates to a satellite power controller (PCU), in particular to a satellite power controller, a testability verification method and a testability verification platform. Background technique [0002] Satellites are technology-intensive and complex high-tech products. Despite the guarantee of high reliability, satellites operate in a space environment full of vacuum, weightlessness, high and low temperature, strong radiation and full of unknown interference factors for several years or even ten years, and aging of components and failures are inevitable. In order to ensure the safety of the satellite and avoid the breakdown of the entire system caused by the failure of a single component, it must be quickly and effectively dealt with at the beginning of the failure to maintain the normal function of the system. To achieve the above technical requirements, it is necessary to carry out test design work starting from satellite design, to ensur...

Claims

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Application Information

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IPC IPC(8): G05B23/02G06F17/50G06Q10/06G06Q50/06
CPCG05B23/0213G06Q10/0639G06Q50/06G06F30/367
Inventor 李安寿孙波柳新军朱洪雨张雷张东来贾毅婷李志栋张斌韩骞逸石玉
Owner SHENZHEN ACAD OF AEROSPACE TECH