Hierarchical software health management method and system for microsatellites

A technology for microsatellites and health management, applied in the field of software health management systems for microsatellites, it can solve the problems of difficult system implementation and complex algorithms, improve timeliness and accuracy, simplify computation, and improve the reliability of the whole satellite Effect

Active Publication Date: 2020-02-14
INNOVATION ACAD FOR MICROSATELLITES OF CAS +1
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, with the development trend of software-intensive micro-satellites, there are more and more software failures caused by the increasing software complexity. Therefore, it may be difficult to expose software abnormalities in a timely manner by relying solely on the status monitoring of on-board hardware.
In addition, although there are literatures mentioning some studies on on-board autonomous health management systems, these systems are not well classified and processed according to signal characteristics from the perspective of engineering implementation.
Due to the large amount of satellite sampling signals and the complex algorithms required for system analysis and processing, these systems are difficult to implement in the effective resource environment on the satellite

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  • Hierarchical software health management method and system for microsatellites
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  • Hierarchical software health management method and system for microsatellites

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Embodiment Construction

[0034] In the following description, the present invention is described with reference to various examples. One skilled in the art will recognize, however, that the various embodiments may be practiced without one or more of the specific details, or with other alternative and / or additional methods, materials, or components. In other instances, well-known structures, materials, or operations are not shown or described in detail so as not to obscure aspects of the various embodiments of the invention. Similarly, for purposes of explanation, specific quantities, materials and configurations are set forth in order to provide a thorough understanding of embodiments of the invention. However, the invention may be practiced without these specific details. Furthermore, it should be understood that the various embodiments shown in the drawings are illustrative representations and are not necessarily drawn to scale.

[0035] In this specification, reference to "one embodiment" or "the...

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Abstract

The invention provides a hierarchical software health management method and system for microsatellites. The hierarchical software health management system performs hierarchical health management on satellites according to different subsystems, and comprises a sensor layer, a state monitoring layer, a health evaluation layer, a prediction layer, a decision processing layer and the like. Through software sensors deployed at operation key nodes of all sub-components of satellite housekeeping, the hierarchical software health management method collects running state data of each sub-component andanalyzes the running state data to obtain fault information, hierarchically evaluates the health condition of the current satellite system in combination with satellite historical telemetry data, software system knowledge and the fault information, pre-judges the health condition of the system at the future moment, and finally makes a health hazard strategy.

Description

technical field [0001] The invention relates to the field of fault diagnosis of satellite software, in particular to a micro-satellite-oriented software health management system. Background technique [0002] Although microsatellites are small in size and light in weight, compared with large satellites, their basic components have not been greatly reduced, but still include various sensors, actuators, and integrated management systems. At the same time, due to cost constraints, microsatellites usually use software redundancy to improve the reliability of the entire star. However, most of the satellite in-orbit failures involve software errors or abnormal software-hardware interaction scenarios. Therefore, this software redundancy design leads to software-intensive design, which greatly increases the probability of satellite in-orbit failures. In order to minimize fault propagation and its impact, once a fault occurs, it must be detected as soon as possible and its slow-chan...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F11/30
CPCG06F11/302G06F11/3065G06F11/3089
Inventor 王明亮常亮王番王永朱振才高才栋
Owner INNOVATION ACAD FOR MICROSATELLITES OF CAS
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