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Remote sensing satellite autonomous health management system

A health management system and remote sensing satellite technology, applied in the field of remote sensing satellite autonomous health management systems, can solve problems such as failure to detect satellite deterioration trends in time, inability to adapt to work mode remote sensing satellite health management needs, and extensive fault detection thresholds.

Pending Publication Date: 2020-10-23
BEIJING INST OF SPACECRAFT SYST ENG
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  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, because the fault detection model of the autonomous health management mentioned above is designed for the fixed satellite mode, the fault detection threshold is relatively extensive, and it is impossible to detect the deterioration trend of the satellite in time, especially unable to adapt to the health management requirements of remote sensing satellites with changing working modes and complex satellite states.

Method used

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  • Remote sensing satellite autonomous health management system
  • Remote sensing satellite autonomous health management system
  • Remote sensing satellite autonomous health management system

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Embodiment Construction

[0025] Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. Although exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited by the embodiments set forth herein. Rather, these embodiments are provided for more thorough understanding of the present disclosure and to fully convey the scope of the present disclosure to those skilled in the art. It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0026] figure 1 It is a structural block diagram of the remote sensing satellite autonomous health management system provided by the embodiment of the presen...

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Abstract

The invention discloses a remote sensing satellite autonomous health management system. The system comprises a basic data management module, an operation state management module, a mode conversion management module, a health state detection module and a system health management module. According to the invention, the working mode of the remote sensing satellite is continuously changed; according to the remote sensing satellite fault isolation reconstruction method, the targeted autonomous health management function is still realized, the influence of different working modes on the refinement degree of the health management criterion is avoided, the accuracy degree of the fault isolation reconstruction operation is improved, and the continuous and stable operation capability of the remote sensing satellite is further improved.

Description

technical field [0001] The invention belongs to the technical field of overall satellite design, and in particular relates to an autonomous health management system for remote sensing satellites. Background technique [0002] Autonomous health management of spacecraft refers to the ability to operate independently, safely and reliably without relying on ground support. The degree of autonomy reflects the degree of dependence of spacecraft health management on the ground and operators. Autonomous health management technology can provide three capabilities of the spacecraft: first, real-time processing of satellite raw health telemetry data, extracting and downloading effective information, reducing the workload of ground system monitoring and interpretation one by one, and avoiding missed and wrong judgments; Predict the working status and development trend of system components according to the spacecraft failure prediction model or reliability model to avoid failures; the t...

Claims

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Application Information

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IPC IPC(8): G06Q10/06G06Q10/00G05B23/02B64G1/10
CPCG06Q10/0639G06Q10/20G05B23/0275B64G1/10
Inventor 任放潘莉张新伟曹海翊赵晨光鲁超莫凡徐驰国爱燕戴君陈曦张莎莎姚鑫雨孙海涛殷亚州黄金印
Owner BEIJING INST OF SPACECRAFT SYST ENG
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