Satellite long-period heteroscedasticity degradation prediction and evaluation method based on GRU and GARCH

A heteroscedasticity and long-period technology, which is applied in the field of satellite long-period heteroscedasticity degradation prediction and evaluation based on GRU and GARCH, can solve the problems of limited abnormality monitoring effect and rough threshold setting

Pending Publication Date: 2020-12-18
BEIHANG UNIV
View PDF0 Cites 11 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, there are also certain patent achievements in satellite degradation prediction evaluation and anomaly monitoring, such as "A satellite anomaly detection method against network autoencoder", "A method for automatic error detection of satellite telemetry parameter position information", " A Data-Driven Satellite Subsystem Anomaly Prediction Method", etc. Traditional anomaly monitoring methods are based on artificially set thresholds to monitor the deviation between satellite parameters and thresholds. Such methods are vulnerable to artificially set thresholds. Due to satellite fluctuations and seasonal changes in parameters, the traditional threshold setting is relatively rough, and the monitoring effect on some abnormal points is limited

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Satellite long-period heteroscedasticity degradation prediction and evaluation method based on GRU and GARCH
  • Satellite long-period heteroscedasticity degradation prediction and evaluation method based on GRU and GARCH
  • Satellite long-period heteroscedasticity degradation prediction and evaluation method based on GRU and GARCH

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0074] The embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings. It should be understood that the embodiments described below are only used to illustrate and explain the present invention, and are not intended to limit the present invention.

[0075] figure 1It is the first schematic flow chart of a GRU and GARCH-based satellite long-period heteroscedastic degradation prediction and evaluation method provided by an embodiment of the present invention, as shown in figure 1 As shown, the steps include:

[0076] Step 1: The sensor collects satellite telemetry parameter data;

[0077] Real satellite in-orbit telemetry data is used as an example in this patent. All data in this case comes from a sun-synchronous orbit satellite. During satellite operation, temperature is an important parameter. The parameter selected in this case is "temperature in the service module", hereinafter referred to as "temperature". A la...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

The embodiment of the invention provides a satellite long-period heteroscedasticity degradation prediction and evaluation method based on GRU and GARCH, and the design idea comprises: firstly carryingout preprocessing and time sequence decomposition on an original parameter for the long-term degradation and heteroscedasticity characteristics of telemetry parameter data collected by a sensor, andpredicting a trend term through a GRU model. In order to solve the problem of long-term degradation, the GARCH model predicts residual terms to solve the problem of heteroscedasticity; and a satelliteparameter prediction result is obtained in combination with a satellite seasonal period rule. Meanwhile, normal fluctuation threshold information of the satellite is extracted from the residual termand is combined with the season term and the trend term, so that construction of the satellite stability consistency adaptive threshold is realized, and the satellite stability consistency health assessment method is provided based on the adaptive threshold. The method can accurately predict the telemetry data which is greatly influenced and fluctuated by the satellite environment and multiple tasks, and the threshold value can be updated on line and is more effective and accurate compared with a traditional method.

Description

technical field [0001] The invention relates to the satellite field, in particular to a GRU and GARCH-based satellite long-period heteroscedastic degradation prediction and evaluation method. Background technique [0002] Since the satellite is in the harsh outer space environment such as solar radiation for a long time, unpredictable abnormalities or failures may occur during its in-orbit operation. Taking measures in advance to detect these unpredictable abnormalities or failures in time is crucial to ensuring the long-term stable operation of the satellite. important. Therefore, anomaly detection of telemetry data is of great significance in the fields of satellite troubleshooting and real-time health monitoring. Considering the complex design structure and harsh working environment of the satellite, it is impossible to directly perform anomaly detection in the outer space environment. At present, by installing multiple sensors on each component of the satellite, the on...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
Patent Type & Authority Applications(China)
IPC IPC(8): G06Q10/04G06N3/04
CPCG06Q10/04G06N3/048G06N3/045
Inventor 陶来发张统郝杰贾苑丁宇吕琛
Owner BEIHANG UNIV
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products