Variable sequence calculation method containing plurality of spacecraft telemetry parameters

A technology of telemetry parameters and calculation methods, applied in the field of variable sequence calculation of telemetry parameters, can solve problems such as inaccurate calculation results, statistical analysis results of influencing index variables, different start and end time periods and sampling intervals of multiple telemetry parameters, etc. The effect of improving accuracy and avoiding abnormal data

Active Publication Date: 2020-05-08
CHINA XIAN SATELLITE CONTROL CENT
View PDF6 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003]Currently, the methods of using multiple telemetry parameters to calculate derived variables or compound variables mostly focus on flexible and scalable configuration methods, but they all complete single-point values At the same time, there are two problems in the existing calculation methods for multivariate sequences with non-uniform time scales: first, the data start and end time periods and sampling intervals of multiple telemetry parameters may be different, and the calculation method is carried out according to the specified time Sampling alignment may introduce a large number of redundant points, which will affect the statistical analysis results of indicator variables; second, there may be large differences in the sampling intervals of multiple telemetry parameters, and the calculation results of variables between the sampling interval differences are not accurate. The impact of some abnormal data

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
  • Variable sequence calculation method containing plurality of spacecraft telemetry parameters
  • Variable sequence calculation method containing plurality of spacecraft telemetry parameters
  • Variable sequence calculation method containing plurality of spacecraft telemetry parameters

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0023] The present invention will be further described below in conjunction with the accompanying drawings and embodiments, and the present invention includes but not limited to the following embodiments.

[0024] Such as figure 1 As shown, the present invention provides a variable sequence calculation method comprising a plurality of spacecraft telemetry parameters, which specifically includes the following steps:

[0025] The first step: multi-telemetry parameter extraction, data preparation and sequence merging;

[0026] The second step: variable calculation and sequence result collection;

[0027] Step 3: Filtering of variable sequence calculation results.

[0028] The input of this calculation method has three items: paraCalStr, startTime, endTime, and paraCalStr contains telemetry parameter code and "+, -, *, / , %, ==, >, =, <=, (,), [ ,]” is an expression string, startTime is the start time of the sequence calculation, and endTime is the end time of the sequence calc...

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 invention provides a variable sequence calculation method containing a plurality of spacecraft telemetry parameters. The method comprises the following steps: firstly, extracting names of all telemetry parameter codes, preparing required telemetry parameter sequences, combining the telemetry parameter sequences, carrying out null value filling processing on the combined telemetry parameter sequences, then calculating variable values according to paraCalStr, finally forming a variable sequence by all the calculated variable values, and filtering a result sequence. According to the method, the problem that a large number of redundant points are introduced through interpolation alignment is solved, the statistical property of the result variable sequence is guaranteed, abnormal data possibly introduced due to the sampling interval time difference of multiple telemetry parameters is avoided, and the accuracy of the calculation result of the variable sequence containing the multiple spacecraft telemetry parameters is improved.

Description

technical field [0001] The invention belongs to the field of spacecraft telemetry data analysis, in particular to a variable sequence calculation method of telemetry parameters. Background technique [0002] When conducting medium- and long-term trend analysis and prediction of spacecraft components, and evaluation and evaluation of performance indicators, it is necessary to use long-term telemetry data sequences. A new variable is calculated by a combination of telemetry parameters, and the value sequence calculation of the long-term interval of the new variable is completed. [0003] At present, the methods of using multiple telemetry parameters to calculate derived variables or compound variables are mostly focused on flexible and scalable configuration methods, but they all complete the calculation of single point values, and the existing multivariate sequences with different time scales There are also two problems in the calculation method: First, the data start and en...

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): G06F17/18
CPCG06F17/18
Inventor 付枫刘军李卫平李剑锋吴东星高宇李涵秋宁顺成韩星郭小红杨怀军王婷
Owner CHINA XIAN SATELLITE CONTROL CENT
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