A Method for Dividing Analysis Window of Multi-telemetry Parameters of Spacecraft
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- 中国人民解放军63789部队
- Publication Date
- 2019-03-15
- Estimated Expiration
- Not applicable · inactive patent
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Abstract
Description
technical field
[0001] The invention belongs to the field of spacecraft telemetry data analysis, and in particular relates to a multi-telemetry parameter analysis window division method of a spacecraft. Background technique
[0002] With the development of information technology, fault feature extraction and diagnosis technology has been greatly developed in the field of spacecraft telemetry data analysis. Among them, determining the feature analysis window is a basic problem in the analysis of spacecraft telemetry data, which directly determines the accuracy and reliability of feature extraction and diagnostic detection.
[0003] At present, the multi-telemetry data analysis of spacecraft mostly uses fixed windows or sliding windows to divide each parameter into multiple analysis subsequences in turn. There are two problems in this division method: First, due to the maneuvering characteristics of the spacecraft and the complexity of the space environment, it is difficult t...