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A Spacecraft On-orbit Abnormal Alarm and Fault Diagnosis System

A fault diagnosis system and abnormal alarm technology, applied in the field of aerospace fault diagnosis, can solve problems such as uncertainty, difficult description, and difficulty in penumbra description.

Active Publication Date: 2017-12-08
BEIJING INST OF SPACECRAFT SYST ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the evidence used in the actual diagnosis process is not completely accurate, some information is not perfect, and some are uncertain
For example, in the state of the earth's shadow, it is more difficult to describe the penumbra area. Since when the penumbra is regarded as the earth's shadow, it is difficult to describe it with precise reasoning

Method used

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  • A Spacecraft On-orbit Abnormal Alarm and Fault Diagnosis System
  • A Spacecraft On-orbit Abnormal Alarm and Fault Diagnosis System
  • A Spacecraft On-orbit Abnormal Alarm and Fault Diagnosis System

Examples

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example 1

[0057] Example 1: Bus voltage drop (undervoltage) in the lighting area

[0058] The normal value of the bus voltage in the light area should be 42V±0.5V. The reasons for the voltage drop are:

[0059] (1) The fault of the shunt regulator causes the shunt value to be too large, the output power of the solar cell array is shunted, the bus voltage control fails, and the load cannot be powered. Check the error signal output of the busbar: north VN4 (south VN12) ≥ 6V. Whether the -12V power supply is open circuit (telemetry code).

[0060] (2) INTO MOON SHADOW. (Normal phenomenon, calculated according to calculation and forecast)

[0061] (3) The load current on the bus is overcurrent. It cannot return to normal until the short circuit factor is eliminated

[0062] (4) The solar panel reverses and stops. Return the sailboard to its normal state.

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Abstract

The invention discloses a spacecraft on-orbit anomaly alarming and fault diagnosing system. A knowledge editor inputs well-compiled alarming diagnosis knowledge; a data buffer area buffers inputted original telemetering data; a data area extracts telemetering data or a telemetering instruction from the data buffer area when a reasoning controller carries out logic matching operation and stores the data or the instruction; a rule area loads the well-compiled alarming diagnosis knowledge from the knowledge editor, and in the rule area, each piece of the alarming diagnosis knowledge is called a rule; the reasoning controller carries out logic matching operation on the original telemetering data in the data area and the alarming diagnosis knowledge in the rule area to acquire diagnosis results; a diagnosis result which needs to be outputted is selected to be outputted to a blackboard; the blackboard stores the diagnosis result acquired through the logic matching operation by the reasoning controller; and a result buffer area buffers the diagnosis result which is selected to be outputted by the reasoning controller and the result is sent to a client, and after a user checks the diagnosis result via the client, a confirmation message is answered.

Description

technical field [0001] The invention belongs to the technical field of aerospace fault diagnosis, in particular to an on-orbit abnormal alarm and fault diagnosis system for spacecraft. Background technique [0002] The core of the reasoning machine subsystem is to perform logical reasoning operations based on expert knowledge and input measurement and control data, and finally deduce the abnormal state of the spacecraft. Its essence is to realize a virtual machine with logical reasoning ability. Early expert systems mainly used deterministic reasoning algorithms, and the evidence represented by this method was deterministic. For example, taking the state of the earth shadow as an example, it is either the light area or the earth shadow area, and there is no ambiguity. Its reasoning process is based on mathematical logic, the reasoning process is rigorous, and the conclusion is also accurate, either true or false. However, the evidence used in the actual diagnosis process i...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B23/02
CPCG05B23/0229
Inventor 王环秦巍闫谦时郭义琪颜灵伟韩洪波王晓晨李强田华东邱瑞郭永富张晓鹏罗毓芳陈曦金迪陈炜钊左子瑾张香燕刘鹏翁嘉
Owner BEIJING INST OF SPACECRAFT SYST ENG