Solar wing spreading reliability estimation method based on multilevel gray comprehensive model

A comprehensive model, reliable technology, applied in special data processing applications, instruments, electrical digital data processing, etc., can solve problems such as lack of experience, incomplete information, small samples, etc.

Inactive Publication Date: 2012-02-15
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
View PDF2 Cites 15 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] Purpose of the invention: In order to solve the reliability evaluation problem of solar wing deployment under the uncertainty of less data, small samples, incomplete information and lack of experience, on the basis of absorbing the advantages of gray system theory, it is proposed to divide the reliability elements into layers , and use the analytic hierarchy process, combined with the matter-element method to determine the weight of each reliability factor, thereby improving the objectivity of each weight index, forming a reliability based on a multi-level, gray comprehensive evaluation model that can solve small sample data. sex assessment method

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
  • Solar wing spreading reliability estimation method based on multilevel gray comprehensive model
  • Solar wing spreading reliability estimation method based on multilevel gray comprehensive model
  • Solar wing spreading reliability estimation method based on multilevel gray comprehensive model

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0036] In order to make the purpose, technical solution and advantages of the present invention clearer, the best embodiments will be described in detail below with reference to the accompanying drawings.

[0037] The method of the present invention is as figure 1 As shown, the specific steps are as follows:

[0038] Step 1: Determine the reliability evaluation index set and determine the index level;

[0039] Combined with the characteristics of the experimental object itself and a large amount of literature, the test elements and the characteristics of key components in the solar wing deployment test are divided into the following categories: image 3 The three levels shown include four first-level indicators: the basic frequency of the unfolded state, the minimum static moment margin, the evaluation index of the hinge driving characteristic and the evaluation index of the unfolding experiment; the hinge driving characteristic evaluation index includes the following five as...

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 discloses a solar wing spreading reliability estimation method based on a multilevel gray comprehensive model. The method comprises the following steps: determining a reliability estimation index set, and determining an index grade; organizing experts to score the index set; establishing an evaluation matrix, and determining an evaluation grey class; computing weight of each factor by using a matter element method and an analytic hierarchy process; computing a grey evaluation coefficient; and outputting a comprehensive evaluation result. The method provided by the invention is applied to the reliability estimation on a small sample and a limited information experiment object, and can accurately estimate the solar wing spreading reliability. The method has the advantages that the reliability factor can be layered, and the analytic hierarchy process is combined with the matter element method to determine the weight of the reliability factor, and the comprehensive estimation result is intuitive, objective and credible.

Description

technical field [0001] The invention relates to a reliability evaluation method for small sample and poor information experimental objects, in particular to a solar wing deployment reliability test evaluation method based on a multi-level gray comprehensive model. Background technique [0002] With the rapid development of aerospace technology, the structure of spacecraft is becoming more and more complex, and its functions are increasing. Various mechanisms are required to complete various tasks. If the solar wings cannot be deployed normally, it will cause disastrous consequences and cause heavy losses to national property. However, due to the high cost of the solar wing mechanism, it is impossible to conduct large-scale experiments. Gray evaluation is good at dealing with poor information systems, it can model, predict and evaluate under the condition of short data and little information. Gray system theory is a good mathematical tool for uncertain problems with little ...

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): G06F19/00
Inventor 皮德常于安雷
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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