Study on test method of reliability assessment used for performance parameter-measured spacecraft mechanism

Ji Li Rong; Tao Zhang; Tian Fu Xu; Yue Qi

doi:10.3873/j.issn.1000-1328.2012.03.016

Study on test method of reliability assessment used for performance parameter-measured spacecraft mechanism

Ji Li Rong^*, Tao Zhang, Tian Fu Xu, Yue Qi

^*Corresponding author for this work

Beijing Institute of Technology

Research output: Contribution to journal › Article › peer-review

7 Citations (Scopus)

Abstract

Against the functional characteristic of performance parameter measured spacecraft mechanism and the feasibility of test methods, a practical method for assessing the reliability is proposed. The method is used to measure the key parameters to determine the reliability characteristics and the allowable value range corresponding to the trouble-free working conditions based on an analysis of the product performance. Using the observed sample values and mathematical statistics method, the lower confidence limit of product reliability can be evaluated. Examples indicate that the method in this paper is much simpler, easier to use, and can meet to the aerospace products' reliability test requirements.

Original language	English
Pages (from-to)	387-391
Number of pages	5
Journal	Yuhang Xuebao/Journal of Astronautics
Volume	33
Issue number	3
DOIs	https://doi.org/10.3873/j.issn.1000-1328.2012.03.016
Publication status	Published - Mar 2012

Keywords

Confedence lower limit
Normal distribution
Performance parameter
Reliability assessment
Reliability characteristic
Spacecraft mechanism

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10.3873/j.issn.1000-1328.2012.03.016

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title = "Study on test method of reliability assessment used for performance parameter-measured spacecraft mechanism",

abstract = "Against the functional characteristic of performance parameter measured spacecraft mechanism and the feasibility of test methods, a practical method for assessing the reliability is proposed. The method is used to measure the key parameters to determine the reliability characteristics and the allowable value range corresponding to the trouble-free working conditions based on an analysis of the product performance. Using the observed sample values and mathematical statistics method, the lower confidence limit of product reliability can be evaluated. Examples indicate that the method in this paper is much simpler, easier to use, and can meet to the aerospace products' reliability test requirements.",

keywords = "Confedence lower limit, Normal distribution, Performance parameter, Reliability assessment, Reliability characteristic, Spacecraft mechanism",

author = "Rong, {Ji Li} and Tao Zhang and Xu, {Tian Fu} and Yue Qi",

year = "2012",

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doi = "10.3873/j.issn.1000-1328.2012.03.016",

language = "English",

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T1 - Study on test method of reliability assessment used for performance parameter-measured spacecraft mechanism

AU - Rong, Ji Li

AU - Zhang, Tao

AU - Xu, Tian Fu

AU - Qi, Yue

PY - 2012/3

Y1 - 2012/3

N2 - Against the functional characteristic of performance parameter measured spacecraft mechanism and the feasibility of test methods, a practical method for assessing the reliability is proposed. The method is used to measure the key parameters to determine the reliability characteristics and the allowable value range corresponding to the trouble-free working conditions based on an analysis of the product performance. Using the observed sample values and mathematical statistics method, the lower confidence limit of product reliability can be evaluated. Examples indicate that the method in this paper is much simpler, easier to use, and can meet to the aerospace products' reliability test requirements.

AB - Against the functional characteristic of performance parameter measured spacecraft mechanism and the feasibility of test methods, a practical method for assessing the reliability is proposed. The method is used to measure the key parameters to determine the reliability characteristics and the allowable value range corresponding to the trouble-free working conditions based on an analysis of the product performance. Using the observed sample values and mathematical statistics method, the lower confidence limit of product reliability can be evaluated. Examples indicate that the method in this paper is much simpler, easier to use, and can meet to the aerospace products' reliability test requirements.

KW - Confedence lower limit

KW - Normal distribution

KW - Performance parameter

KW - Reliability assessment

KW - Reliability characteristic

KW - Spacecraft mechanism

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M3 - Article

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VL - 33

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EP - 391

JO - Yuhang Xuebao/Journal of Astronautics

JF - Yuhang Xuebao/Journal of Astronautics

IS - 3

ER -

Study on test method of reliability assessment used for performance parameter-measured spacecraft mechanism

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Keywords

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