Calculation of Angular Variation of Spacecraft Assembly Considering Measurement Uncertainty

Jing Zhao Yang; Guo Xi Li; Bao Zhong Wu

doi:10.4028/www.scientific.net/AMM.457-458.1058

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 457-458Calculation of Angular Variation of Spacecraft...

Calculation of Angular Variation of Spacecraft Assembly Considering Measurement Uncertainty

Abstract:

The present studies of assembly accuracy predicting for complex products are mainly oriented to the early design stage. The final product assembly accuracy is computed using a variation propagation model, which is constructed based on design tolerance model and assembly model. Generally, the solving results are quite different with the actual values. In this paper, the axis angular variation calculation of the spacecraft cabin at the assembly phase was studied. And a novel analysis method for assembly variation was proposed with the consideration of measurement uncertainty of the key characteristics. An example was studied to illustrate and demonstrate the feasibility of the proposed method.

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Periodical:

Applied Mechanics and Materials (Volumes 457-458)

Pages:

1058-1063

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.457-458.1058

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Online since:

October 2013

Authors:

Jing Zhao Yang*, Guo Xi Li, Bao Zhong Wu

Keywords:

Assembly Variation, Key Characteristic, Measurement Uncertainty

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References

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