Assembly precision prediction method for spacecraft based on 3D model

Wei Hu, Jian Hua Liu*, Ke Jiang, Chong Ying Guo

*此作品的通讯作者

科研成果: 期刊稿件文章同行评审

11 引用 (Scopus)

摘要

Aiming at the problem of assembly precision prediction for spacecraft, a new method based on 3D model was proposed. By summarizing the features of spacecraft assembly, the integrated assembly tolerance information model including assembly model, part model, structure model and tolerance model was constructed. Based on the construction of 3D model coordinate system, the tolerance variation effects of critical assembly node along with the tolerance variation transformation among different coordinate systems were analyzed. With the use of minimum deviation path, the deviation propagation path of spacecraft assembly was obtained and the prediction of the assembly precision was implemented by using extreme value method. Results from the tests on spacecraft section docking and equipment installation validated this new approach.

源语言英语
页(从-至)990-999
页数10
期刊Jisuanji Jicheng Zhizao Xitong/Computer Integrated Manufacturing Systems, CIMS
19
5
出版状态已出版 - 5月 2013

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