概念设计中可重构航天器动特性快速预示方法

Da Wei Guo, Yuan Yuan He*, Zhen Jiang Yue, Jie Kang, Li Liu

*此作品的通讯作者

科研成果: 期刊稿件文章同行评审

13 引用 (Scopus)

摘要

To solve the problems of the reconfigurable spacecraft structural dynamic characteristics rapid evaluation considering contact and friction in conceptual design, a rapid predicting method is proposed. Based on the features of a typical reconfigurable spacecraft, the method uses the analysis and identification of dynamic characteristics, model equivalence based on virtual material, and estimation of equivalence data to form the processing flow, and realizes the equivalence of refined model. In the simulation verification, the proposed method is used to predict the structural dynamic characteristics of a conceptual design scheme, and under the premise of accuracy, the efficiency of analysis is improved. The results indicate that the proposed method can support the conceptual design and provide foundation for the iteration and optimization design of reconfigurable spacecraft.

投稿的翻译标题A Rapid Dynamic Characteristics Predicting Method of Reconfigurable Spacecraft in Conceptual Design
源语言繁体中文
页(从-至)1490-1498
页数9
期刊Yuhang Xuebao/Journal of Astronautics
41
12
DOI
出版状态已出版 - 30 12月 2020

关键词

  • Conceptual design
  • Rapid predicting method
  • Reconfigurable spacecraft
  • Structural dynamic characteristic

指纹

探究 '概念设计中可重构航天器动特性快速预示方法' 的科研主题。它们共同构成独一无二的指纹。

引用此