TY - JOUR
T1 - 概念设计中可重构航天器动特性快速预示方法
AU - Guo, Da Wei
AU - He, Yuan Yuan
AU - Yue, Zhen Jiang
AU - Kang, Jie
AU - Liu, Li
N1 - Publisher Copyright:
© 2020, Editorial Dept. of JA. All right reserved.
PY - 2020/12/30
Y1 - 2020/12/30
N2 - 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.
AB - 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.
KW - Conceptual design
KW - Rapid predicting method
KW - Reconfigurable spacecraft
KW - Structural dynamic characteristic
UR - http://www.scopus.com/inward/record.url?scp=85099285881&partnerID=8YFLogxK
U2 - 10.3873/j.issn.1000-1328.2020.12.002
DO - 10.3873/j.issn.1000-1328.2020.12.002
M3 - 文章
AN - SCOPUS:85099285881
SN - 1000-1328
VL - 41
SP - 1490
EP - 1498
JO - Yuhang Xuebao/Journal of Astronautics
JF - Yuhang Xuebao/Journal of Astronautics
IS - 12
ER -