摘要
In order to give full play to the advantages of innovation in the conceptual design stage, and to satisfy the dual constraints of geometry and performance for the reconfigurable spacecraft, a conceptual design method of reconfigurable spacecraft based on visualization model is proposed. The architecture with openness and extensibility of the conceptual design platform was given, and the platform was built with high-reality interactive interface and rapid performance evaluation function, which can realize the assembly of different configurations of reconfigurable spacecraft. The computational example shows that the proposed conceptual design method can meet the conceptual design requirements of reconfigurable spacecraft, and the developed platform can provide conditions for the conceptual design scheme argumentation of reconfigurable spacecraft.
投稿的翻译标题 | Conceptual design method of reconfigurable spacecraft based on visualization model |
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源语言 | 繁体中文 |
页(从-至) | 1405-1411 |
页数 | 7 |
期刊 | Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics |
卷 | 46 |
期 | 7 |
DOI | |
出版状态 | 已出版 - 1 7月 2020 |
关键词
- Conceptual design
- Performance evaluation
- Reconfigurable spacecraft
- Satellite design
- Visualization