| 3rd International Conference on Aeronautical Materials and Aerospace Engineering | |
| Assembly Method for Satellite Propulsion System based on HoloLens | |
| 航空航天工程 | |
| Zhang, Wei^1 ; Zhang, Jie^1 ; Chen, Huajun^1 ; Zhang, Bin^1 ; Liu, Feng^1 ; Zhao, Jun^1 | |
| Beijing Institute of Spacecraft Environment Engineering, Beijing Engineering Research Center, Intelligent Assembly Technology and Equipment for Aerospace Product, Beijing, China^1 | |
| 关键词: Assembly modes; Computer stations; Digital assembly; Digital modes; Propulsion assembly; Propulsion system; Satellite designs; Satellite propulsion systems; | |
| Others : https://iopscience.iop.org/article/10.1088/1757-899X/608/1/012035/pdf DOI : 10.1088/1757-899X/608/1/012035 |
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| 学科分类:航空航天科学 | |
| 来源: IOP | |
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【 摘 要 】
As the satellite design changes from the traditional 2D mode to the 3D digital mode, the satellite assembly also enters the 3D assembly mode. An effective and accurate propulsion system assembly information transmission method from designers to operators is not formed, in the process of complex propulsion assembly, operators need to frequently confirm status back and forth between satellite and computer stations, and accidents with incorrect polarity in component installation often occur. In order to improve efficiency and quality of satellite propulsion system installation, a system based on HoloLens is designed. The successful application of this system provides a new solution for satellite propulsion system installation and marks a new step in the digital assembly capacity.
【 预 览 】
| Files | Size | Format | View |
|---|---|---|---|
| Assembly Method for Satellite Propulsion System based on HoloLens | 909KB |
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