Open AccessAssembly Method for Satellite Propulsion System based on HoloLens
Author(s) -
Wei Zhang,
Jie Zhang,
Huajun Chen,
Bin Zhang,
Feng Liu,
Zhao Jing
Publication year - 2019
Publication title -
iop conference series. materials science and engineering
Language(s) - English
Resource type - Journals
eISSN - 1757-899X
pISSN - 1757-8981
DOI - 10.1088/1757-899x/608/1/012035
Subject(s) - propulsion , satellite , satellite system , process (computing) , computer science , mode (computer interface) , component (thermodynamics) , systems engineering , engineering , simulation , aerospace engineering , human–computer interaction , operating system , physics , gnss applications , thermodynamics
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.