The Application of Integrated Technique on the Control and Display Parts of Spacecraft

Abstract:

This paper introduced actuality and developing direction of manufacture technology in spacecraft base on the application of CAD/CAM integrated technique, described the integrated designing process according to the requirements that the control and display parts of spacecraft must meet the conditions of the resistance to mechanical environment, thermal, EMC, anti-radiation and process feasibility, presented the applied method on integrated technique based on Pro/E, and induced the working flow of CAD/CAM integrated technique in the control and display parts of spacecraft. This paper is helpful in pushing further study on the application of integrated technique in the control and display parts of spacecraft.

• Periodical: Applied Mechanics and Materials (Volumes 184-185)
• Pages: 1574-1577
• DOI: https://doi.org/10.4028/www.scientific.net/AMM.184-185.1574
• Online since: June 2012
• Authors: Cheng Bin Ding, Yin Ning
• Keywords: CAD/CAM Integrated Technique, Control of Spacecraft, Display Parts of Spacecraft

References

[1] Guofu Yin. Mechanical CAD/CAM Technique Elements[M]. Wuhan China: Huazhong University of Science an Technology Publishing Company. 2010: 1-6.

[2] Jianguo Zhang. The actuality and developing direction of manufacturing new technology on aircraft and spacecraft[J］. Jiangsu Aircraft. 2006, 4: 22-23.

[3] Mujber T.S. Virtual reality applications in manufacturing process simulation. Journal of Materials Processing Technology, 2004, 155: 1834-1838.

DOI: 10.1016/j.jmatprotec.2004.04.401