The research of multi-satellite deploying method for upper stage
- Paper number
IAC-09.D2.3.13
- Author
Mr. junfeng wang, China Academy of Launch Vehicle Technology, China
- Coauthor
Mr. Lin Shen, China Academy of Launch Vehicle Technology, China
- Coauthor
Mr. Xie Zebing, China Academy of Launch Vehicle Technology, China
- Coauthor
Prof. Yang Jianmin, China
- Year
2009
- Abstract
This paper presents the orbit design method for deploying 4 MEO satellites in one orbit. Firstly, the multi-satellite deploying strategy with the theory of impulse maneuver is studied, and then the optimal energy saving scheme is achieved. During the detail design, the traditional design method in launch coordinate system or geocentric equatorial coordinate system is very complicated. Therefore, the orbit coordinate system is defined, and the kinetics equations in it are established as well. The result shows that the orbit coordinate system can greatly simplify the orbit design, and has significant reference to later spacecraft research.
- Abstract document
- Manuscript document
IAC-09.D2.3.13.pdf (🔒 authorized access only).
To get the manuscript, please contact IAF Secretariat.