Space Targets Collision Probability Model
- DOI
- 10.2991/icmmct-17.2017.57How to use a DOI?
- Keywords
- PDF;Collision Probability;Circle Domain Integral
- Abstract
The existence of space debris limits the development of the modern space industry.So it is necessary to study space targets collision probability.Collision probability Pc can be simplified as two-dimension unequal variances PDF[2] within circle domain integral by coordinate transformation and projection error .The integral can be turned into PDF within circle domain integral through the compression space and area circular approximation, and it can be a form of infinite series whose the first term and the recurrence formula are known .Finally,we use instance( U.S.and Russian satellite collision probability in a circular orbit) to explicit expression for validation,and the results show that the method is feasible.
- Copyright
- © 2017, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - QingGuo Zhou PY - 2017/04 DA - 2017/04 TI - Space Targets Collision Probability Model BT - Proceedings of the 2017 5th International Conference on Machinery, Materials and Computing Technology (ICMMCT 2017) PB - Atlantis Press SP - 280 EP - 283 SN - 2352-5401 UR - https://doi.org/10.2991/icmmct-17.2017.57 DO - 10.2991/icmmct-17.2017.57 ID - Zhou2017/04 ER -