DocumentCode
3028288
Title
A selecting method in collision risk assessment
Author
Zhang, Rongzhi ; Zhou, Fengqi ; Wang, Xiuhong ; Wang, Xinfeng
Author_Institution
Northwestern Polytech. Univ., Xi´´an, China
fYear
2010
fDate
8-10 June 2010
Firstpage
841
Lastpage
844
Abstract
With the increase of space debris, the technology of spacecraft collision avoidance has become more and more important. In this paper, an analytical method of selecting objects is investigated based on mean elements, which is free from the restriction of the spacecraft launch time and the instantaneous position. If only the launch orbit of a spacecraft is known, this method can be used to select potential dangerous objects from thousands of space objects for several days before the launch window of the mission.
Keywords
collision avoidance; position control; risk management; space vehicles; collision risk assessment; instantaneous position; launch window; selecting method; space debris; space objects; spacecraft collision avoidance; spacecraft launch time; Collision avoidance; Filtering; Optimization; Orbits; Satellites; Space debris; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location
Harbin
Print_ISBN
978-1-4244-6043-4
Electronic_ISBN
978-1-4244-7505-6
Type
conf
DOI
10.1109/ISSCAA.2010.5632329
Filename
5632329
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