DocumentCode
536296
Title
Electromagnetic satellite cluster collision prediction and avoidance
Author
Su, Jianmin ; Dong, Yunfeng
Author_Institution
Astronaut. Acad., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
Volume
2
fYear
2010
fDate
29-31 Oct. 2010
Firstpage
767
Lastpage
770
Abstract
A two-spacecraft cluster in deep space collision prediction and avoidance is discussed in this paper, with double-integral model as dynamics model. Collision probability calculation is based on relative motion states and covariance matrix prediction. Collision avoidance mechanism, employing electromagnetic force as control force, distance and distance rate as feedback, will start when collision probability is beyond upper limit. Control law was designed by making use of Lyapunov method, aimed to avoid collision and make distance rate approach to zero.
Keywords
Lyapunov methods; artificial satellites; collision avoidance; covariance matrices; electromagnetic forces; feedback; integral equations; Lyapunov method; collision probability calculation; control force; covariance matrix prediction; double integral model; dynamics model; electromagnetic force; electromagnetic satellite cluster collision avoidance; electromagnetic satellite cluster collision prediction; feedback; two spacecraft cluster; Electromagnetics; Extraterrestrial measurements; Indium tin oxide; Position measurement; Predictive models;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Computing and Intelligent Systems (ICIS), 2010 IEEE International Conference on
Conference_Location
Xiamen
Print_ISBN
978-1-4244-6582-8
Type
conf
DOI
10.1109/ICICISYS.2010.5658625
Filename
5658625
Link To Document