DocumentCode
483328
Title
Satellite Orbit Determination Based on StahelDonoho Kernel Estimator
Author
Xiaogang Pan ; Haiyin Zhou
Author_Institution
Sch. of Sci., Nat. Univ. of Defense Technol., Changsha
fYear
2009
fDate
23-25 Jan. 2009
Firstpage
867
Lastpage
871
Abstract
Dynamic model error and observation model error was the main factor to badly pollute the precision of orbit determination, especially in space based observation. Model error compensation technology was researched by designing semi-parametric orbit determination regression model. Stahel-Donoho Kernel estimator was applied to solve the semi-parametric model, which can effectively estimate the model error and restrain the gross error. Simulation Experiments was processed under space based surveillance system, and results proved that the Stahel-Donoho Kernel estimator can improve the precision of orbit determination largely.
Keywords
artificial satellites; error analysis; error compensation; surveillance; Stahel-Donoho kernel estimator; dynamic model error; model error compensation; observation model error; satellite orbit determination; space based surveillance system; Data mining; Error compensation; Extraterrestrial measurements; Kernel; Pollution measurement; Predictive models; Satellites; Solid modeling; Space technology; Surveillance; determination; model error compensation; semi-parametric regression model; stahel-donoho kernel estimator;
fLanguage
English
Publisher
ieee
Conference_Titel
Knowledge Discovery and Data Mining, 2009. WKDD 2009. Second International Workshop on
Conference_Location
Moscow
Print_ISBN
978-0-7695-3543-2
Type
conf
DOI
10.1109/WKDD.2009.225
Filename
4772072
Link To Document