DocumentCode :
2628095
Title :
Evaluation of acceleration and motion model parameters from IGS final orbits
Author :
Ushakov, Yu.
Author_Institution :
Siberian Fed. Univ., Krasnoyarsk, Russia
fYear :
2013
fDate :
12-13 Sept. 2013
Firstpage :
1
Lastpage :
2
Abstract :
Given an IGS final orbit of a space vehicle, we evaluate its acceleration using numerical differentiation. Its precision turns out to be sufficient to estimate the parameters of radiation pressure models.
Keywords :
acceleration; artificial satellites; celestial mechanics; satellite navigation; IGS final orbits; acceleration model parameter; motion model parameter; numerical differentiation; radiation pressure model; space vehicle; Earth; Sun; least squares problem; numerical differentiation; radiation pressure force; space vehicle;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Communications (SIBCON), 2013 International Siberian Conference on
Conference_Location :
Krasnoyarsk
Print_ISBN :
978-1-4799-1060-1
Type :
conf
DOI :
10.1109/SIBCON.2013.6693594
Filename :
6693594
Link To Document :
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