DocumentCode
2315478
Title
Multi-LEO combined orbit determination modeling based on hybrid satellite constellation and nonlinear optimal estimation algorithm
Author
Zhao, Deyong ; Gao, Cuijuan ; Wu, Baojun ; Wang, Jiongqi
Author_Institution
Dept. of Manage. Eng., Ordnance Eng. Coll., Shijiazhuang, China
Volume
8
fYear
2010
fDate
10-12 Aug. 2010
Firstpage
4083
Lastpage
4087
Abstract
For multi-LEO combined orbit determination (COD) satellite-network based on space-based tracking telemetry and command (STTC) hybrid satellite constellation (HSC), if kinematic orbit information of low earth orbit (LEO) can be taken full advantage of participating in dynamic precise orbit determination (POD) and making them achieve best matching, integrative COD models based on kinematic and dynamic information can be constructed to realize dynamic smoothness of kinematic information. Firstly, multi-LEO COD models based on kinematic and dynamic information are constituted on base of analyzing the design method of STTC HSC and system composition of COD satellite-network. Then integrative COD models based on prior trajectory information considering nonlinear semi-parametric modeling of observation models errors and sparse parameters modeling of dynamic models were established, and the nonlinear optimal weighting estimation algorithm of multi-structural nonlinear COD models were designed. Theoretical analysis and simulation computation results show that COD nonlinear optimal weighting method based on prior trajectory information can realize LEOs dynamic information optimal matching with kinematic prior information, and can restrain nonlinear influence factor including measure models and ephemeris errors to the effects of POD precision by considering models errors modeling and dynamic models sparse parameters denotation.
Keywords
Earth orbit; artificial satellites; satellite communication; telemetry; COD satellite-network; hybrid satellite constellation; kinematic orbit information; kinematic prior information; low Earth orbit; multiLEO combined orbit determination; nonlinear influence factor; nonlinear optimal estimation algorithm; precise orbit determination; prior trajectory information; space-based tracking telemetry and command; Analytical models; Computational modeling; Heuristic algorithms; Kinematics; Low earth orbit satellites; Orbits; hybrid satellite constellation; integrative COD models; nonlinear optimal estimation1;
fLanguage
English
Publisher
ieee
Conference_Titel
Natural Computation (ICNC), 2010 Sixth International Conference on
Conference_Location
Yantai, Shandong
Print_ISBN
978-1-4244-5958-2
Type
conf
DOI
10.1109/ICNC.2010.5584868
Filename
5584868
Link To Document