DocumentCode
3055676
Title
Orbit determination via UD-filters
Author
Raol, J.R. ; Sinha, N.K.
Author_Institution
McMaster University, Hamilton, Ontario, Canada
fYear
1984
fDate
12-14 Dec. 1984
Firstpage
29
Lastpage
30
Abstract
The application of UD Filter (UDF) and UD-Filter-RTS Smoother (UDRS) to estimate the orbital states of a search and rescue satellite aided tracking (SARSAT) satellite is considered. Inertial co-ordinates´ six states (IC6) for the filter and Altman´s Unified State Model´s (USM)-seven states (U7) for the time propagation are used. The angles and range data simulated for groundbased tracking site are considered as observables. The UD algorithms performed with acceptable accuracy in satellite position estimation.
Keywords
Extraterrestrial measurements; Filters; Frequency measurement; Ground support; Instruments; Position measurement; Relays; Satellite broadcasting; Signal processing; State estimation;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1984. The 23rd IEEE Conference on
Conference_Location
Las Vegas, Nevada, USA
Type
conf
DOI
10.1109/CDC.1984.272245
Filename
4047827
Link To Document