DocumentCode
1141804
Title
Attitude Determination Via Nonlinear Filtering
Author
Kau, S. ; Kumar, K.S.P. ; Granley, Gerald B.
Author_Institution
Department of Electrical Engineering University of Minnesota Minneapolis, Minn.
Issue
6
fYear
1969
Firstpage
906
Lastpage
911
Abstract
The theory of nonlinear filtering has been applied to the problem of the attitude determination of a satellite. Two approximation methods have been studied with a view to practical implementation. Computer simulation results are included.
Keywords
Acceleration; Computer simulation; Earth; Equations; Filtering theory; Geometry; Position measurement; Satellites; State estimation; Torque control;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1969.309965
Filename
4103421
Link To Document