DocumentCode
783141
Title
Estimation of Rodrigues parameters from vector observations
Author
Idan, M.
Author_Institution
Fac. of Aerosp. Eng., Israel Inst. of Technol., Haifa, Israel
Volume
32
Issue
2
fYear
1996
fDate
4/1/1996 12:00:00 AM
Firstpage
578
Lastpage
586
Abstract
A recursive minimum variance algorithm for attitude determination is presented. The attitude is expressed by the Rodrigues vector, where only three parameters are needed to describe orientation. The advantage of using the Rodrigues parameters is computational. Attitude calculations involve only relatively simple algebraic expressions, which is advantageous especially in real-time applications. The efficiency of the derived algorithm is demonstrated using Monte-Carlo computer simulation results and in an initial alignment aerospace application.
Keywords
Monte Carlo methods; attitude control; recursive estimation; vectors; Monte-Carlo computer simulation; Rodrigues parameters; algebraic expressions; alignment aerospace application; attitude determination; orientation; recursive minimum variance algorithm; vector observations; Aerodynamics; Aerospace control; Aerospace engineering; Aircraft; Application software; Equations; Missiles; Parameter estimation; Position measurement; Quaternions; Recursive estimation;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/7.489502
Filename
489502
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