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
Link To Document :
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