DocumentCode :
792605
Title :
Euler angle transformations
Author :
Pio, Richard L.
Author_Institution :
Hughes Aircraft Company, Culver City, CA, USA
Volume :
11
Issue :
4
fYear :
1966
fDate :
10/1/1966 12:00:00 AM
Firstpage :
707
Lastpage :
715
Abstract :
The definition of sets of Euler angles is discussed and a useful tool for treating the mathematics associated with Euler angles is illustrated. Restricting attention to right-handed coordinate systems and positive rotations, twelve distinct but equivalent sets of Euler angles are partitioned into two subsets. The method of determining a set of orthogonal infinitesimal rotations equivalent to nonorthogonal infinitesimal increments on a set of Euler angles is illustrated. It is shown that the same solution yields expressions for the angular velocities of the final coordinate system relative to the reference coordinate system in terms of derivatives of the Euler angles. The ease with which the infinitesimal increments of one Euler set in terms of the increments of another equivalent Euler set can be determined by the symbolic technique is illustrated. This technique offers a systematic approach to error analysis of sequences of rotations.
Keywords :
Control system analysis; Aircraft; Angular velocity; Equations; Error analysis; Helium; Mathematics; Motion analysis; Space vehicles; Vehicle dynamics; Writing;
fLanguage :
English
Journal_Title :
Automatic Control, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9286
Type :
jour
DOI :
10.1109/TAC.1966.1098430
Filename :
1098430
Link To Document :
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