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