• 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