• DocumentCode
    2478245
  • Title

    2H Singularity-Free Momentum Generation with Non-Redundant Single Gimbaled Control Moment Gyroscopes

  • Author

    Sands, Timothy A. ; Kim, Jae Jun ; Agrawal, Brij

  • Author_Institution
    Naval Postgraduate Sch., Monterey, CA
  • fYear
    2006
  • fDate
    13-15 Dec. 2006
  • Firstpage
    1551
  • Lastpage
    1556
  • Abstract
    Two objectives dominate consideration of control moment gyroscopes (CMGs) for spacecraft maneuvers: high torque (equivalently momentum) and singularity-free operations. This paper adds to the significant body of research towards these two goals utilizing a minimal 3-CMG array to provide 646% singularity-free momentum performance increase spherically, compared to the ubiquitous pyramid arrangement skewed at 54.73deg. Spherical 1H (1 CMGs-worth momentum) singularity free momentum is established with birectional 1H and 2H in the third direction in a baseline configuration. Lastly, momentum space reshaping is shown via mixed skew angles. These claims are demonstrated analytically, then heuristically, and finally validated experimentally
  • Keywords
    gyroscopes; motion control; space vehicles; 2H singularity-free momentum generation; control moment gyroscopes; spacecraft maneuvers; Actuators; Aerospace engineering; Design optimization; Equations; Gyroscopes; Optimal control; Space vehicles; Torque control; USA Councils; Wheels;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 2006 45th IEEE Conference on
  • Conference_Location
    San Diego, CA
  • Print_ISBN
    1-4244-0171-2
  • Type

    conf

  • DOI
    10.1109/CDC.2006.377310
  • Filename
    4177743