• DocumentCode
    487294
  • Title

    Obstacles to High Fidelity Multibody Dynamics Simulation

  • Author

    Lips, K.W. ; Singh, R.P.

  • Author_Institution
    Honeywell, Inc. Space & Strategic Avionics Division, Clearwater, Florida
  • fYear
    1988
  • fDate
    15-17 June 1988
  • Firstpage
    587
  • Lastpage
    594
  • Abstract
    This study takes a wide ranging look at issues involved in the dynamic modeling of complex, multibodied orbiting space systems. The nature of the multibody problem is reviewed and capabilities and limitations of two major codes (DISCOS, TREETOPS) are assessed. Problem areas that limit accuracy or contribute to uncertainty in the modeling, simulation process are identified. As a specific case, the significance of including, or of not including, 2nd degree geometric nonlinearity in the elastic displacement field (foreshortening) is evaluated Conclusion and recommendations are made concerning the direction future development should take in order to achieve higher fidelity, more computationally efficient multibody software solutions.
  • Keywords
    Aerospace electronics; Antenna measurements; Control design; Equations; Extraterrestrial measurements; Lips; Physics; Sorting; Space vehicles; Spaceborne radar;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1988
  • Conference_Location
    Atlanta, Ga, USA
  • Type

    conf

  • Filename
    4789787