• DocumentCode
    3592671
  • Title

    Nonlinear Flutter Analysis of a Missile Fin/Actuator

  • Author

    Girard, Donald D.

  • Author_Institution
    Raytheon Company, Missile Systems Division, Bedford, Massachusetts 01730
  • fYear
    1986
  • Firstpage
    1137
  • Lastpage
    1142
  • Abstract
    An analysis method based on simulation in the time and frequency domain is described for analyzing flutter of a missile fin actuator in the presence of nonlinearities. The method is illustrated by applying it to a hydraulic actuator with backlash and to a pneumatic actuator having nonlinear gas dynamics. All the work was done through computer simulation using the higher order language, ACSL (Reference 1).
  • Keywords
    Analytical models; Computational modeling; Computer simulation; Costs; Fires; Frequency domain analysis; Hydraulic actuators; Missiles; Pneumatic actuators; Stress;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1986
  • Type

    conf

  • Filename
    4789104
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=3592671