• DocumentCode
    2983509
  • Title

    Aeroelastic interactions with flight control of transatmospheric vehicles

  • Author

    Swaim, R.L.

  • Author_Institution
    Oklahoma State Univ., Stillwater, OK, USA
  • fYear
    1988
  • fDate
    23-27 May 1988
  • Firstpage
    574
  • Abstract
    The research needed on structural dynamics interactions with digital body dynamics and stability augmentation systems to allow confidence in vehicle design are discussed. This includes high-temperature-gradient effects on two- and three-dimensional total-vehicle elastic mode shapes and natural frequencies; robust control laws tolerant of wide uncertainties in elastic mode data; and compatible mathematical models for dynamic analysis of structures exhibiting low-frequency shell-type elastic modes. The expected use of metal matrix and carbon-carbon composite materials and ceramics with internally circulated cooling fluid will greatly complicate proper modeling and analysis of these interactions
  • Keywords
    aerospace control; stability; ceramics; composite materials; digital body dynamics; elastic mode data; flight control; high-temperature-gradient effects; internally circulated cooling fluid; low-frequency shell-type elastic modes; natural frequencies; robust control laws; stability augmentation systems; structural dynamics interactions; total-vehicle elastic mode shapes; transatmospheric vehicles; vehicle design; Aerodynamics; Aerospace control; Frequency; Mathematical model; Robust control; Shape control; Stability; Uncertainty; Vehicle dynamics; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace and Electronics Conference, 1988. NAECON 1988., Proceedings of the IEEE 1988 National
  • Conference_Location
    Dayton, OH
  • Type

    conf

  • DOI
    10.1109/NAECON.1988.195064
  • Filename
    195064