• DocumentCode
    1600882
  • Title

    Modern control bank-to-turn autopilot for HAVE DASH II missile

  • Author

    Lee, K.L. ; Langehough, M.A. ; Chamberlain, R.A.

  • Author_Institution
    Boeing Co., Seattle, WA, USA
  • fYear
    1992
  • Firstpage
    214
  • Abstract
    The application of a modern control bank-to-turn autopilot to the HAVE DASH II air-to-air missile is addressed. The application of control techniques to an asymmetric airframe with highly nonlinear aerodynamic characteristics is discussed. Included are a summary of the mission and airframe concept, a discussion of the bank-to-turn control technique, a description of the aerodynamic characteristic, and resulting stability margins. Results of a six-degree-of-freedom simulation verification study are also shown
  • Keywords
    aerospace control; missiles; stability; HAVE DASH II air-to-air missile; asymmetric airframe; bank-to-turn autopilot; highly nonlinear aerodynamic characteristics; six-degree-of-freedom simulation verification study; stability margins; Actuators; Aerodynamics; Control systems; Force control; Missiles; Modems; Software testing; Stability; System testing; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Applications, 1992., First IEEE Conference on
  • Conference_Location
    Dayton, OH
  • Print_ISBN
    0-7803-0047-5
  • Type

    conf

  • DOI
    10.1109/CCA.1992.269874
  • Filename
    269874