• DocumentCode
    1602895
  • Title

    Control of spinning flying vehicles utilizing partial body despin techniques

  • Author

    Salman, Mishah Uzziél ; Chang, Borchin ; Ilg, Mark Dean

  • Author_Institution
    Dept. of Mech. Eng., Drexel Univ., Philadelphia, PA, USA
  • fYear
    2009
  • Firstpage
    326
  • Lastpage
    331
  • Abstract
    Despinning the front end of a spinning flying munition is an important step towards flight control of said vehicle. A counter-rotation control scheme is proposed to despin and stabilize the front end of the vehicle at a definable still roll position with respect to earth. Classical and Hinfin control theories are employed to construct the despin controller.
  • Keywords
    Hinfin control; aircraft control; military systems; missile control; stability; Hinfin control; counter-rotation control scheme; flight control; missile control; partial body despin technique; roll position; spinning flying munition vehicle control; stabilization; Actuators; Aerodynamics; Control systems; Earth; Frequency; Missiles; Space technology; Spinning; Vehicle dynamics; Weapons;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Asian Control Conference, 2009. ASCC 2009. 7th
  • Conference_Location
    Hong Kong
  • Print_ISBN
    978-89-956056-2-2
  • Electronic_ISBN
    978-89-956056-9-1
  • Type

    conf

  • Filename
    5276252
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=1602895