• DocumentCode
    485950
  • Title

    Symmetric Linear Systems

  • Author

    Lewis, John ; Martin, Clyde

  • Author_Institution
    Ames Research Center, NASA, Moffett Field, CA 94035
  • fYear
    1983
  • fDate
    22-24 June 1983
  • Firstpage
    1182
  • Lastpage
    1183
  • Abstract
    A major limitation to the use of helicopters in heavy construction has been that the masses that can be effectively and safely transported are restricted. One solution was the construction of the so-called heavy-lift helicopters. However it has been established that there are physical and economic limitations to the payload that can be transported. It has been proposed to circumvent this limitation by using multiple helicopters to move a single mass. The concept has been flight tested for two helicopters (twinlift) and the results were encouraging but showed that automatic control would be necessary to make the concept successful. In this paper the authors present some initial models and explore some of the control-theoretic problems inherent in the twinlift problem. A simplified linear model is examined, and it is shown that certain natural control schemes are not feasible, but that it is possible to control the linear model while preserving the essential characteristics of twinlift profile.
  • Keywords
    Aerodynamics; Automatic control; Automatic testing; Damping; Helicopters; Linear systems; Mathematics; Military aircraft; NASA; Payloads;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1983
  • Conference_Location
    San Francisco, CA, USA
  • Type

    conf

  • Filename
    4788294