• DocumentCode
    485774
  • Title

    Control Law Design and Dynamic Evaluations for a MAGLEV Vehicle with a Combined Lift and Guidance Suspension System

  • Author

    Kortum, W. ; Utzt, A.

  • Author_Institution
    DFVLR (German Aerospace Research Establishment), Institute for Flight Systems Dynamics, D-8031 Wessling, FRG
  • fYear
    1983
  • fDate
    22-24 June 1983
  • Firstpage
    276
  • Lastpage
    282
  • Abstract
    For a magnetically levitated vehicle (MAGLEV) with a combined lift and guidance system using u-shaped electro-magnets control law design based on simplified (design) models and dynamic simulations with more complex (evaluation models) are treated. It is demonstrated, that, even in view of the coupling of lateral (guidance) and vertical (lift) modes, caused by the inclined magnets, it is still possible to design the control law from a vertical model only. The control design is performed by quadratic synthesis (RICCATI design), because the given design specifications can be most easily translated into performance criteria of this type. The dynamic evaluations, which are carried through with a general purpose vehicle simulation program, show - with a minor extension for one lateral mode (yaw) - that above strategy yields good results meeting all dynamic specifications. Especially, the lateral response - not considered in the design - due to wind gusts is well damped and also the vertical response due to track irregularities and track flexibility is well behaved and stable.
  • Keywords
    Aerodynamics; Control systems; Feedback control; Magnetic levitation; Magnets; Navigation; Propulsion; Rails; Vehicle dynamics; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1983
  • Conference_Location
    San Francisco, CA, USA
  • Type

    conf

  • Filename
    4788115