1–10 von 28 Ergebnissen
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    Application of velocity-based gain-scheduling to lateral auto-pilot design for an agile missile

    Leith, D.J. / Tsourdos, A. / White, B.A. et al. | Tema Archiv | 2001

    Robust augmented lateral acceleration flight control design for a quasi-linear parameter-varying missile

    Bruyere, L / Tsourdos, A / White, B A | SAGE Publications | 2005

    Robust Analysis for Missile Lateral Acceleration Control Using Finite Inclusion Theorem

    Bruyère, L. | Online Contents | 2005
    Beteiligte: Tsourdos, A.

    Differential Geometric Guidance Based on the Involute of the Target's Trajectory

    Ariff, O. | Online Contents | 2005
    Beteiligte: Tsourdos, A.

    Fuzzy gain-scheduled missile autopilot design using evolutionary algorithms

    Screenuch, T. / Tsourdos, A. / Hughes, E.J. et al. | IEEE | 2006

      Fuzzy Gain-Scheduled Missile-Autopilot Design using Evolutionary Algorithms

      Screenuch, T. | Online Contents | 2006
      Beteiligte: Tsourdos, A.

    Direct Intercept Guidance using Differential Geometry Concepts

    White, B.A. / Zbikowski, R. / Tsourdos, A. | IEEE | 2007

    Missile autopilot design using quasi-LPV polynomial eigenstructure assignment

    White, B.A. / Bruyere, L. / Tsourdos, A. | IEEE | 2007

      Missile Autopilot Design using Quasi-LPV Polynomial Eigenstructure Assignment

      White, B.A. | Online Contents | 2007
      Beteiligte: Tsourdos, A.

    Fuzzy logic consequent perturbation analysis for electric vehicles

    Economou, J T / Tsourdos, A / White, B A | SAGE Publications | 2007

      Fuzzy logic consequent perturbation analysis for electric vehicles

      Economou, J. | Online Contents | 2007
      Beteiligte: Tsourdos, A.