• DocumentCode
    1301970
  • Title

    Performance Analysis of Guidance Laws Based on Timescale Gap

  • Author

    Dhananjay, Narayanachar ; Ghose, Debasish ; Bhat, M. Seetharama

  • Author_Institution
    Dept. of Aerosp. Eng., Indian Inst. of Sci., Bangalore, India
  • Volume
    18
  • Issue
    3
  • fYear
    2010
  • fDate
    5/1/2010 12:00:00 AM
  • Firstpage
    574
  • Lastpage
    590
  • Abstract
    An analytical treatment of performance analysis of guidance laws is possible only in simplistic scenarios. As the complexity of the guidance system increases, a search for analytical solutions becomes quite impractical. In this paper, a new performance measure, based upon the notion of a timescale gap that can be computed through numerical simulations, is developed for performance analysis of guidance laws. Finite time Lyapunov exponents are used to define the timescale gap. It is shown that the timescale gap can be used for quantification of the rate of convergence of trajectories to the collision course. Comparison between several guidance laws, based on the timescale gap, is presented. Realistic simulations to study the effect of aerodynamics and atmospheric variations on the timescale gap of these guidance laws are also presented.
  • Keywords
    Lyapunov methods; collision avoidance; differential geometry; game theory; missile guidance; nonlinear control systems; numerical analysis; collision course; finite time Lyapunov exponents; guidance laws analysis; numerical simulations; performance analysis; timescale gap; trajectory convergence rate; Guidance laws; nonlinear systems; proportional navigation; timescale gap;
  • fLanguage
    English
  • Journal_Title
    Control Systems Technology, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    1063-6536
  • Type

    jour

  • DOI
    10.1109/TCST.2009.2024534
  • Filename
    5208380