• DocumentCode
    1442045
  • Title

    Comments on "True proportional navigation with maneuvering target"

  • Author

    Rao, S.K.

  • Author_Institution
    Naval Sci. & Tech. Lab., Gov. of India Minist. of Defence, Vigyan Nagar, India
  • Volume
    33
  • Issue
    1
  • fYear
    1997
  • Firstpage
    273
  • Lastpage
    274
  • Abstract
    In the paper by D. Ghose (Jan. 1994), the author rightly pointed about the unrealistic target maneuvers considered by C.D. Yang et al. (1989) and by P.J. Yuan (1992) and he carried out the analysis for the target maneuver which is inversely proportional to the relative velocity component normal to the line of sight (LOs). This target maneuver is somewhat near to a realistic one, but still it suffers from one drawback. With this maneuver, the target pulls a high acceleration when the interceptor is on a collision course and a negligible acceleration when the LOS rate is already high. The author discusses realistic true proportional navigation (RTPN) because conventional true proportional navigation (TPN) is not used in actual scenario. The result is a third-order nonlinear equation.
  • Keywords
    missile guidance; navigation; nonlinear equations; target tracking; maneuvering target; missiles homing; proportional navigation; third-order nonlinear equation; Acceleration; Aerodynamics; Aerospace and electronic systems; Communication system control; Data communication; Differential equations; Navigation; Nonlinear equations; Sensor fusion; Target tracking;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/7.570778
  • Filename
    570778