• DocumentCode
    1232750
  • Title

    Capturability of realistic generalized true proportional navigation

  • Author

    Chakravarthy, A. ; Ghose, D.

  • Author_Institution
    Flight Mechanics & Simulation Div., Aeronautical Dev. Agency, Bangalore, India
  • Volume
    32
  • Issue
    1
  • fYear
    1996
  • Firstpage
    407
  • Lastpage
    418
  • Abstract
    The capturability of a realistic generalized true proportional navigation (RGTPN) guidance law, against a nonmaneuvering target, is analyzed. The RGTPN law is obtained by relaxing the somewhat unrealistic assumption of constant closing velocity, made in all earlier studies on generalized true proportional navigation (GTPN), and incorporating the actual time-varying value in the guidance law. Closed-form solutions for the complete capture region of RGTPN is obtained in terms of both zero and acceptable non-zero miss distances. It is shown that the capture region of RGTPN in the initial relative velocity space is significantly smaller than that of GTPN, for reasonable values of navigation constant (N) and angular direction (η) of the missile commanded latax. However, for certain values of N and η, capturability of RGTPN is found to be better. It is also shown that if in one of the versions of GTPN, which uses constant values of both the closing velocity and the line-of-sight (LOS) angular velocity in the guidance law the corresponding realistic time-varying quantities are used, the capture region actually expands to cover the whole of the initial relative velocity space. A number of examples are given to compare the capture performance of RGTPN with other versions of the GTPN guidance laws.
  • Keywords
    control system analysis; missile guidance; proportional control; radar applications; radar tracking; radionavigation; time-varying systems; actual time-varying value; capturability; closed-form solutions; closing velocity; complete capture region; engagement model; guidance law; homing guidance; initial relative velocity space; line-of-sight angular velocity; missile commanded latax; nonmaneuvering target; realistic generalized true proportional navigation; tactical missiles; Aerospace simulation; Angular velocity; Closed-form solution; Inertial navigation; Missiles; Time varying systems; Velocity measurement;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/7.481281
  • Filename
    481281