• DocumentCode
    1345392
  • Title

    The proportional navigation dilemma-pure or true?

  • Author

    Shukla, U.S. ; Mahapatra, P.R.

  • Author_Institution
    Dept. of Aerosp. Eng., Indian Inst. of Sci., Bangalore, India
  • Volume
    26
  • Issue
    2
  • fYear
    1990
  • fDate
    3/1/1990 12:00:00 AM
  • Firstpage
    382
  • Lastpage
    392
  • Abstract
    Two generic classes of proportional navigation (PN) laws are compared in detail. One class consists of pursuer-velocity-referenced systems, which include pure proportional navigation (PPN) and its variants; the second category consists of line-of-sight- (LOS-) referenced systems such as true proportional navigation (TPN), generalized true proportional navigation (GTPN), and generalized guidance laws. The existing closed-form solutions are discussed in detail, and the classical linear and quasilinear analytical solutions are summarized. A critical comparison is then made with regard to the definition, implementation, and analytical aspects of the guidance laws, including the method, the nature of solution, and an appraisal of the behavior of the pursuer motion resulting from the laws. It is established that, in spite of some restricted advantages in the solvability of the equations of motion, the LOS-referenced PN schemes suffer from serious limitations in terms of implementation and trajectory behavior. Among the major drawbacks are forward velocity variation requirement, relatively large control effort requirement, restrictions on initial engagement conditions to ensure intercept, lack of robustness, and possibility of unbounded acceleration. It is concluded that PPN is a better guidance law in a practical sense than TPN and its generalizations
  • Keywords
    missiles; navigation; closed-form solutions; guidance laws; line of sight referenced system; linear solution; pure proportional navigation; pursuer motion; pursuer-velocity-referenced systems; quasilinear analytical solutions; robustness; tactical guided missiles; true proportional navigation; unbounded acceleration; Acceleration; Appraisal; Closed-form solution; Force control; Missiles; Motion analysis; Navigation; Optical control; Proportional control; Velocity control;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/7.53445
  • Filename
    53445