• DocumentCode
    2767589
  • Title

    Modern guidance laws via receding horizon control without the time-to-go

  • Author

    Kim, Ki Baek ; Kim, Myung-Joon ; Kwon, Wook Hyun

  • Author_Institution
    Dept. of Electr. Eng., Seoul Nat. Univ., South Korea
  • Volume
    4
  • fYear
    1998
  • fDate
    16-18 Dec 1998
  • Firstpage
    4202
  • Abstract
    A receding horizon guidance law (RHG) is proposed which is useful when the time-to-go is inaccurate or is unavailable, or the accurate time-to-go is difficult to estimate in a sampling time. In the presence of arbitrary target maneuvers and an initial lateral miss distance rate between the target and missile, it is shown that the proposed RHG can make lateral miss distance (MD) below the predescribed value in the prespecified time without the time-to-go. Through simulation, guidance performance of RHG is illustrated and RHG is compared with the optimal guidance law in terms of miss distance and missile acceleration
  • Keywords
    missile guidance; optimal control; arbitrary target maneuvers; lateral miss distance; missile acceleration; modern guidance laws; optimal guidance law; receding horizon control; Acceleration; Cost function; Ear; Jamming; Missiles; Navigation; Optimal control; Pollution measurement; Radar; Sampling methods;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1998. Proceedings of the 37th IEEE Conference on
  • Conference_Location
    Tampa, FL
  • ISSN
    0191-2216
  • Print_ISBN
    0-7803-4394-8
  • Type

    conf

  • DOI
    10.1109/CDC.1998.761962
  • Filename
    761962