• DocumentCode
    9488
  • Title

    Generalized Formulation of Weighted Optimal Guidance Laws with Impact Angle Constraint

  • Author

    Chang-Hun Lee ; Min-jea Tahk ; Jin-Ik Lee

  • Author_Institution
    Dept. of Aerosp. Eng., Korea Adv. Inst. of Sci. & Technol. (KAIST), Daejeon, South Korea
  • Volume
    49
  • Issue
    2
  • fYear
    2013
  • fDate
    Apr-13
  • Firstpage
    1317
  • Lastpage
    1322
  • Abstract
    The generalized formulation of weighted optimal guidance laws with impact angle constraint is investigated here. From the generalized formulation, we explicitly find the feasible set of weighting functions that lead to analytical forms of weighted optimal guidance laws. This result has potential significance because it can provide additional degrees of freedom in designing a guidance law that accomplishes the specified guidance objective.
  • Keywords
    missile guidance; degrees of freedom; generalized formulation; impact angle constraint; weighted optimal guidance laws; weighting functions;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.2013.6494416
  • Filename
    6494416
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=9488