• DocumentCode
    821203
  • Title

    An optimal terminal guidance law

  • Author

    Nazaroff, Gregory J.

  • Author_Institution
    Aeronautic Ford, Newport Beach, CA, USA
  • Volume
    21
  • Issue
    3
  • fYear
    1976
  • fDate
    6/1/1976 12:00:00 AM
  • Firstpage
    407
  • Lastpage
    408
  • Abstract
    An optimal terminal guidance law is derived using linear optimal control theory.
  • Keywords
    Interception problems; Linear systems, time-varying continuous-time; Missile guidance; Optimal control; Acceleration; Aerodynamics; Automatic control; Computer vision; Differential equations; Geometry; Missiles; Optimal control; Proportional control; State estimation;
  • fLanguage
    English
  • Journal_Title
    Automatic Control, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9286
  • Type

    jour

  • DOI
    10.1109/TAC.1976.1101212
  • Filename
    1101212
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=821203