• DocumentCode
    114267
  • Title

    Generalized optimal midcourse guidance

  • Author

    Morgan, Robert W. ; Noseck, Aaron P.

  • Author_Institution
    Raytheon Missile Syst., Tucson, AZ, USA
  • fYear
    2014
  • fDate
    15-17 Dec. 2014
  • Firstpage
    260
  • Lastpage
    264
  • Abstract
    This work addresses guiding a missile during the midcourse phase of flight. In particular, it is assumed the missile has the goal of arriving at a (possibly moving) target at a specified terminal flight path angle. A family of new guidance laws are derived that will allow the designer more flexibility to meet specific mission objectives.
  • Keywords
    missile guidance; optimal control; generalized optimal midcourse guidance; missile guidance; specific mission objectives; specified terminal flight path angle; Cost function; Geometry; Missiles; Optimal control; Polynomials; Vectors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control (CDC), 2014 IEEE 53rd Annual Conference on
  • Conference_Location
    Los Angeles, CA
  • Print_ISBN
    978-1-4799-7746-8
  • Type

    conf

  • DOI
    10.1109/CDC.2014.7039391
  • Filename
    7039391
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=114267