• DocumentCode
    295183
  • Title

    An implementable high-order guidance law for homing missiles

  • Author

    Aggarwal, Romesh ; Boudreau, Daniel

  • Author_Institution
    Raytheon Electron. Syst., Raytheon Co., Tewksbury, MA, USA
  • Volume
    2
  • fYear
    1995
  • fDate
    13-15 Dec 1995
  • Firstpage
    1865
  • Abstract
    A high-order optimal guidance law for tactical missiles is derived using measurable/realizable states in its autopilot/airframe (AP/AF) plant model. This derivation yields a form of the guidance law that can be implemented in an operational missile system
  • Keywords
    missile guidance; optimal control; transfer functions; autopilot/airframe plant model; high-order guidance law; homing missiles; measurable/realizable states; tactical missiles; Acceleration; Accelerometers; Aerodynamics; Geometry; Missiles; Navigation; Optimal control; Stability; State-space methods; Transfer functions;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1995., Proceedings of the 34th IEEE Conference on
  • Conference_Location
    New Orleans, LA
  • ISSN
    0191-2216
  • Print_ISBN
    0-7803-2685-7
  • Type

    conf

  • DOI
    10.1109/CDC.1995.480614
  • Filename
    480614
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=295183