• DocumentCode
    2839877
  • Title

    Integrated flight/fire control for attack helicopters

  • Author

    Osder, Stephen

  • Author_Institution
    McDonnell Douglas Helicopter Co., Mesa, AZ, USA
  • fYear
    1991
  • fDate
    14-17 Oct 1991
  • Firstpage
    287
  • Lastpage
    298
  • Abstract
    The author shows that integrated flight and fire control modes, analogous to those used in fixed-wing applications, can be implemented to enhance an attack helicopter´s air-to-air and air-to-ground combat effectiveness. With fly-by-wire active flight controls and state-of-the-art technology in target acquisition and tracking, integrated flight/fire control can increase firing opportunities, improve weapon accuracy and enhance survivability. Two typical applications are illustrated, using detailed simulations of the fly-by-wire controlled helicopter and associated weapons systems. The author also describes the avionics architecture needed to implement an integrated system and shows that it is achievable with a straightforward extension of designs already in place for advanced versions of the AH-64 aircraft
  • Keywords
    aerospace computer control; aircraft control; digital simulation; helicopters; military computing; military systems; weapons; AH-64 aircraft; air-to-air combat; air-to-ground combat effectiveness; attack helicopters; avionics architecture; fixed-wing applications; flight/fire control; fly-by-wire active flight controls; missile; simulations; survivability; target acquisition; tracking; weapon accuracy; Aerospace control; Aerospace electronics; Aircraft; Fires; Helicopters; Intelligent sensors; Missiles; Rockets; Turning; Weapons;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Avionics Systems Conference, 1991. Proceedings., IEEE/AIAA 10th
  • Conference_Location
    Los Angeles, CA
  • Type

    conf

  • DOI
    10.1109/DASC.1991.177182
  • Filename
    177182