• DocumentCode
    2086048
  • Title

    Dynamic conversion of flight path angle commands to body attitude commands

  • Author

    Cloutier, James R. ; Stansbery, Donald T.

  • Author_Institution
    Munitions Directorate, U.S. Air Force Res. Lab., Eglin AFB, FL, USA
  • Volume
    1
  • fYear
    2002
  • fDate
    2002
  • Firstpage
    221
  • Abstract
    A state-dependent Riccati equation based controller with integral servomechanism tracking is designed to convert flight path angle commands to angle-of-attack and bank angle commands for a bank-to-turn air vehicle. This problem is challenging because the controls are highly nonlinear, appearing in the dynamics as products of sines and cosines.
  • Keywords
    Riccati equations; aircraft navigation; attitude control; dynamics; military aircraft; servomechanisms; tracking; air vehicle; angle-of-attack; bank angle commands; dynamics; flight path angle commands; integral servomechanism; state-dependent Riccati equation; tracking; Aerodynamics; Attitude control; Force control; Integral equations; Laboratories; Military computing; Nonlinear equations; Vehicle dynamics; Vehicles; Weapons;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 2002. Proceedings of the 2002
  • ISSN
    0743-1619
  • Print_ISBN
    0-7803-7298-0
  • Type

    conf

  • DOI
    10.1109/ACC.2002.1024807
  • Filename
    1024807
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=2086048