• DocumentCode
    326863
  • Title

    Recovery guidance for linear systems with input and state constraints

  • Author

    Devasia, Santosh ; Meyer, George

  • Author_Institution
    Dept. of Mech. Eng., Utah Univ., Salt Lake City, UT, USA
  • Volume
    2
  • fYear
    1998
  • fDate
    21-26 Jun 1998
  • Firstpage
    1122
  • Abstract
    When a fixed regulator is used to stabilize a desired state trajectory (guidance law), large initial tracking errors can lead to input saturation, which can result in performance deterioration. A method to modify the guidance law for recovering state-trajectory tracking (without violating input and state constraints) is presented. Although it may be feasible to find such a satisfactory recovery guidance manoeuvre for a given initial tracking error, online development of recovery guidance manoeuvres may not be computationally tractable. A technique is developed to use precomputed recovery guidance manoeuvres (for a finite set of initial tracking errors) to generate recovery guidance manoeuvres for other initial errors
  • Keywords
    aircraft navigation; feedback; feedforward; linear systems; optimal control; tracking; aircraft guidance; feedback; feedforward; initial errors; linear systems; optimal control; recovery guidance; state constraints; state-trajectory tracking; tracking errors; Actuators; Automatic generation control; Control systems; Error correction; Feedback; Linear systems; Mechanical engineering; NASA; Regulators; Trajectory;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1998. Proceedings of the 1998
  • Conference_Location
    Philadelphia, PA
  • ISSN
    0743-1619
  • Print_ISBN
    0-7803-4530-4
  • Type

    conf

  • DOI
    10.1109/ACC.1998.703586
  • Filename
    703586