• DocumentCode
    971843
  • Title

    Linear time-varying eigenstructure assignment with flight control application

  • Author

    Lee, Ho Chul ; Choi, Jae Weon

  • Author_Institution
    Sch. of Mech. Eng., Pusan Nat. Univ., South Korea
  • Volume
    40
  • Issue
    1
  • fYear
    2004
  • fDate
    1/1/2004 12:00:00 AM
  • Firstpage
    145
  • Lastpage
    157
  • Abstract
    This work is concerned with the assignment of a desired PD-eigenstructure for linear time-varying systems. Despite its well-known limitations, gain scheduling control appeared to be a focus of the research efforts. Scheduling of frozen-time, frozen-state controllers for fast time-varying dynamics is known to be mathematically fallacious, and practically hazardous. Therefore, recent research efforts are being directed towards applying time-varying controllers. In this paper we: 1) introduce a differential algebraic eigenvalue theory for linear time-varying systems; and 2) propose a PD-eigenstructure assignment scheme via a differential Sylvester equation and a command generator tracker (CGT) for linear time-varying systems. The PD-eigenstructure assignment is utilized as a regulator. A feedforward gain for tracking control is computed by using the command generator tracker. The whole design procedures of the proposed PD-eigenstructure assignment scheme are systematic in nature. The scheme could be used to determine the stability of linear time-varying systems easily as well as to provide a new horizon of designing controllers for the linear time-varying systems. A missile flight control application is presented to validate the proposed schemes.
  • Keywords
    aerospace control; eigenstructure assignment; feedforward; linear systems; missile control; time-varying systems; command generator tracker; differential Sylvester equation; differential algebraic eigenvalue theory; feedforward gain; gain scheduling control; linear time-varying eigenstructure assignment; missile flight control application; time-varying dynamics; tracking control; Acceleration; Aerospace control; Aircraft; Control systems; Differential equations; Dynamic scheduling; Eigenvalues and eigenfunctions; Missiles; Stability; Time varying systems;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.2004.1292149
  • Filename
    1292149