• DocumentCode
    794367
  • Title

    Methods for injection-error analysis and their comparison

  • Author

    Irwin, John D. ; Hung, James C.

  • Author_Institution
    University of Tennessee, Knoxville, TN, USA
  • Volume
    12
  • Issue
    3
  • fYear
    1967
  • fDate
    6/1/1967 12:00:00 AM
  • Firstpage
    276
  • Lastpage
    281
  • Abstract
    Statistical techniques for the analysis of missile injection errors are studied in detail. The commonly used direct and adjoint methods are reviewed and extended. It is shown that the determination of the covariance matrix is equivalent to the determination of two transformation matrices for both methods. In general, the adjoint method is more efficient. But for a special case the direct method could be preferable depending upon the relative dimension of the system state and the error source. Two examples are given to verify the results. The techniques presented can be applied equally well to a wide variety of control system problems.
  • Keywords
    Linear systems, time-varying continuous-time; Missile guidance; Computer errors; Control systems; Covariance matrix; Engines; Fuels; Hardware; Milling machines; Missiles; Space vehicles; Uncertainty;
  • fLanguage
    English
  • Journal_Title
    Automatic Control, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9286
  • Type

    jour

  • DOI
    10.1109/TAC.1967.1098598
  • Filename
    1098598