• DocumentCode
    2650195
  • Title

    Spherical target state estimators

  • Author

    Souza, Christopher N D´ ; McClure, Mark A. ; Cloutier, James R.

  • Author_Institution
    Navigation and Control Branch, US Air Force Armament Directorate, Eglin AFB, FL, USA
  • Volume
    2
  • fYear
    1994
  • fDate
    29 June-1 July 1994
  • Firstpage
    1675
  • Abstract
    A spherical filter formulation is derived and the resulting nonlinear estimator is applied to a tactical air-to-air missile intercept problem. An Extended Kalman filter is used to estimate the target acceleration in the line-of-sight frame. The estimator models the target acceleration as a first-order Gauss-Markov process. A method suggested by Singer was used to select the process noise power spectral density matrix. Next, a kinematic constraint is used to improve the estimated target acceleration by using a fictitious measurement to augment the seeker measurements. Finally, a form of adaptive filtering is used to obtain a better value for the target acceleration time constant. These techniques are evaluated using a representative target engagement scenario.
  • Keywords
    Gaussian processes; Markov processes; adaptive Kalman filters; kinematics; missile guidance; state estimation; adaptive filtering; extended Kalman filter; first-order Gauss-Markov process; kinematic constraint; line-of-sight frame; noise power spectral density matrix; nonlinear estimator; spherical filter; tactical air-to-air missile intercept; target acceleration estimation; Acceleration; Accelerometers; Filters; Force control; Kinematics; Missiles; Motion estimation; Navigation; Nonlinear equations; State estimation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1994
  • Print_ISBN
    0-7803-1783-1
  • Type

    conf

  • DOI
    10.1109/ACC.1994.752356
  • Filename
    752356