• DocumentCode
    1945710
  • Title

    Modified strapdown inertial navigator error models

  • Author

    Scherzinger, Bruno M. ; Reid, D. Blake

  • Author_Institution
    Appl. Anal. Corp., Markham, Ont., Canada
  • fYear
    1994
  • fDate
    11-15 Apr 1994
  • Firstpage
    426
  • Lastpage
    430
  • Abstract
    The paper revisits the problem of error modeling for strapdown INS for the purpose of navigation sensor blending with a Kalman filter. This problem has been addressed repeatedly over the last 30 years, and different perspectives on INS error modeling have emerged. The paper reviews these, focussing in particular on the properties and relative advantages and disadvantages of the φ-angle and ψ-angle error models. The paper then addresses some new concepts for the design of a Kalman filter model for integrated navigation. The sometimes troublesome problem of the explicit occurrence of the specific force in both error models is averted with the modified φ-angle and ψ-angle error models proposed in the paper, in which the explicit representation of the specific force is canceled via a transformation of the velocity error states
  • Keywords
    Kalman filters; aircraft; error analysis; filtering and prediction theory; inertial navigation; φ-angle error models; ψ-angle error models; INS; Kalman filter; design; modified strapdown inertial navigator error models; navigation sensor blending; specific force; velocity error states; Acceleration; Accelerometers; Analytical models; Bandwidth; Computer errors; Earth; Error correction; Inertial navigation; State estimation; Vehicle dynamics;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Position Location and Navigation Symposium, 1994., IEEE
  • Conference_Location
    Las Vegas, NV
  • Print_ISBN
    0-7803-1435-2
  • Type

    conf

  • DOI
    10.1109/PLANS.1994.303345
  • Filename
    303345