• DocumentCode
    1177046
  • Title

    The Least-Square Approximation of Inertial Platform Drift

  • Author

    Danik, Boris

  • Author_Institution
    General Precision Aerospace Wayne, N. J.
  • Issue
    5
  • fYear
    1966
  • Firstpage
    591
  • Lastpage
    594
  • Abstract
    The drift angle of an inertial platform which is gyro-stabilized with respect to inertial space is equal to the integral of the gyro drift rate. Under controlled laboratory environment the drift angle, denoted by y, may be measured and plotted against time in an interval [0, T]. Without loss in generality, one may take y(0)= 0. A straight line yf can be found, such that the quantity E2 is minimized, where begin{equation*}E^2 = {frac{1}{T}int^{T}_{0}(y-y_f)^{2}}dt.end{equation*} The equation for yf is of the form yf = at + b and, in general, both a and b are nonzero. It is desirable to determine a statistical relationship between the gyro drift rate and the expected value of the minimum E2 for any given interval T. An analysis in this paper determines this relationship and derives a general expression for , where the symbol <*> denotes statistical expectation. It is found that increases linearly with the variance of the gyro drift rate. This general formula is then developed in detail for the case of a first-order Markovian gyro drift. is evaluated numerically and its square root plotted vs. the interval T and the gyro correlation time. The same problem is also solved for the case when yf is constrained to intersect the origin, i.e., when b=0.
  • Keywords
    Analytical models; Autocorrelation; Genetic expression; Integral equations; Loss measurement; Switches; Time measurement; Correlation; Markovian; gyro; inertial; least-square; nonstationary; orthonormal; platform;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.1966.4501936
  • Filename
    4501936