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Coning compensation in strapdown inertial navigation systems

  • US 5,828,980 A
  • Filed: 07/01/1997
  • Issued: 10/27/1998
  • Est. Priority Date: 03/18/1996
  • Status: Expired due to Term
First Claim
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1. A coning compensation method for use in a strapdown inertial navigation system, the method utilizing the incremental angles of rotation of a coordinate system expressed as a vector Δ

  • Θ

    (k,n,m) and measured in successive time periods to obtain an estimate of the coning compensation for NK successive time periods, the vector Δ

    Θ

    (k,n,m) corresponding to the vector angle of rotation for the (mNK+nK+k)'"'"'th data sampling interval of duration T as provided by orthogonally mounted gyros in a body-fixed coordinate system, k taking on integer values from 1 to K, n taking on integer values from 1 to N, m taking on integer values, N and K being predetermined integers, the method comprising the steps;

    calculating R(h,m) for K equal to 5 and h equal to 1, 2, and 3, R(h,m) being the vector cross-product of the sum of U(h,k)Δ

    Θ

    (k,n,m) and the sum of V(h,k)Δ

    Θ

    (k,n,m), the sums being taken over all values of k and all values of n, U(h,k) and V(h,k) being predetermined numbers for all values of h and k;

    calculating R(m), R(m) being the sum of W(h)R(h,m) over all values of h, W(h) being a predetermined number for each value of h where h takes on the values 1, 2, and 3, the estimate of the coning compensation comprising R(m).

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