Claims
- 1. A method for updating the attitude of a body by utilizing a plurality of gyros to measure as a function of time the angular rate vector or the integrated angular rate vector for the body, the method comprising the steps:obtaining measured values of the angular rate vector at a plurality of readout intervals; obtaining a smoothed value of each of one or more smoothed representations of the angular rate vector at the end of each of a plurality of smoothing intervals, a smoothed representation being a weighted sum of the measured values obtained during a smoothing interval, at least one of the weights for at least one of the smoothed representations being different from the other weights for the same smoothed representation, the ratio of the smoothing interval to the readout interval being an integer N; obtaining the updated attitude of the body at the end of an update interval by utilizing the attitude at the beginning of the update interval and the smoothed values of the smoothed representations of the angular rate vector obtained during the update interval, the ratio of the update interval to the smoothing interval being an integer M.
- 2. The method of claim 1 wherein the angular rate vector is represented within an update interval by a power series in time measured from the beginning of the update interval, the q'th vector coefficient being the vector coefficient of the q'th power of time, the q'th vector coefficient being proportional to the q'th derivative of the angular rate vector evaluated at the beginning of the update interval, q taking on integer values beginning with zero, the estimated q'th vector coefficient being a weighted sum of the smoothed values obtained during the update interval.
- 3. The method of claim 1 wherein the attitude is updated at the end of an update interval by applying a rotation vector to the attitude at the end of the prior update interval, the rotation vector being a weighted sum of (1) a plurality of the smoothed values and (2) the values of a plurality of cross-products of the smoothed values, the smoothed values having been obtained during the update interval.
- 4. The method of claim 1 wherein smoothed values of a plurality of smoothed representations of the angular rate vector are obtained for each smoothing interval, the smoothing interval being equal to the update interval.
- 5. The method of claim 4 wherein the step of obtaining a smoothed value comprises the steps:summing the first n measured values of the angular rate vector in a smoothing interval to obtain the n'th value of a first smoothed representation of the angular rate vector, n taking on integer values from 1 to N, the N'th value of the first smoothed representation being the smoothed value of the first smoothed representation; summing the first n values of the (k−1)'th smoothed representation of the angular rate vector to obtain the n'th value of an k'th smoothed representation of the angular rate vector, k being an integer greater than 1, the N 'th value of the k'th smoothed representation being the smoothed value of the k'th smoothed representation.
- 6. The method of claim 5 wherein the number of smoothed representations is 3 and the attitude is updated at the end of an update interval by applying a rotation vector to the attitude at the end of the prior update interval, the rotation vector being a weighted sum of the smoothed values, a first cross-product, a second cross-product, and a third cross-product, the first cross-product being the cross product of the smoothed values of the first and second smoothed representations, the second cross-product being the cross product of the smoothed values of the first and third smoothed representations, the third cross-product being the cross product of the smoothed values of the second and third smoothed representations, the weight of each smoothed value, the first cross-product, the second cross-product, and the third cross-product being proportional respectively to 1/(update interval), −3/N, 6/N2, and −12/N3.
- 7. The method of claim 4 wherein the angular rate vector is represented within an update interval by a power series in time measured from the beginning of the update interval, the q'th vector coefficient being the vector coefficient of the q'th power of time, the q'th vector coefficient being proportional to the q'th derivative of the angular rate vector evaluated at the beginning of the update interval, q taking on integer values beginning with zero, the estimated q'th vector coefficient being a weighted sum of the smoothed values of a plurality of smoothed representations of the angular rate vector obtained during the smoothing interval.
- 8. The method of claim 4 wherein the attitude is updated at the end of an update interval by applying a rotation vector to the attitude at the end of the prior update interval, the rotation vector being a weighted sum of (1) a plurality of the smoothed values and (2) the values of a plurality of cross-products of the smoothed values, the smoothed values having been obtained during the update interval.
- 9. The method of claim 1 wherein a single smoothed value from a single smoothed representation of the angular rate vector is obtained during each smoothing interval.
- 10. The method of claim 9 wherein the angular rate vector is represented within an update interval by a power series in time measured from the beginning of the update interval, the q'th vector coefficient being the vector coefficient of the q'th power of time, the q'th vector coefficient being proportional to the q'th derivative of the angular rate vector evaluated at the beginning of the update interval, q taking on integer values beginning with zero, the estimated q'th vector coefficient being a weighted sum of the smoothed values obtained during the update interval.
- 11. The method of claim 9 wherein the attitude is updated at the end of an update interval by applying a rotation vector to the attitude at the end of the prior update interval, the rotation vector being a weighted sum of (1) a plurality of the smoothed values and (2) the values of a plurality of cross-products of the smoothed values, the smoothed values having been obtained during the update interval.
- 12. The method of claim 11 wherein the number of smoothed representations is 1 and the attitude is updated at the end of an update interval by applying a rotation vector to the attitude at the end of the prior update interval, the rotation vector being a weighted sum of the smoothed values S (m) and the cross-products of the smoothed values S (m)×S (m+p), the index m denoting the associated smoothing interval and taking on values from 1 to N−1, the index p taking on values from 1 to N−m, the weights applied to each smoothed value and to each cross-product being proportional respectively to 1 and X(p), the weight X(p) being independent of m.
- 13. The method of claim 12 wherein N equals 2 and X(1) equals 3/4.
- 14. The method of claim 12 wherein N equals 3, X(1) equals 124/80, and X(2) equals 33/80.
- 15. The method of claim 12 wherein N equals 4, X(1) equals 17909/7560, X(2) equals 5858/7560, and X(3) equals 3985/7560.
- 16. The method of claim 12 wherein N equals 5, X(1) equals 193356/60480, X(2) equals 66994/60480, X(3) equals 65404/60480, and X(4) equals 29761/60480.
- 17. An apparatus for practicing the method of claim 1.
- 18. An apparatus for updating the attitude of a body by converting gyro measurements of the angular rate vector or the integrated angular rate vector of a body during an update interval into a change of attitude of the body during the update interval, the apparatus comprising:an interface processor for obtaining measured values of the angular rate vector at a plurality of readout intervals; a smoothing processor for obtaining a smoothed value of each of one or more smoothed representations of the angular rate vector at the end of each of a plurality of smoothing intervals, a smoothed representation being a weighted sum of the measured values obtained during a smoothing interval, at least one of the weights for at least one of the smoothed representations being different from the other weights for the same smoothed representation, the ratio of the smoothing interval to the readout interval being an integer N; an updating processor for obtaining the updated attitude of the body at the end of an update interval by utilizing the attitude at the beginning of the update interval and the smoothed values of the smoothed representations of the angular rate vector obtained during the update interval, the ratio of the update interval to the smoothing interval being an integer.
- 19. The apparatus of claim 18 wherein the angular rate vector is represented within an update interval by a power series in time measured from the beginning of the update interval, the q'th vector coefficient being the vector coefficient of the q'th power of time, the q'th vector coefficient being proportional to the q'th derivative of the angular rate vector evaluated at the beginning of the update interval, q taking on integer values beginning with zero, the estimated q'th vector coefficient being a weighted sum of the smoothed values obtained during the update interval.
- 20. The apparatus of claim 18 wherein the updating processor updates the attitude at the end of an update interval by applying a rotation vector to the attitude at the end of the prior update interval, the rotation vector being a weighted sum of (1) a plurality of the smoothed values and (2) the values of a plurality of cross-products of the smoothed values, the smoothed values having been obtained during the update interval.
- 21. The apparatus of claim 18 wherein the smoothing processor obtains smoothed values of a plurality of smoothed representations of the angular rate vector for each smoothing interval, the smoothing interval being equal to the update interval.
- 22. The apparatus of claim 21 wherein the smoothing processor performs the operations:summing the first n measured values of the angular rate vector in a smoothing interval to obtain the n'th value of a first smoothed representation of the angular rate vector, n taking on integer values from 1 to N, the N'th value of the first smoothed representation being the smoothed value of the first smoothed representation; summing the first n values of the (k−1)'th smoothed representation of the angular rate vector to obtain the n'th value of a k'th smoothed representation of the angular rate vector, k being an integer greater than 1, the N'th value of the k'th smoothed representation being the smoothed value of the k'th smoothed representation.
- 23. The apparatus of claim 21 wherein the angular rate vector is represented within an update interval by a power series in time measured from the beginning of the update interval, the q'th vector coefficient being the vector coefficient of the q'th power of time, the q'th vector coefficient being proportional to the q'th derivative of the angular rate vector evaluated at the beginning of the update interval, q taking on integer values beginning with zero, the estimated q'th vector coefficient being a weighted sum of the smoothed values of a plurality of smoothed representations of the angular rate vector obtained during the smoothing interval.
- 24. The apparatus of claim 21 wherein the updating processor updates the attitude at the end of an update interval by applying a rotation vector to the attitude at the end of the prior update interval, the rotation vector being a weighted sum of (1) a plurality of the smoothed values and (2) the values of a plurality of cross-products of the smoothed values, the smoothed values having been obtained during the update interval.
- 25. The apparatus of claim 18 wherein the smoothing processor obtains a single smoothed value from a single smoothed representation of the angular rate vector during each smoothing interval.
- 26. The apparatus of claim 25 wherein the angular rate vector is represented within an update interval by a power series in time measured from the beginning of the update interval, the q'th vector coefficient being the vector coefficient of the q'th power of time, the q'th vector coefficient being proportional to the q'th derivative of the angular rate vector evaluated at the beginning of the update interval, q taking on integer values beginning with zero, the estimated q'th vector coefficient being a weighted sum of the smoothed values obtained during the update interval.
- 27. The apparatus of claim 25 wherein the updating processor updates the attitude at the end of an update interval by applying a rotation vector to the attitude at the end of the prior update interval, the rotation vector being a weighted sum of (1) a plurality of the smoothed values and (2) the values of a plurality of cross-products of the smoothed values, the smoothed values having been obtained during the update interval.
- 28. The apparatus of claim 27 wherein the number of smoothed representations is 1 and the attitude is updated at the end of an update interval by applying a rotation vector to the attitude at the end of the prior update interval, the rotation vector being a weighted sum of the smoothed values S(m) and the cross-products of the smoothed values S(m)×S(m+p), the index m denoting the associated smoothing interval and taking on values from 1 to N−1, the index taking on values from 1 to N−m, the weights applied to each smoothed value and to each cross-product being proportional respectively to 1 and X(p), the weight X(p) being independent of m.
CROSS-REFERENCE TO RELATED APPLICATIONS
This application claims the benefit of U.S. Provisional Application No. 60/082,768, filed Apr. 23, 1998.
US Referenced Citations (2)
Number |
Name |
Date |
Kind |
5485273 |
Mark et al. |
Jan 1996 |
|
5828980 |
Tazartes et al. |
Oct 1998 |
|
Non-Patent Literature Citations (2)
Entry |
Jiang et al., “Improved Strapdown Coning Algorithms,” IEEE Transactions on Aerospace and Electronic Suystems, vol. 28, No. 2, pp. 484-490, Apr. 1992.* |
Ignagni, M. , “On the Orientation Vector Differential Equation in Strapdown Inertial Systems,” IEEE Transactions on Aerospace and Electronic Systems, vol. 30, No. 4, pp. 10761081, Oct. 1994. |
Provisional Applications (1)
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Number |
Date |
Country |
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60/082768 |
Apr 1998 |
US |