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Design of Multi-Sensor Attitude Determination Systems

by

Gebre-Egziabher, D., R. C. Hayward and J. D. Powell

in

IEEE Transactions on Aerospace Electronic Systems, Vol. 40, No. 2, pp. 627-649, 2004.

Category: Journal Article

Click here to request an electronic copy of this paper.

Abstract:

The design of inexpensive multi-sensor attitude determination systems is discussed. The systems discussed fuse information from a triad of solid state rate gyros with an aiding system mechanized using GPS or magnetometers and accelerometers. Euler angle and quaternion-based sensor fusion algorithms are developed. Methods for gain scheduling and estimator pole placement are presented. Using simulation and flight test results, it is shown that quaternion-based algorithms simplify gain scheduling and improve transient response.


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