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NASA NTRS · 20010067774

Attitude Representations for Kalman Filtering

Abstract

The four-component quaternion has the lowest dimensionality possible for a globally nonsingular attitude representation, it represents the attitude matrix as a homogeneous quadratic function, and its dynamic propagation equation is bilinear in the quaternion and the angular velocity. The quaternion is required to obey a unit norm constraint, though, so Kalman filters often employ a quaternion for the global attitude estimate and a three-component representation for small errors about the estimate. We consider these mixed attitude representations for both a first-order Extended Kalman filter and a second-order filter, as well for quaternion-norm-preserving attitude propagation.

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BibTeXRIS

Markley, F. Landis, Bauer, Frank H.. 2001-01-01. Attitude Representations for Kalman Filtering. https://ntrs.nasa.gov/citations/20010067774

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