Attitude Estimation or Quaternion Estimation?

The absence of a globally nonsingular three-parameter representation of the rotation group forces attitude Kalman filters to estimate either a singular or a redundant attitude representation. We compare two filtering strategies using simplified kinematics and measurement models. Our favored strategy...

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Veröffentlicht in:The Journal of the astronautical sciences 2004-01, Vol.52 (1-2), p.221-238
1. Verfasser: Markley, F. Landis
Format: Artikel
Sprache:eng
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Zusammenfassung:The absence of a globally nonsingular three-parameter representation of the rotation group forces attitude Kalman filters to estimate either a singular or a redundant attitude representation. We compare two filtering strategies using simplified kinematics and measurement models. Our favored strategy estimates a three-parameter representation of attitude deviations from a reference attitude specified by a higher-dimensional nonsingular parameterization. The deviations from the reference are assumed to be small enough to avoid any singularity or discontinuity of the three-dimensional parameterization. We point out some disadvantages of the other strategy, which directly estimates the four-component quaternion representation.
ISSN:0021-9142
2195-0571
DOI:10.1007/BF03546430