Unscented Filtering for Spacecraft Attitude Estimation
作者： John L. Crassidis , F. Landis Markley
DOI: 10.2514/2.5102
关键词: Mathematics 、 Attitude control 、 Kalman filter 、 Control theory 、 Unscented transform 、 Ensemble Kalman filter 、 Invariant extended Kalman filter 、 Extended Kalman filter 、 Quaternion 、 Filter (signal processing) 、 Control and Systems Engineering 、 Space and Planetary Science 、 Electrical and Electronic Engineering 、 Applied mathematics 、 Aerospace engineering
摘要: A new spacecraft attitude estimation approach based on the unscented lter is derived. For … conditions in attitude estimation problems. The lter formulation is based on standard attitude–…
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