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Nonlinear Attitude Filtering MethodsThis paper provides a survey of modern nonlinear filtering methods for attitude estimation. Early applications relied mostly on the extended Kalman filter for attitude estimation. Since these applications, several new approaches have been developed that have proven to be superior to the extended Kalman filter. Several of these approaches maintain the basic structure of the extended Kalman filter, but employ various modifications in order to provide better convergence or improve other performance characteristics. Examples of such approaches include: filter QUEST, extended QUEST, the super-iterated extended Kalman filter, the interlaced extended Kalman filter, and the second-order Kalman filter. Filters that propagate and update a discrete set of sigma points rather than using linearized equations for the mean and covariance are also reviewed. A two-step approach is discussed with a first-step state that linearizes the measurement model and an iterative second step to recover the desired attitude states. These approaches are all based on the Gaussian assumption that the probability density function is adequately specified by its mean and covariance. Other approaches that do not require this assumption are reviewed, including particle filters and a Bayesian filter based on a non-Gaussian, finite-parameter probability density function on SO(3). Finally, the predictive filter, nonlinear observers and adaptive approaches are shown. The strengths and weaknesses of the various approaches are discussed.
Document ID
20050212421
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
F Landis Markley
(Goddard Space Flight Center Greenbelt, Maryland, United States)
John L Crassidis
(University at Buffalo, State University of New York Buffalo, New York, United States)
Yang Cheng
(University at Buffalo, State University of New York Buffalo, New York, United States)
Date Acquired
September 7, 2013
Publication Date
August 15, 2005
Publication Information
Publication: AIAA Guidance, Navigation, and Control Conference and Exhibit
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA-2005-5927
Meeting Information
Meeting: AIAA Guidance, Navigation, and Control Conference and Exhibit
Location: San Francisco, CA
Country: US
Start Date: August 15, 2005
End Date: August 18, 2005
Sponsors: American Institute of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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