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Adaptable Iterative and Recursive Kalman Filter SchemesNonlinear filters are often very computationally expensive and usually not suitable for real-time applications. Real-time navigation algorithms are typically based on linear estimators, such as the extended Kalman filter (EKF) and, to a much lesser extent, the unscented Kalman filter. The Iterated Kalman filter (IKF) and the Recursive Update Filter (RUF) are two algorithms that reduce the consequences of the linearization assumption of the EKF by performing N updates for each new measurement, where N is the number of recursions, a tuning parameter. This paper introduces an adaptable RUF algorithm to calculate N on the go, a similar technique can be used for the IKF as well.
Document ID
20140006041
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Zanetti, Renato
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
May 22, 2014
Publication Date
January 26, 2014
Subject Category
Statistics And Probability
Report/Patent Number
JSC-CN-30315
AAS 14-345
Report Number: JSC-CN-30315
Report Number: AAS 14-345
Meeting Information
Meeting: AAS Spaceflight Mechanics Meeting
Location: Santa Fe, NM
Country: Mexico
Start Date: January 26, 2014
End Date: January 31, 2014
Sponsors: American Astronomical Society
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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