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Attitude determination and calibration using a recursive maximum likelihood-based adaptive Kalman filterAn adaptive Kalman filter design that utilizes recursive maximum likelihood parameter identification is discussed. At the center of this design is the Kalman filter itself, which has the responsibility for attitude determination. At the same time, the identification algorithm is continually identifying the system parameters. The approach is applicable to nonlinear, as well as linear systems. This adaptive Kalman filter design has much potential for real time implementation, especially considering the fast clock speeds, cache memory and internal RAM available today. The recursive maximum likelihood algorithm is discussed in detail, with special attention directed towards its unique matrix formulation. The procedure for using the algorithm is described along with comments on how this algorithm interacts with the Kalman filter.
Document ID
19910007775
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kelly, D. A.
(A & B Design Engineering Co., Inc., West Acton MA., United States)
Fermelia, A.
(Hughes Aircraft Co. Aurora, CO., United States)
Lee, G. K. F.
(North Carolina State Univ. Raleigh., United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1990
Publication Information
Publication: NASA, Goddard Space Flight Center, Flight Mechanics(Estimation Theory Symposium, 1990
Subject Category
Astrodynamics
Accession Number
91N17088
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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