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Estimation of Kalman filter model parameters from an ensemble of testsA methodology for estimating initial mean and covariance parameters in a Kalman filter model from an ensemble of nonidentical tests is presented. In addition, the problem of estimating time constants and process noise levels is addressed. Practical problems such as developing and validating inertial instrument error models from laboratory test data or developing error models of individual phases of a test are generally considered.
Document ID
19810002567
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gibbs, B. P.
(Business and Technological Systems, Inc. Bowie, MD, United States)
Haley, D. R.
(Business and Technological Systems, Inc. Bowie, MD, United States)
Levine, W.
(Business and Technological Systems, Inc. Bowie, MD, United States)
Porter, D. W.
(Business and Technological Systems, Inc. Bowie, MD, United States)
Vahlberg, C. J.
(Business and Technological Systems, Inc. Bowie, MD, United States)
Date Acquired
August 11, 2013
Publication Date
October 1, 1980
Publication Information
Publication: NASA. Goddard Space Flight Center Fifth Ann. Flight Mech.(Estimation Theory Symp.
Subject Category
Astrodynamics
Accession Number
81N11075
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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