DocumentCode :
1147172
Title :
State Estimation and Divergence Analysis
Author :
Catlin, Donald E. ; Geddes, Robert L.
Author_Institution :
The Analytic Sciences Corporation
Issue :
5
fYear :
1984
Firstpage :
594
Lastpage :
602
Abstract :
A growing memory discrete dynamic model for performing temporal extrapolations along a predetermined path in a random field is presented. This dynamic model is used to drive a linear system that is itself driven by discrete white noise. The coupled system is used to derive a state estimation scheme that recursively processes noisy measurements of the system. In addition, using the aforementioned dynamic model as a reference (truth) model, the authors develop a covariance analysis to measure the estimation errors that occur when the dynamics along the path through the field are modeled as a Markov linear model and state estimation is performed using discrete Kalman filtering. The performance evaluation of an inertial navigation system influenced by the Earth´s gravity field aboard a maneuvering ship is provided as a specific illustrative example.
Keywords :
Drives; Estimation error; Extrapolation; Kalman filters; Linear systems; Nonlinear filters; Performance analysis; Performance evaluation; State estimation; White noise;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.1984.310527
Filename :
4103960
Link To Document :
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