DocumentCode
2059936
Title
Design of Schmidt-Kalman filter for target tracking with navigation errors
Author
Yang, Chun ; Blasch, Erik ; Douville, Phil
Author_Institution
Sigtem Technol., Inc., San Mateo, CA, USA
fYear
2010
fDate
6-13 March 2010
Firstpage
1
Lastpage
12
Abstract
In most target tracking formulations, the tracking sensor location is typically assumed perfectly known. Without accounting for navigation errors of the sensor platform, regular Kalman filters tend to be optimistic (i.e., the covariance matrix far below the actual mean squared errors). In this paper, the Schmidt-Kalman filter (SKF) is formulated for target tracking with navigation errors. The SKF does not estimate the navigation errors explicitly but rather takes into account (i.e., considers) the navigation error covariance provided by an on-board navigation unit in the tracking filter formulation. Including the navigation errors leads to the so-called ¿consider covariance.¿ By exploring the structural navigation errors, the SKF is not only more consistent but also produces smaller mean squared errors than regular Kalman filters. Monte Carlo simulation results are presented in the paper to demonstrate the operation and performance of the SKF for target tracking in the presence of navigation errors.
Keywords
Kalman filters; Monte Carlo methods; design; navigation; target tracking; Monte Carlo simulation; Schmidt-Kalman filter design; consider covariance; covariance matrix; mean squared errors; regular Kalman filters; structural navigation errors; target tracking; tracking sensor location; Covariance matrix; Filters; Force sensors; Missiles; Navigation; Position measurement; Radar measurements; Radar tracking; Sensor fusion; Target tracking;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2010 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4244-3887-7
Electronic_ISBN
1095-323X
Type
conf
DOI
10.1109/AERO.2010.5446689
Filename
5446689
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