DocumentCode
1127323
Title
Steady State Results for the X, Y, Z Kalman Tracking Filter
Author
Ramachandra, K.V. ; Srinivasan, V.S.
Author_Institution
Electronics and Radar Development Establishment, Bangalore 560001, India
Issue
4
fYear
1977
fDate
7/1/1977 12:00:00 AM
Firstpage
419
Lastpage
423
Abstract
An X, Y, Z Kalman tracking filter is described and its steady state characteristics are analytically determined when the radar sensor meaures range, bearing, and elevation (¿, ¿, ¿) at uniform intervals of time, T seconds. The relationship between the quantities measured by the sensor (¿, ¿,¿) and the Cartesian coordinate system (X, Y, Z) is explicitly considered.
Keywords
Acceleration; Coordinate measuring machines; Covariance matrix; Kalman filters; Noise measurement; Radar measurements; Radar tracking; Steady-state; Vehicles; Zinc;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1977.308482
Filename
4101837
Link To Document