Analytical results are presented for determining the steady-state components of the gain and error covariance matrices of the two-state Kalman tracking filter with white noise maneuver capability.
Analytical Results for a Kalman Tracker Using Position and Rate Measurements
IEEE Transactions on Aerospace and Electronic Systems ; AES-19 , 5 ; 776-778
1983-09-01
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Article (Journal)
Electronic Resource
English
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