A fourth-order extended Kalman filter is developed to estimate target maneuvers, and a guidance law using these estimates is implemented.
Missile Guidance Based on Kalman Filter Estimation of Target Maneuver
IEEE Transactions on Aerospace and Electronic Systems ; AES-20 , 6 ; 736-741
01.11.1984
929567 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Missile guidance based on Kalman filter estimation of target maneuver
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