Title :
Missile Guidance Based on Kalman Filter Estimation of Target Maneuver
Author :
Tang, Y.M. ; Borrie, J.A.
Author_Institution :
Luoyang Dynamic Institute Chinese Aeronautical Establishment People´´s Republic of China
Abstract :
A fourth-order extended Kalman filter is developed to estimate target maneuvers, and a guidance law using these estimates is implemented.
Keywords :
Acceleration; Aerodynamics; Equations; Gaussian noise; Missiles; Noise measurement; Sampling methods; State estimation; Time measurement; Virtual manufacturing;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
DOI :
10.1109/TAES.1984.310456
