Missile Guidance Based on Kalman Filter Estimation of Target Maneuver |
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Authors: | Tang Y.M. Borrie J.A. |
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Affiliation: | Luoyang Dynamic Institute Chinese Aeronautical Establishment People's Republic of China; |
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Abstract: | ![]() A fourth-order extended Kalman filter is developed to estimate target maneuvers, and a guidance law using these estimates is implemented. |
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