Abstract:The problem of guidance control of an interceptor against a ballistic missile flying with some decoys around is studied in this paper. Before the determination of the real target, it is necessary for the interceptor to keep targets reachable as many as possible. First, the terminal guidance problem is analyzed under the complex detection circumstance, and the missile-target relative motion equations are established in the line-of-sight coordinate system. Secondly, the Kalman Filter theory is applied to estimat… Show more
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