Maneuver Control Strategies to Maximize Prediction Errors in Ballistic Middle Phase

摘要

In this paper, two maneuver strategies in ballistic missile (BM) defense scenarios are proposed, by using which the prediction errors of the defense system are maximized, and energy consumption of the BM is also concerned. In discrete control-input case, the optimal direction angle of the maneuver locates in the first quadrant of velocity coordinates and increases as the moment of maneuver increases. When the maneuver frequency increases, the predicted error also increases. In continuous control-input case, a large amplitude maneuver at a certain time is more effective.