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本文在分析空空导弹末端控制(Endgame)原理的基础上,研究了导弹Endgame系统的动力学和不确定性,最后对空空导弹末端控制制导规律进行了讨论,认为基于微分对策理论的最优化导引律和基于鲁棒H~∞控制理论的最优化导引律对空空导弹的末端控制制导具有明显的适用性。
Based on the analysis of the principle of Endgame, this paper studies the dynamics and uncertainty of the missile Endgame system. Finally, the control law of end-control of air-to-air missile is discussed. It is considered that the optimization guidance based on differential game theory Law and the optimal guidance law based on robust H ~ ∞ control theory have obvious applicability to the end-control guidance of air-to-air missiles.