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本文采用变步长加速法对反辐射导弹惯性制导段的控制参数进行了优化,并针对变步长加速法收敛慢的问题提出了一种改进方法,取得了满意的结果。
In this paper, variable step-size acceleration method is used to optimize the control parameters of inertial guidance section of anti-radiation missile, and an improved method is proposed to solve the problem of slow convergence with variable step size acceleration method. Satisfactory results have been obtained.