《Table 1 Parameters for instance analysis》

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《基于空中红外对抗随机过程的制导精度分析（英文）》

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A tail-chase countering engagement at the same elevation was chosen to analyze the influence of the guidance parameters and discrimination time on the guidance precision.In this instance，the total flight time of the missile was set to 10s，and the target had started to launch decoys directly downwards since the missile was launched.In this situation，the missile hasonly vertical downward disturbance.and the parameters for this instance are listed in Table 1.