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在有随高度变化的非常值风干扰、反辐射导弹采用比例导引法制导的情况下，讨论了反辐射导弹运动学环节的建模问题，并且通过计算机对该模型进行了验证。
Under the condition of abnormal value wind disturbance with altitude and anti-radiation missile guided by proportional guidance method, the modeling problem of anti-radiation missile kinematics is discussed, and the model is validated by computer.