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本文论述用于空空导弹的一些制导技术。主要强调的是,由瞄准线加速度增大的比例导航形式。结论是,瞄准线加速度与比例导航相加,对自动导引导弹末端精度的改善不大。
This article discusses some guidance techniques for air-to-air missiles. The main emphasis is on the form of proportional navigation with increased line of sight acceleration. The conclusion is that the addition of line-of-sight acceleration to proportional navigation improves the accuracy of the tip of the automated guided missile slightly.