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概述本文研究了某些气动参数对空——空导弹性能的不同影响。阻力对射程的影响是显而易见的,但阻尼导数对寻的导弹性能的影响却是难以捉摸的。用简化方法对脱靶量所进行的解析估算表明,其结果与弹道的数值计算结果极其吻合,所得参数对射程和脱靶量的重要性可按减小的顺序排列如下:阻力和升力线斜率;力矩的稳定和操纵导数;操纵力导数和非线性
Summary This paper studies the different effects of certain aerodynamic parameters on the performance of air-to-air missiles. The effect of drag on range is obvious, but the effect of damping derivatives on the performance of missiles is elusive. The analytical estimates of the miss distance using the simplified method show that the results are in good agreement with the numerical results of the trajectory. The importance of the parameters obtained for range and miss distance can be ranked in decreasing order as follows: resistance and lift line slope; torque Stable and manipulated derivatives; Derivatives and non-linearities