近距格斗空空导弹发射边界判定研究

简要介绍中空空导弹发射边界的拟合方法，在此基础上提出一种基于工程设计经验的“定参数查表拟合法”，该方法选取对导弹发射边界影响较大的参数作为拟合公式的自变量，通过两次回归算法的构造出拟事公式，并对拟合公式进行了验证计算。计算结果表明，该方法满足空战中对空空导弹发射包线计算的实时性要求，并具有较高的拟合精度。

Research for Launching Envelope of Short Range Air-to-Air Missile

Several mathematical approach methods of air to air missile launching envelops are briefly described, and a new method named fixing parameter and checked table method based on engineering design experiences is proposed. It chooses some parameters which greatly affect launching envelopes as formula's self variables, then chooses the approach formula by twice regression algorithm. The result shows that this method can meet the time requirement for air to air missile launching envelope computation in air combat and have higher accuracy.