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特征结构配置适用于中程空空技术（ＥＭＲＡＡＴ）导弹自动驾驶仪的设计。通过选择一些在模型去耦基础上的理想特征矢量，来计算特征结构配置的反馈增益，并用Ａｎｄｒｙ等人建议的正交投影解法来计算特征矢量。将这种解法与Ｂｏｓｓｉ和Ｌａｎｇｅｈｏｕｇｈ提出的线性二次调节设计方法作一比较。
The feature configuration is suitable for the design of the mid-range space-time technology (EMRAAT) missile autopilot. The feedback gain of the feature configuration is calculated by selecting some ideal feature vectors based on model decoupling and the feature vectors are calculated using the orthogonal projection solution proposed by Andry et al. This solution is compared with the linear quadratic adjustment method proposed by Bossi and Langehough.