针对平面拦截问题，选择导弹和目标之间的相对速度矢量与导弹-目标视线之间的夹角（称为相对航向误差角）作为将要被控制到零的输出。

For the case of planar interception, the so called relative heading error angle between the relative velocity vector and the LoS (Line of Sight) is chosen as the output to be controlled to zero.

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虽然成功已离她远去，但她却能稍微改变命运的航向，除此以外，她别无选择。

Although success left her away, she had no alternative but change her fate course slightly.

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