For strong nonlinear of large airspace maneuvering cruise missile occurring during the course of descending and switching to aclinic fly,the fuzzy PID control metiod is designed for pitching path.

• 针对大空域机动巡航导弹下降转平飞过程中出现的强非线性特点,在俯仰通道设计了模糊PID双模控制方案。