... 飞航式反雷达火箭 aerodynamic radar booster 飞航式导弹 aerodynamically unsupported missile; air-supported missile; aircraft type vehicle; guided bomber; missile plane; wing-borne missile; winged missile 飞航式导弹库 cruise missile; doodlebug; fly bomb ...
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While designing winged missile flight control system, attitude stable scheme is traditional selected in our country. The method means that measuring the missile attitude angles and angle-rate by sensor, attitude angular PID control is executed by close loop.
在设计飞航导弹的飞行控制系统时，国内一般采用传统的姿态稳定控制方案，即由敏感元件测量导弹的空间姿态角和姿态角速度，形成闭合回路，进行姿态角的PID控制。
参考来源 - 反舰导弹末端机动弹道的实现研究·2,447,543篇论文数据，部分数据来源于NoteExpress
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