我们已经了解建立一个不受导弹弹体运动干扰的精确测量的视线速率是必不可少的。任何这样的耦合会减少稳定余量和降低导引过程的精度。理论上,我们要求自动驾驶仪调整导弹的响应并且由导引头内的速率陀螺将导引头从导弹的运动中迅速解耦出 We have learned that it is imperative to establish a precisely measured line-of-sight rate that is unaffected by missile projectile motion. Any such coupling will reduce the stability margin and reduce the accuracy of the guidance process. In theory, we asked the autopilot to adjust the missile’s response and promptly decoupling the seeker from the missile’s motion by the rate gyro in the seeker