本文涉及一个方向控制装置,此装置用于控制导弹在其末段的俯冲机动飞行,即导弹从投放点到末端的控制。它同时使用纵向和横向加速度计来敏感纵向和横向距离,以使导弹按予定的末段俯冲飞行路线运动,并提供适当的单个控制指令给导弹制导系统和自动驾驶的俯仰、偏航和横滚伺服控制系统。这些俯仰、偏航和横滾伺服控制系统操纵所用各控 This article relates to a directional control device that is used to control the submarine maneuvering of a missile at its final stage, that is, the control of the missile from the point of delivery to the end. It uses both longitudinal and lateral accelerometers for both longitudinal and lateral sensitivities to allow the missile to follow a predetermined final subduction flight path and provide appropriate individual control commands to the missile guidance system and to the autonomous pilot's pitch, yaw and roll Servo control system. These pitch, yaw and roll servo control systems control each of the controls