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DUAL MODE GUIDANCE AND CONTROL SYSTEM FOR A HOMING MISSILE

机译:制导导弹的双模制导与控制系统

摘要

A missile guidance system having two control modes alternatively controlling the thrust vector of the missile. The first control mode provides turning commands for substantially aligning the missile towards an airborne target, and the second control mode controls the missile on a homing path in pursuit of the target once the missile is aligned. A threshold detector operates switches for selectively enabling the control modes, where the first mode is enabled at an angular rate of the target line-of-sight above a predetermined threshold and the second mode is enabled at a light-of-sight rate below the threshold. The first mode provides thrust vector control signals corresponding to a signal sum of the component angle signals of the line-of-sight emitted by a narrow field of view infrared sensor mounted on the missile and continuously locked on to the target, angular rate signals of the line-of-sight, and acceleration signals emitted by an accelerometer having orthogonal sensing axes normal to the line-of-sight. The second mode provides thrust vector control signals corresponding to the difference between the signal sum of the first mode and accelerometer signals emitted by an accelerometer mounted on the missile having orthogonal sensing axes normal to the missile.
机译:一种具有两种控制模式的导弹制导系统,可交替控制导弹的推力矢量。第一控制模式提供转向命令,以使导弹基本对准机载目标,并且一旦导弹对准,第二控制模式就控制导弹在寻找目标的寻靶路径上。阈值检测器操作用于选择性地启用控制模式的开关,其中第一模式以高于预定阈值的目标视线的角速率启用,而第二模式以低于视线的视线速率启用。阈。第一模式提供推力矢量控制信号,该信号对应于由安装在导弹上并连续锁定在目标上的窄视场红外传感器发射的视线的分量角信号的信号和的信号角速度信号。加速度计发出的加速度信号,该加速度计具有正交于传感线的正交感测轴。第二模式提供推力矢量控制信号,该推力矢量控制信号对应于第一模式的信号总和与安装在具有正交于导弹的正交感测轴的导弹上的加速度计发射的加速度计信号之间的差。

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