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    • 7. 发明授权
    • Target for torpedo launch system
    • 鱼雷发射系统的目标
    • US4046993A
    • 1977-09-06
    • US700655
    • 1976-06-28
    • Charles A. WilsonPatrick J. Moran
    • Charles A. WilsonPatrick J. Moran
    • G06G7/80
    • G06G7/80
    • A system for determining the proper instant of time to launch an object, h as a target or torpedo, from an aircraft to cause the object to impact a water surface at a predetermined nose-down angle, thereby preventing structural damage due to high impact forces. The system utilizes signals produced by instrumentation representative of the aircraft pitch and angular rate of pitch. The desired launch altitude and predetermined impact angle are physically set into the system by means of adjustable voltage sources. These parameters are processed in the system such that the system forms a complete electronic analogy to the physical laws which govern the motion of the free falling object. In operation, the system continuously computes the predicted impact angle based on the instantaneous inputs of the aircraft's altitude, pitch angle and pitch rate. It then compares the predicted impact angle with the predetermined impact angle. Whenever the predicted impact angle exceeds the predetermined impact angle, a launch signal is produced to release the object.
    • 一种用于确定从飞行器发射诸如目标或鱼雷的物体的适当时刻的适当时刻的系统,以使物体以预定的向下倾斜角度冲击水面,从而防止由于高冲击力引起的结构损坏 。 该系统利用由代表飞机俯仰和俯仰角度速率的仪表产生的信号。 通过可调电压源将期望的发射高度和预定的撞击角物理地设置到系统中。 这些参数在系统中被处理,使得系统与控制自由落体的运动的物理规律形成完整的电子类比。 在运行中,系统基于飞机高度,俯仰角和俯仰速率的瞬时输入,连续计算预测的冲击角。 然后将预测的冲击角与预定的冲击角进行比较。 每当预测的冲击角超过预定冲击角时,产生发射信号以释放物体。