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    • 9. 发明授权
    • Guided missile using fluidic sensing and steering
    • 导弹使用流体感应和转向
    • US3979085A
    • 1976-09-07
    • US513015
    • 1974-10-08
    • John P. Leonard
    • John P. Leonard
    • F42B10/66F42B15/18
    • F42B10/66
    • A missile using fluidic sensors for determination of net aerodynamic forcend moment on the missile. The force and moment thus determined are processed and summed by fluidic amplifiers and integrators to provide control signals for fluidic thrusters or other steerers for the missile. The sensors are diametrically opposed pairs of pressure taps located axially and circumferentially in the missile skin. Net aerodynamic force on the missile is taken as the algebraic sum from all the sensors in a linear fluidic summer, and net aerodynamic moment is taken from the proportional sum of the sensors in accordance with their position along the axis of the missile. This proportional sum is made in a fluidic vortex summer.
    • 使用流体传感器确定导弹上净空气动力和力矩的导弹。 由此确定的力和力矩由流体放大器和积分器进行处理和求和,为流体推进器或导弹的其他导向器提供控制信号。 传感器在导弹皮肤中沿轴向和周向定位的直径相对的压力抽头对。 在线性流动夏季,导弹上的净空气动力学作为所有传感器的代数和,并根据其沿导弹轴线的位置从传感器的比例和获取净空气动力学力矩。 这个比例总和是在流体涡旋夏季进行的。