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    • 1. 发明授权
    • Angle encoder
    • 角度编码器
    • US4899955A
    • 1990-02-13
    • US300635
    • 1989-01-23
    • Jean A. FattalDavid J. DugasLouis L. Tella
    • Jean A. FattalDavid J. DugasLouis L. Tella
    • F41G7/22G01C19/28
    • F41G7/2213G01C19/28Y10T74/1264
    • An angle encoder for determining the pitch (or yaw) angle of a gyroscopic mass with respect to the pitch (or yaw) axis of a missile in flight is shown to be the combination of: (a) an optical encoder pattern disposed on the periphery of the gyroscopic mass, such pattern preferably being divided into a substantially equal reflective portion and a nonreflective portion; (b) an optical sensor arrangement having a limited field of view, such arrangement being mounted on the body of the missile to provide a first signal whose level is indicative of the reflective or nonreflective portion in the limited field of view; and (c) circuitry for converting the first signal into a signal indicative of the pitch (or yaw) angle of the missile.
    • 用于确定陀螺质量相对于飞行中的导弹的俯仰(或偏航)轴的俯仰(或偏航)角度的角度编码器被示为以下的组合:(a)设置在外围的光学编码器图案 的陀螺质量,这种图案优选地被分成基本上相等的反射部分和非反射部分; (b)具有有限视野的光学传感器装置,这种布置被安装在导弹的主体上以提供第一信号,其第一信号的电平指示有限视场内的反射或非反射部分; 和(c)用于将第一信号转换成指示导弹的俯仰(或偏航)角度的信号的电路。