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    • 1. 发明授权
    • Method of improving satellite reacquisition performance for integrated GP/IG navigational systems
    • 综合GP / IG导航系统改善卫星重新获取性能的方法
    • US06640189B2
    • 2003-10-28
    • US09955609
    • 2001-09-19
    • Michael S. PerlmutterIan Humphrey
    • Michael S. PerlmutterIan Humphrey
    • G01C2100
    • G01S19/26G01C21/165G01S19/49
    • A method of reacquiring a satellite signal within an integrated GP/IG navigation system includes detecting a loss of synchronization between a timing code in the satellite signal and a corresponding reference timing code. The method includes receiving position data from an inertial guidance unit. The position data is representative of an estimated position (and its associated uncertainty) of the navigation system. The method also includes estimating a distance from the navigation system to the satellite, as a function of the position data, and deriving an initial delay from the distance. The method includes delaying the reference timing code, with respect to the timing code embedded in the satellite signal, by an offset delay substantially equal to the initial delay. The method includes incrementally varying the offset delay until the timing code embedded in the satellite signal is synchronized with the reference timing code, or until the offset delay equals a predetermined end limit value.
    • 在集成GP / IG导航系统内重新获取卫星信号的方法包括检测卫星信号中的定时码与对应的参考定时码之间的同步丢失。 该方法包括从惯性引导单元接收位置数据。 位置数据代表导航系统的估计位置(及其相关联的不确定性)。 该方法还包括根据位置数据估计从导航系统到卫星的距离,以及从该距离导出初始延迟。 该方法包括相对于嵌入在卫星信号中的定时码延迟参考定时码与基本上等于初始延迟的偏移延迟。 该方法包括逐渐改变偏移延迟,直到嵌入在卫星信号中的定时代码与参考定时码同步,或者直到偏移延迟等于预定的限制值。
    • 3. 发明授权
    • Method and apparatus for suppressing off-axis modes in laser and ring
laser gyroscopes
    • 用于抑制激光和环激光伽马射线偏轴模式的方法和装置
    • US5166949A
    • 1992-11-24
    • US631592
    • 1990-12-20
    • Michael S. Perlmutter
    • Michael S. Perlmutter
    • G01C19/66H01S3/034H01S3/083
    • H01S3/083G01C19/665H01S3/034
    • A dielectric interference film having a central region of one thickness and a peripheral region of a different thickness is superimposed on one of the mirrors of a ring laser gyroscope for the purpose of suppressing off-axis resonant modes that are characteristic of a resonant cavity. The central region is designed to intercept a large portion of the fundamental mode power and a lesser portion of the off-axis mode power. The difference in thickness between the central and peripheral regions causes the reflected light from the two regions to differ in phase by approximately one-half wavelength and destructively interfere. As a result of the imbalance of the fundamental and off-axis mode powers incident on the central region, the reflectivity losses of the off-axis modes are more pronounced than those of the fundamental mode with the result that the off-axis modes are completely suppressed.
    • 为了抑制作为谐振腔的特征的离轴共振模式,将具有一个厚度的中心区域和不同厚度的周边区域的电介质干涉膜叠加在环形激光陀螺仪的一个反射镜上。 中心区域被设计成拦截基本模式功率的大部分和离轴模式功率的较小部分。 中心区域和外围区域之间的厚度差导致来自两个区域的反射光的相位相差大约二分之一的波长并且相消干涉。 由于入射到中心区域的基极和离轴模式功率的不平衡,离轴模式的反射率损耗比基模的反射率损失更明显,结果是离轴模式完全 被压制
    • 5. 发明授权
    • Pressure-equalized self-compensating discharge configuration for
triangular ring laser gyroscopes
    • 三角环激光陀螺仪的均压自补偿放电配置
    • US5430755A
    • 1995-07-04
    • US705248
    • 1991-05-24
    • Michael S. Perlmutter
    • Michael S. Perlmutter
    • G01C19/66G01B9/02
    • G01C19/661
    • A triangular ring laser gyroscope having a single anode, single cathode, and self-compensating discharge path which cancels gyro bias, bias drift, and noise. The discharge path extends from the anode through a cross channel in the center of the gyro block to the cathode. Counter-propagating laser beams traverse one segment of the discharge path in the direction of the Langmuir flow from anode to cathode, and another segment of the discharge path of equal length in a direction opposite to that flow. The Langmuir return flow from cathode to anode occurs along the walls of the gyro cavity, producing a more uniform gas flow velocity in the central region of the discharge path. Drag effects on the counter-propagating laser beams are equal but opposite, and the laser beams traverse a more uniform region of the Langmuir flow when thermally-induced changes in the gyro cause beam wandering. Gyro bias, bias drift, and noise are substantially cancelled.
    • 具有单个阳极,单个阴极和自补偿放电路径的三角形环形激光陀螺仪,其抵消陀螺仪偏置,偏置漂移和噪声。 放电路径从阳极延伸通过陀螺仪块中心的交叉通道到阴极。 反向传播的激光束沿着Langmuir流从阳极到阴极的方向穿过放电路径的一个部分,并且沿着与该流相反的方向具有相等长度的另一段放电路径。 从阴极到阳极的Langmuir回流沿着陀螺腔的壁发生,在排放路径的中心区域产生更均匀的气体流速。 在反向传播的激光束上的拖曳效应相等但相反,当陀螺仪的热诱导变化导致光束漂移时,激光束横越Langmuir流的更均匀的区域。 陀螺偏置,偏置漂移和噪声基本上被取消。