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    • 1. 发明申请
    • METHOD AND SYSTEM FOR LATITUDE ADAPTIVE NAVIGATION QUALITY ESTIMATION
    • 用于自适应导航质量估计的方法和系统
    • US20110137560A1
    • 2011-06-09
    • US12630403
    • 2009-12-03
    • Reed R. May
    • Reed R. May
    • G01C21/16
    • G01C21/16G01C19/38G01C25/005
    • A method and system for navigation quality estimation is provided. The method comprises obtaining an alignment observation, comparing the alignment observation to a current heading estimate, and updating the current heading estimate based on the comparison. A heading error estimate is updated based on the updated current heading estimate, and an estimated drift rate is determined based on the heading error estimate and an operational latitude. A determination is then made whether a drift rate requirement is met by the estimated drift rate. If the drift rate requirement is not met, the method is repeated until the drift rate requirement is met.
    • 提供了一种用于导航质量估计的方法和系统。 该方法包括获得比对观察,比较对准观测与当前航向估计,以及基于比较来更新当前航向估计。 基于更新的当前航向估计来更新航向误差估计,并且基于航向误差估计和操作纬度来确定估计漂移率。 然后确定漂移率要求是否由估计的漂移率满足。 如果不满足漂移率要求,则重复该方法,直到满足漂移率要求为止。
    • 3. 发明授权
    • Method and system for latitude adaptive navigation quality estimation
    • 纬度自适应导航质量估算方法与系统
    • US08209117B2
    • 2012-06-26
    • US12630403
    • 2009-12-03
    • Reed R. May
    • Reed R. May
    • G01C21/00
    • G01C21/16G01C19/38G01C25/005
    • A method and system for navigation quality estimation is provided. The method comprises obtaining an alignment observation, comparing the alignment observation to a current heading estimate, and updating the current heading estimate based on the comparison. A heading error estimate is updated based on the updated current heading estimate, and an estimated drift rate is determined based on the heading error estimate and an operational latitude. A determination is then made whether a drift rate requirement is met by the estimated drift rate. If the drift rate requirement is not met, the method is repeated until the drift rate requirement is met.
    • 提供了一种用于导航质量估计的方法和系统。 该方法包括获得比对观察,比较对准观测与当前航向估计,以及基于比较来更新当前航向估计。 基于更新的当前航向估计来更新航向误差估计,并且基于航向误差估计和操作纬度来确定估计漂移率。 然后确定漂移率要求是否由估计的漂移率满足。 如果不满足漂移率要求,则重复该方法,直到满足漂移率要求为止。
    • 5. 发明授权
    • System and method for dynamically estimating output variances for carrier-smoothing filters
    • 用于动态估计载波平滑滤波器的输出方差的系统和方法
    • US07609204B2
    • 2009-10-27
    • US11215169
    • 2005-08-30
    • Reed R. MayKenneth S. Morgan
    • Reed R. MayKenneth S. Morgan
    • G01S1/00
    • G01S19/15G01S19/32G01S19/43
    • An improved system and method is disclosed for dynamically estimating the output variances of carrier-smoothing filters used, for example, in GPS receivers. By accurately estimating the output variances of the carrier-smoothing filters as they transition from initialization to steady-state operation, it is possible to calculate any required protection levels without having to wait for the filters to fully stabilize. As one example, a system for estimating output variances of a carrier-smoothing filter for use in a satellite navigation system receiver is disclosed, which includes a plurality of smoothing filters associated with a navigation processing unit in a satellite navigation receiver. One or more processors associated with the navigation processing unit executes an algorithm for each smoothing filter, which provides a method for dynamically calculating an output variance for a respective smoothing filter as it transitions in response to new input variance values. The method also predicts the settling point of the output variance for that smoothing filter given a set of pseudorange and carrier-phase values to be applied. Therefore, using this novel output variance prediction method, precision navigation applications such as, for example, airborne GPS-based precision landing system applications can begin operations with suitable calculated protection level values without having to wait for the smoothing filters to stabilize. Thus, such precision landing systems are available for use as soon as the required protection level values are reached.
    • 公开了一种改进的系统和方法,用于动态估计例如在GPS接收机中使用的载波平滑滤波器的输出方差。 通过准确估计载波平滑滤波器从初始化到稳态运行的输出方差,可以计算任何所需的保护电平,而无需等待滤波器完全稳定。 作为一个示例,公开了一种用于估计用于卫星导航系统接收机的载波平滑滤波器的输出方差的系统,其包括与卫星导航接收机中的导航处理单元相关联的多个平滑滤波器。 与导航处理单元相关联的一个或多个处理器执行每个平滑滤波器的算法,该算法提供一种用于在响应于新的输入方差值而转变时动态计算各个平滑滤波器的输出方差的方法。 该方法还预测给定要应用的伪距和载波相位值的集合的平滑滤波器的输出方差的稳定点。 因此,使用这种新颖的输出方差预测方法,诸如例如基于机载GPS的精确着陆系统应用的精密导航应用可以开始具有适当计算的保护等级值的操作,而不必等待平滑滤波器稳定。 因此,一旦达到所需的保护等级值,这种精密着陆系统就可以使用。
    • 6. 发明授权
    • Arrangement for converting a plan position indicator radar display to a
scaled perspective display
    • 将平面位置指示器雷达显示转换成缩放透视显示的布置
    • US5357258A
    • 1994-10-18
    • US157252
    • 1993-11-26
    • Reed R. May
    • Reed R. May
    • G01S7/20G01S7/298G01S7/512
    • G01S7/298G01S7/20
    • A plan position indicator display is converted to a correctly scaled perspective display based on aircraft altitude and display parameters. Two cartesian based display memories are involved. One memory stores the plan position indicator image to be converted and the other memory stores the converted image ready for direct display on a bit-mapped display device. The arrangement is such that a plan position indicator display pixel address is provided for each pixel in the memory which stores the converted image for permitting said latter memory to be completely filled with the most appropriate pixel values at the frame rate without the need for further pixel filling or erasing.
    • 平面位置指示器显示被转换为基于飞机高度和显示参数的正确缩放的透视显示。 涉及两个笛卡尔式显示存储器。 一个存储器存储要转换的平面位置指示器图像,并且另一个存储器存储转换图像准备好直接显示在位映射显示设备上。 该布置使得为存储转换图像的存储器中的每个像素提供平面位置指示器显示像素地址,以允许以帧速率完全填充最合适的像素值,而不需要进一步的像素 填写或删除。