首页> 外国专利> SYSTEMS AND METHODS FOR CREATING TWO INDEPENDENT DIFFERENT SPATIAL POSITION VALUES, TWO INDEPENDENT DIFFERENT INERTIAL VALUES OR BOTH, USING ONE IMPROVED NAVIGATION DEVICE

SYSTEMS AND METHODS FOR CREATING TWO INDEPENDENT DIFFERENT SPATIAL POSITION VALUES, TWO INDEPENDENT DIFFERENT INERTIAL VALUES OR BOTH, USING ONE IMPROVED NAVIGATION DEVICE

机译:使用一个改进的导航设备创建两个独立的不同的空间位置值,两个独立的不同的惯性值或两者的系统和方法

摘要

FIELD: calculating; counting.;SUBSTANCE: invention relates to the field of navigational instrument-making and can be used in systems and methods of generating two independent unequal values of spatial position, two independent unequal inertial values or both, using one improved navigation device. For this purpose, the on-board aircraft equipment system comprises: an inertial navigation device configured to generate a first group of spatial position values; attitude-and-heading reference system, made with possibility of creation of primary group of values of spatial position and secondary group of values of spatial position; and a display device configured to receive a first group of spatial position values, primary group of values of spatial position and secondary group of spatial position values, wherein if first group of spatial position values and primary group of values of spatial position give different results, then display device determines which of the first group of spatial position values and the primary group of spatial position values is correct by determining differences between spatial position values and detection, which of the differences is below the threshold value.;EFFECT: technical result is expansion of functional capabilities.;20 cl, 2 dwg
机译:领域:计算;发明领域本发明涉及导航仪器制造领域,并且可以用于使用一种改进的导航装置来产生两个独立的不相等的空间位置值,两个独立的不相等的惯性值或两者的系统和方法中。为此,机载飞机设备系统包括:惯性导航装置,其被配置为生成第一组空间位置值;以及姿态和航向参考系统,可以创建主要的空间位置值组和次要的空间位置值组;以及显示装置,被配置为接收第一组空间位置值,第一组空间位置值和第二组空间位置值,其中如果第一组空间位置值和第一组空间位置给出不同的结果,然后,显示设备通过确定空间位置值和检测之间的差异(低于阈值)来确定第一组空间位置值和第一组空间位置值是正确的;效果:技术成果是扩展功能能力; 20 cl,2 dwg

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