惯性导航系统
惯性测量装置
计量单位
导航系统
计算机科学
风三角
空中航行
计算机视觉
天文导航
惯性基准装置
观测误差
惯性参考系
加速度计
误差分析
人工智能
全球定位系统
数学
地理
机器人
统计
电信
移动机器人
物理
操作系统
机器人控制
量子力学
地图学
应用数学
作者
Andrei M. Shkel,Yusheng Wang
标识
DOI:10.1002/9781119699910.ch4
摘要
One of the most important characteristics of an inertial navigation system is its navigation accuracy, which is directly related to the measurement errors of the inertial measurement unit (IMU). This chapter analyses the relation between the IMU error and the navigation error in the strapdown inertial navigation. It introduces the terminology, origin, and characteristics of some of the major error sources. Error sources in navigation can be categorized into three groups: IMU errors, initial calibration errors, and numerical errors. Assembly errors mainly come from the shift of the mounting direction of individual inertial sensors from their ideal orientations. The position error will exceed a meter of error within a few seconds of navigation with unaided consumer grade IMUs. Tactical grade IMUs have the capability of attitude measurement with reasonable errors and are able to conduct short-term navigation, with navigation accuracy on the order of meters within 30 seconds of strapdown inertial navigation.
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