An alternative erection procedure for on-ground transfer alignment

H. Rotstein, Y. Baumgarten
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Abstract

This paper presents a procedure for computing the relative orientation between two static inertial navigation systems: a primary and a secondary. The primary system is assumed to be of navigation quality and therefore capable of gyro-compassing to the desired accuracy. The secondary is lower quality and requires external aiding for azimuth and accurate leveling initialization. The assumption that allows the transfer alignment is that the primary and the secondary are rigidly mounted on a mechanical structure that allows for joint rotation around one or more axis while maintaining the relative orientation between the two systems. A pitch axis is typical in practical systems and hence the name “Erection Procedure.” As opposed to the Kalman-filter based procedures in use in several systems today, the new method does not require the computation of a navigation solution while the mechanical system is been erected. Instead, measurements from the navigation sensors are required at a number of discrete stages, and then these measurements are processed to compute the relative orientation between the primary and the secondary. The procedure is easy to implement and yields an exact solution to the problem whenever the underlying assumptions are exactly met. It has been shown to work well both in simulations and in practice. In addition to its practical relevance, this work also sheds additional light into the general question of aligning two static navigation systems.
另一种地面转移校准的安装程序
本文给出了主、副两种静态惯性导航系统相对定位的计算方法。假定主系统具有导航质量,因此能够使陀螺仪罗盘达到所需的精度。次要的质量较低,需要外部辅助方位角和精确的水平初始化。允许传递对准的假设是,主要和次要是刚性安装在一个机械结构上,允许关节围绕一个或多个轴旋转,同时保持两个系统之间的相对方向。俯仰轴在实际系统中是典型的,因此被称为“安装过程”。与目前在一些系统中使用的基于卡尔曼滤波的程序相反,新方法不需要在机械系统建立时计算导航解。相反,导航传感器的测量需要在多个离散阶段进行,然后对这些测量进行处理,以计算主要和次要之间的相对方向。这个过程很容易实现,并且只要基本假设完全满足,就会产生问题的精确解决方案。该方法在模拟和实际应用中都取得了良好的效果。除了其实际意义之外,这项工作还为对齐两个静态导航系统的一般问题提供了额外的启发。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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