Inertial Measurement Unit for Trajectography

Jean-Pascal Martinenq
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引用次数: 1

Abstract

This document presents a technological breakthrough regarding electro-optics systems used for accurate measurement of the position of flying objects in Test Ranges. The innovation presented here consists in using an “Inertial Measurement Unit” (IMU) installed as close as possible to the optronic sensors in the core of the payload. After automatic alignment and self-calibration operations, the IMU delivers directly both accurate trajectory angles azimuth (true bearing) and elevation (above the horizontal plane).
轨迹惯性测量单元
本文介绍了用于精确测量试验场飞行物体位置的光电系统的技术突破。这里提出的创新包括使用“惯性测量单元”(IMU),安装在尽可能靠近有效载荷核心的光电传感器的位置。在自动对准和自校准操作之后,IMU直接提供精确的弹道角度、方位角(真实方位)和仰角(高于水平面)。
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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