首页> 外文会议>AAS/AIAA Space Flight Mechanics Meeting Vol.112 Pt.1, Jan 27-30, 2002, San Antonio, Texas >DEVELOPMENT OF INERTIAL MEASUREMENT SENSOR USING MAGNETIC LEVITATION
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DEVELOPMENT OF INERTIAL MEASUREMENT SENSOR USING MAGNETIC LEVITATION

机译:利用磁悬浮技术开发惯性测量传感器

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An INS(Inertial Navigation System) is composed of a navigation computer and an IMU(Inertial Measurement Unit), and can be applied to estimate a vehicle's state. But the inertial sensors assembled in the IMU are too complicated and expensive to use for the general application purpose. In this study, a new concept of inertial sensor system using magnetic levitation is proposed. The proposed system is expected to replace one single-axis rate or position gyroscope, and one single-axis accelerometer concurrently with a relatively simple structure. A simulation of the proposed system is given tc describe the capability of this new concept.
机译:INS(惯性导航系统)由导航计算机和IMU(惯性测量单元)组成,可用于估算车辆的状态。但是组装在IMU中的惯性传感器太复杂且昂贵,以至于不能用于一般应用目的。在这项研究中,提出了一种利用磁悬浮惯性传感器系统的新概念。拟议的系统有望以相对简单的结构同时取代一台单轴速率或位置陀螺仪和一台单轴加速度计。给出了拟议系统的仿真,以描述该新概念的功能。

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