Measuring Attitude Rates Through Angular Momentum Gyros

Hong-Hua Zhang

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Measuring Attitude Rates Through Angular Momentum Gyros

机译：通过角动量陀螺仪测量姿态速率

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STABLE attitude pointing is required for some remote sensing satellites to get high-resolution imaging. A sensor for measure- ing angular rates with high accuracy is necessary for the attitude control system because the accuracy of the angular rates principally determines the stability of the controlled spacecraft. This Note is devoted tot he description of a sensor called the angular momentum gyro (AMG).

机译：一些遥感卫星需要稳定的姿态指向，才能获得高分辨率的图像。姿态控制系统需要一个用于高精度测量角速度的传感器，因为角速度的精度主要决定了受控航天器的稳定性。本说明专门介绍称为角动量陀螺仪（AMG）的传感器。

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《Journal of Spacecraft and Rockets》 |1999年第6期|p.919-920|共2页
作者
Hong-Hua Zhang;
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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类航空;
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Measuring Attitude Rates Through Angular Momentum Gyros

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