航天器姿态控制系统的控制力矩陀螺仪:发展历史

Q2 Computer Science

Gyroscopy and Navigation Pub Date : 2022-06-16 DOI:10.1134/s2075108722010060

A. V. Sorokin, V. V. Yaremenko

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引用次数: 0

摘要

摘要本文介绍了用于航天器主动三轴姿态控制的控制力矩陀螺仪的研制与应用。这些陀螺仪属于惯性致动器类，其中还包括飞轮控制电机、陀螺仪阻尼器和被动陀螺仪稳定器。控制力矩陀螺仪(CMG)的一个显著特征是存在特殊的驱动器来控制陀螺仪相对于其悬架轴的旋转。通过调节这种旋转的速度，驱动器产生所需的控制力矩。介绍了俄罗斯CMG及其基础系统的主要发展阶段、设计和体系结构特点、应用问题和发展趋势。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

Control Moment Gyroscopes for Spacecraft Attitude Control Systems: History of Development

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Control Moment Gyroscopes for Spacecraft Attitude Control Systems: History of Development

Abstract

The article is devoted to the development and application of control moment gyroscopes used for active triaxial attitude control of spacecraft. These gyroscopes belong to the class of inertial actuators, which also includes flywheel control motors, gyro dampers, and passive gyrostabilizers. A distinctive feature of control moment gyroscopes (CMG) is the presence of special drives that control the rotation of the gyroscope relative to its suspension axes. By regulating the speed of this rotation, the drive creates the required control moment. The paper describes the main development stages of Russian CMG and systems based on them, the features of their design and architecture, application issues and development trends.

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来源期刊

Gyroscopy and Navigation Computer Science-Computer Science (all)

CiteScore

2.80

自引率

0.00%

发文量

期刊介绍： Gyroscopy and Navigation is an international peer reviewed journal that covers the following subjects: inertial sensors, navigation and orientation systems; global satellite navigation systems; integrated INS/GNSS navigation systems; navigation in GNSS-degraded environments and indoor navigation; gravimetric systems and map-aided navigation; hydroacoustic navigation systems; navigation devices and sensors (logs, echo sounders, magnetic compasses); navigation and sonar data processing algorithms. The journal welcomes manuscripts from all countries in the English or Russian language.