摘要
介绍了卫星惯性姿态敏感器(IAS)的工作原理,分析了惯性姿态敏感器设计及关键技术。通过比较各种惯性姿态敏感器的优缺点,分析了卫星惯性姿态敏感器的发展历程,探讨了卫星用惯性姿态敏感器的发展方向。
The principle of inertial attitude sensor (IAS) in satellite is introduced in this paper, and also are the design and key technology of IAS. The development course of IAS is presented through the comparison of advantages and disadvantages among different sensors. The trend to develop IAS in satellite is analyzed at last.
出处
《上海航天》
2003年第5期33-37,共5页
Aerospace Shanghai
