Attitude sensitivity and stability are the important technical features of satellite. Measuring satellite attitude with star sensor is a present measuring technique with highest accuracy.
姿态敏感和姿态稳定是卫星的重要技术之一，星体敏感器是目前最高精度的姿态测量技术。
Since the measurement of the yaw angle is unavailable by horizon sensor, an attitude control scheme of the satellite is proposed based on yaw observer.
由于采用的红外地平仪无法测量卫星的偏航信息，提出了一种基于偏航观测器的姿态控制方案。
The principle of inertial attitude sensor (IAS) in satellite is introduced in this paper, and also are the design and key technology of IAS.
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。
应用推荐