摘要
本文介绍了对地定向三轴稳定卫星的圆锥扫描式地球敏感器的姿态测量原理、输出几何关系和数学模型。
The attitude determination theory, geomelric relation between the outputs and mathematical model of the cone scanning earth sensor for the earth pointing three axis stablized satellite are presented in the paper, and some examples are also given to illustrate the necessity of paying much attention to the coupling problem between axes in the attitude control of large angle maneuver.
出处
《航天控制》
CSCD
北大核心
1995年第4期14-21,共8页
Aerospace Control
