首页>
外国专利>
Singularity avoidance in satellite attitude control
Singularity avoidance in satellite attitude control
展开▼
机译:卫星姿态控制中避免奇点
展开▼
页面导航
摘要
著录项
相似文献
摘要
Control moment gyros in an array are rotated to reorient a satellite by an attitude signal. If the signal causes a gyro to have position that will produce a singularity in attitude control, a disturbance is introduced into the signal to avoid the singularity.
展开▼