首页>
外国专利>
ATTITUDE CONTROL SYSTEM FOR SMALL SATELLITES
ATTITUDE CONTROL SYSTEM FOR SMALL SATELLITES
展开▼
机译:小卫星的姿态控制系统
展开▼
页面导航
摘要
著录项
相似文献
摘要
Various embodiments of the present invention include an attitude control system for use with small satellites. According to various embodiments, the system allows rapid retargeting (e.g., high slew rates) and full three-axis attitude control of small satellites using a compact actuation system. In certain embodiments, the compact actuation system includes a plurality of single-gimbaled control moment gyroscopes (SGCMG) arranged in a pyramidal configuration that are disposed within a small satellite.
展开▼