The steering laws of single gimbal control moment gyms (SGCMGs) are analyzed and compared for a spacecraft attitude control system based on the singular value decomposition (SVD) theory.

• 摘要基于奇异值分解理论，对航天器姿态控制系统中使用的单框架控制力矩陀螺(SGCMG)的操纵律进行了分析和比较研究。