The multi-target rapid maneuver control problem is studied for agile satellites with Variable Speed ControlMomentGyro(VSCMG) as actuator.
研究了以变速控制力矩陀螺(VSCMG)作为执行机构的卫星多目标快速机动的控制问题。
2
The single gimbal controlmomentgyro (SGCMG) configuration of a large spacecraft is studied. First, the research object of analyzing configuration is restricted.
根据实际情况限定了大型航天器单框架控制力矩陀螺(SGCMG)构型分析研究的对象;
3
The design of a gradient singularity avoidance pseudo-inverse control law used for double gimbal controlmomentgyro (DGCMG), its principle and calculation were introduced.