The relation among parameters is derived and the stability of single axis flexible spacecraft attitude control system is studied.
推导系统参数间的关系式，分析挠性空间飞行器主轴姿态控制系统稳定性问题。
The relation among parameters is derived and the stability of single axis flexible spacecraft attitude control system is studied.
推导系统参数间的关系式，分析挠性空间飞行器主轴姿态控制系统稳定性问题。
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