即当阻尼器参数确定后，双自旋卫星姿态稳定取决于平台和转子的标称角速度。
After damper parameter is given , the stability of dual spinning satellites will lie on angular velocity of the flat floor and rotor .
带挠性附件双自旋卫星的Liapunov稳定准则
Liapunov Stability Criteria for Dual Spin Satellites with Flexible Appendages
双自旋稳定