This paper extends his method and derives the stability condition for the spin Spacecraft with Cavities partially filled with liquid, that is I2>Ix+I2. I1 and I2 are positive definite functions of the spacecraft parameters.

• 本文推广他的方法；导出了空腔充液自旋卫星的稳定性条件；即I_z>I_x+I_2。 I_1及I_2是卫星参数的正定函数；且I_2