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
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