讨论了转子轴系统的偏心质量矩和轴承刚度对系统振动响应的影响。
The influence of eccentricity mass moment and the bearing stiffness to vibration characteristics of rotor system was discussed in detail.
通过建立三轴稳定质量矩拦截器的数学模型，得到一个非线性动力系统。
According to the constructed model of the mass moment interceptor with three-axial stabilization, a nonlinear dynamic system was acquired.
针对大气层内的机动飞行目标，提出了一种可用于质量矩拦截器末制导段的比例制导律。
Based on the constructed model of the mass moment interception missile (MMIM), a coupled nonlinear system is presented by rational simplification in this paper.
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