此外，文中还提出了改进挠性轴陀螺转子动平衡的一些建议。
Furthermore some Suggestions for improving the balancing of a flexible gyrorotor are presented.
此外，文中还提出了改进挠性轴陀螺转子动平衡的一些建议。
Furthermore some Suggestions for improving the balancing of a flexible gyrorotor are...
螺杆钻具挠性轴设计中的两个主要问题是强度校核和干涉量计算。
The main Problems with designing the flexible shaft on a screw drill are strength check and interference calculation.
通过对计算结果的分析，找出挠性轴设计中存在的问题，并提出相应改进意见。
By analyzing the calculation result, the problem existed in the design of flexible shaft was found out and corresponding improvement measure was put forward.
挠性轴强度校核主要是校核疲劳强度，为此提出了合理设计挠性轴的原则，即挠性轴的疲劳强度应取决于扭转疲劳强度。
Therefore the design criterion for the shaft is proposed, i. e. the fatigue strength of the shaf should depend on the torsional fatigue strength.
在挠性卫星动力学模型的基础上，建立了只考虑太阳帆板三阶振动模态的挠性卫星三轴姿态控制模型。
The three-axis attitude stabilization system of the flexible satellite has been studied, in which three basic vibration modes of the solar array have been considered.
传动轴需采取合适的挠性连接方式。
Transmitting shaft must be connected with suitable flexible coupling.
从挠性陀螺组合安装误差模型入手，推导出存在轴不对准角情况下的挠性陀螺组合静态误差标定模型，并给出静态误差标定的位置试验方案。
The installation error model of the gyroscope integrated is analyzed, and then error calibration model of flexible gyroscope integrated is deduced when malalignment Angle is considered.
研究三轴稳定的挠性航天器姿态的鲁棒控制问题。
The problem of robust attitude control for three-axial-stabilized flexible spacecraft is considered.
本文应用区间矩阵的理论，研究三轴稳定的挠性空间飞行器姿态控制系统的鲁棒稳定性分析问题。
In this paper, the robustness stability analysis of the attitude control system of a three-axis stabilized flexible spacecraft is investigated.
本文应用区间矩阵的理论，研究三轴稳定的挠性空间飞行器姿态控制系统的鲁棒稳定性分析问题。
In this paper, the robustness stability analysis of the attitude control system of a three-axis stabilized flexible spacecraft is investigated.
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