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1)  principal axes of inertia
惯量主轴
1.
The method to calculate principal axes of inertia by adjoint matrix of eigen ma-trix is given,examples are presented.
本文给出了用特征矩阵的伴随矩阵求惯量主轴的代数方法,并通过实例作了说明。
2.
This paper presents the eigen equation of inertial tensor expressed by the three principal invariants, which is an algebra-equation solution to calculate eigen value;proves that eigenvalue is the principal moments of inertia and that eigenvector is the principal axes of inertia;and discusses a certain method to calculate prinpal axes of inertia by adjoint matrix of eigen matrix.
本交给出了惯量张量用其三个主要不变量表示的特征方程,为求特征值提供了一种代数方程解法;论证了特征值即为主惯量,特征矢量即为惯量主轴;探讨了用特征矩阵的伴随矩阵求惯量主轴的方法,并用实例给予了说明。
2)  principal axis of inertia
惯量主轴
1.
In rigid body mechanics, confirming the principal axis of inertia of rigid body is particularly important, its calculation can be made to be simplified and favorable to study the nature and movement law of rigid body.
刚体力学中,确定刚体的惯量主轴,可以简化计算,还有利于研究刚体的性质和运动规律,这样,如何确定刚体的惯量主轴就显得尤为重要。
2.
The principal axis of inertia of a rigid body are its symmetric axis,the rigid body is possessed of geometrical symmetry and its mass are well distributed or its mass are symmetrially distributed.
对于具有几何对称性且质量均匀分布或质量对称分布的刚体,其惯量主轴显而易见,即刚体的对称轴。
3)  the center inertia principal axis
中心惯量主轴
4)  principal axis of inertia
主惯性轴
1.
The technology of the principal axis of inertia measurement mostly applies to the field of spaceflight and missile.
主惯性轴测量技术主要应用在航空航天和导弹研究方面,早期的产品和设计精度不要求对主惯性轴进行测量,并且,由于应用范围的特殊性,主惯性轴测量设备和测量技术一直是处在保密状态,因此,仅有非常有限的文献报道过该技术的研究情况。
5)  principal inertia axis
主惯性轴
1.
The inclination between the rotator s principal inertia axis and circumrotatory axis has been given with its couple imbalance value measured by the machine.
提出了一种将一垂直扭杆安装于双面立式动平衡机主轴内 ,用于测量转子的转动惯量的方法 ,并结合动平衡机所测出的转子偶不平衡量 ,给出转子主惯性轴与参考轴 (旋转轴 )之间的夹角 。
6)  inertial principal axis
惯性主轴
1.
An algorithm for oblique license plate correction is proposed based on the corner point information and inertial principal axis.
提出了一种基于字符角点信息和惯性主轴的车牌倾斜角检测方法。
2.
In order to measure the inertial principal axis of projectile precisely to ensure the flight stability and hit probability,the two-facade four-point method of inertial principal axis was applied.
为了准确测定弹箭的惯性主轴位置以保证弹箭的飞行稳定性和命中率,采用惯性主轴的双立面四点法,分析了测试过程中各截面质心的位置,根据力矩平衡得到弹箭惯性主轴的实际位置。
补充资料:惯量主轴
      见惯量张量。
  

说明:补充资料仅用于学习参考,请勿用于其它任何用途。
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