• The dynamical equations are expressed in terms of generalized coordinates and written in matrix term so that they can be easily used for calculating and program designing.

    该动力学方程组是以广义坐标表出并用矩阵形式表示,便于进行数值计算和程序设计。

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  • The results show that the inverse transfer function matrix is a normal matrix, and this fact is independent of the spacecraft dynamical parameters.

    研究结果表明,逆传递函数矩阵可视为正规矩阵,且动力学参数的摄动不影响其正规性。

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  • Elements by the highly-accuracy six-node triangular element are divided. Stiffness matrix and mass matrix of sandwich panel are established and then deduced dynamical equations of finite elements.

    应用高精度的六节点三角形单元进行单元划分,建立复合夹层板的刚度矩阵、质量矩阵并推导有限元动力学方程。

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  • By combining rigid disk element and 3-d beam element the dynamical control equation of flexible rotor system and its analysis formula of coefficient matrix are developed.

    将刚性圆盘单元和空间梁单元组集推导出了柔性转子系统的动力学控制方程及其系数矩阵的解析表达式。

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  • By combining rigid disk element and 3-d beam element the dynamical control equation of flexible rotor system and its analysis formula of coefficient matrix are developed.

    将刚性圆盘单元和空间梁单元组集推导出了柔性转子系统的动力学控制方程及其系数矩阵的解析表达式。

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