由哈米尔顿原理作为动力学基础，建立起系统的非线性耦合运动方程组。
Based on the Hamiltonian principle, the coupled nonlinear functions of the system are presented as a Neumann problem.
根据国际标准ISO 5982规定的不同姿势下的竖向人体动力模型，建立了具有非经典阻尼的人与结构耦合运动方程。
The vertical human body models with different postures are selected according to ISO5982, and the dynamic coupling equations with non-classical damping for structure and human are established.
通过变换，给出太阳帆板、航天器中心刚体耦合运动微分方程组。
By transformation, the differential equation group of couple motions of solar wings and the central rigid body of the spacecraft is obtained.
通过变换，给出太阳帆板、航天器中心刚体耦合运动微分方程组。
By transformation, the differential equation group of couple motions of solar wings and the central rigid body of the spacecraft is obtained.
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