低重力环境下复杂结构航天器动特性研究的实现途径

WAYS FOR CHARACTERISATION OF COMPLEX STRUCTURAL SPACECRAFT IN LOW GRAVITY ENVIRONMENT

文章从试验技术与理论计算结合的角度,对解决复杂结构航天器低重力环境下大幅度液体晃动非线性动态特性问题和模拟月球重力环境下月球探测器动力学性能的研究,进行了建设性的论述。

Some discussions are given on solving the nonlinear dynamic characteristic problem of large amplitude liquid sloshing for complex structural spacecrafts in low gravity environment and that of the lunar surface vehicle in simulated lunar gravity environment from the view point of combination of the testing technology and theoretical calculation.