航天器随机振动设计载荷比较

Comparison Between Spacecraft Design Load of Random Vibration

将直接影响航天器结构质量的随机振动载荷等效为准静态的设计载荷,是航天器结构设计分析中的一项重要内容。文章简要介绍了基于加速度峰值响应等效的设计载荷与基于位移峰值响应等效的设计载荷的原理与方法;重点运用解析法与有限元仿真比较了两种方法的差别,分析得出基于加速度的设计载荷要大于基于位移的设计载荷。文章推荐使用基于位移峰值响应等效的设计载荷,该方法将有效减轻结构质量。

It is an important step for spacecraft design and analysis to convert random vibration load to quasi static design load, which influences mass of spacecraft structure directly. The theory and methods of design load based on the peak value of acceleration response and displacement response were simply introduced. The differences between the two methods were compared by analytics and FEM. The design load based on the peak value of acceleration response is larger than that based on the peak value of displacement response. The design load based on the peak value of displacement response is recommended and will lighten mass of spacecraft structure.