We use the concept of buffer boundedness based on the dynamic behavior of the markings in the system model.
基于系统模型标识的动态变化，以缓冲界限概念作为稳定性分析判据。
A dynamic model of the buffer seat was established according to the characteristics of the reentry capsule landing, equivalent land impact acceleration and work mechanism of the bumper.
根据返回舱着陆过程中的特点、等效的着陆冲击加速度和缓冲机构的工作原理，建立了缓冲座椅系统的动力学模型。
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