针对基于地面模拟试验传统设计方法难以对全向式多室连通气囊进行优化设计的问题,
采用基于有限元仿真, 试验及多目标优化相结合的方法对该气囊系统进行了优化设计 …

针对多重不确定性因素对缓冲气囊防护特性的影响, 提出一种基于概率-椭球混合模型的缓冲
气囊防护特性可靠性分析方法. 首先, 利用概率模型和椭球凸集模型对装备空降过程中的不确定 …

针对不确定因素对载人空降气囊座椅防护性能的影响, 提出一种基于概率-
概率盒混合模型的气囊座椅防护特性可靠性分析方法. 研制空降乘员气囊座椅 …

In this paper, the approximation non-linear interval number programming (A-NINP) method
is suggested to obtain the optimal buffering characteristics of a landing airbag in manned …

The present study aims at designing a seat position to preserve the safety of occupants
under acceleration and impact loads of landing conditions. So, using astronaut multi-body …

Abstract Design of spacecraft seat which preserves astronaut׳ s safety against sustained
acceleration and impact loads is presented. A novel multi-body dynamics model of seat …

Subject to the limitations of the traditional design method based on the experiments on the
earth to solve the problem of the optimization design for omni-directional multi-chamber …

针对某军用车辆在1 m 高度进行无缓冲平台空投实验, 并建立座椅与乘员的模拟模型.
利用实验获取的座椅安装点冲击信号作为模拟模型的输入数据, 并通过实验结果与模拟结果的 …

In this paper, an efficient multi-objective optimization method for the optimization of astronaut
landing position is presented. The finite element model is employed to simulate the airdrop …

Considering the influence of multi-source uncertainties on airbag protection performance, a
hybrid reliability approach based on probability and ellipsoidal convex models is presented …