航天员上肢典型动作的动力学仿真与分析  

Mechanical Simulation and Analysis of Typical Upper Limb Movements of Astronauts

在线阅读下载全文

作  者:殷梦馨 汪圣伟 叶青 李静文[3] 丁立[3] YIN Mengxin;WANG Shengwei;YE Qing;LI Jingwen;DING Li(Wuhan 2nd Ship Design and Research Institute,Wuhan 430064,China;China University of Mining and Technology(Beijing),Beijing 100083,China;School of Biological and Medical Engineering,Beihang University,Beijing 100191,China)

机构地区:[1]武汉第二船舶设计研究所,武汉430064 [2]中国矿业大学(北京),北京100083 [3]北京航空航天大学生物与医学工程学院,北京100191

出  处:《载人航天》2023年第6期735-743,共9页Manned Spaceflight

摘  要:针对航天员人机交互过程中的操作工效学问题,基于航天员上肢典型动作的力学问题进行仿真分析。考虑上肢的运动特点,利用反向运动学和动力学Kane法进行关节力矩模型和简化肌肉力模型的求算,并针对上肢7自由度冗余问题采用梯度投影算法进行处理。结果表明:搭建的7自由度冗余模型计算结果接近人体真实情况,为了实现开舱门动作的方便性以及考虑设计的冗余量,舱门宽度应尽量避免超过0.6 m;通过分析点按动作在不同的按钮高度条件下的仿真结果,得出按钮高度为0(按钮与肩同高)时,上肢各关节综合负担相对最优。The study addressed the ergonomic issues in the human-machine interaction process for astronauts,focusing on the mechanical aspects of typical upper limb movements.Considering the characteristics of upper limb motion,the research employed inverse kinematics and the Kane method in dynamics to calculate joint torque models and simplified muscle force models.To address the redundancy problem of the upper limb's 7 degrees of freedom,a gradient projection algorithm was applied.The results indicated that the calculated results of the constructed 7-degree of freedom redundant model were close to the real human situation.For the convenience of hatch opening and considering the redundancy in design,the hatch width was recommended to avoid exceeding 0.6 meters.Through the analysis of simulated results of pressing actions under different button heights,it was concluded that a button height of 0(aligned with the shoulder) resulted in a relatively optimal overall joint burden for the upper limb.

关 键 词:航天员 冗余自由度 反向运动学 Kane法 仿真 

分 类 号:R857.1[医药卫生—航空、航天与航海医学] TP391[医药卫生—临床医学]

 

参考文献:

正在载入数据...

 

二级参考文献:

正在载入数据...

 

耦合文献:

正在载入数据...

 

引证文献:

正在载入数据...

 

二级引证文献:

正在载入数据...

 

同被引文献:

正在载入数据...

 

相关期刊文献:

正在载入数据...

相关的主题
相关的作者对象
相关的机构对象