首页 | 本学科首页   官方微博 | 高级检索  
     

不同轴向的径向加速度对科里奥利错觉的影响
引用本文:谢溯江,于立身,毕红哲,贾宏博,刘正,穆大为. 不同轴向的径向加速度对科里奥利错觉的影响[J]. 中华航空航天医学杂志, 2002, 13(2): 77-80
作者姓名:谢溯江  于立身  毕红哲  贾宏博  刘正  穆大为
作者单位:1. 100036,北京,空军航空医学研究所
2. 100036,北京,空军总医院
摘    要:
目的 X、Y轴向的径向加速度对科里奥利错觉的影响。方法 分别对10名青年男性健康志愿者在GL-2000高级空间定向模拟器上,由X轴向径向加速度为 0.27Gx与0Gz时,Y轴向径向加速度为 0.27Gy或0Gy时等量的科里奥利加速度刺激(0.16cm/s^2)引起的科里奥利错觉形态、持续时间、强度进行了比较。结果 同无径向加速度作用相比,在X轴向径向加速度为0.27Gx及Y轴向径向加速度为0.27Gy时,等量的科里奥利加速度刺激引起的科里奥利错觉形态不改变,错觉持续时间明显降低(P<0.05),错觉强度明显增强(P<0.05)。结论 X、Y轴向径向加速度对科里奥利错觉形态无影响,对错觉持续时间及强度均有一定影响,必须加强对径向加速度作用下的科里奥利错觉的预防与克服措施的研究。

关 键 词:科里奥利加速度 错觉 引力 模拟器
修稿时间:2001-11-15

The effect of Gx and Gy on Coriolis illusion
XIE Sujiang,YU Lishen,BI Hongzhe,et al.. The effect of Gx and Gy on Coriolis illusion[J]. Chinese Journal of Aerospace Medicine, 2002, 13(2): 77-80
Authors:XIE Sujiang  YU Lishen  BI Hongzhe  et al.
Affiliation:XIE Sujiang,YU Lishen,BI Hongzhe,et al. Institute of Aviation Medicine,Air Force,Beijing 100036,China
Abstract:
Objective To explore the effect of different axial(X or Y axis) radial acceleration on Coriolis illusion. Methods Ten healthy young men served as subjects. The experiments were performed in GL 2000 advanced spatial disorientation simulator. The form, duration, and intensity of Coriolis illusion induced by equated Coriolis acceleration stimulations with and without the effect of 0.27 G x or 0.27 G y were observed and compared. Results As compared with those without the effect of G x or G y, under the effect of 0.27 G x or G y, the form of Coriolis illusion remained the same, while its duration was significantly shortened( P <0.05), and its intensity significantly increased( P <0.05). Conclusion Viewing that radial and angular accelerations often occur simultaneously during maneuvers of high performance fighter, it is suggested studies about measures for preventing and overcoming Coriolis illusion under the effects of radial acceleration should be strengthened.
Keywords:Coriolis acceleration  Illusion  Gravitation  Simulator
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号