期刊文献+

飞行员地面错觉模拟及其反应参考值 被引量:17

Pilot's ground-based spatial disorientation training and its reference values of response
原文传递
导出
摘要 目的 验证地面错觉训练方案在我军飞行员航空医学训练中应用的可行性,为评价地面错觉模拟训练效果提供参考值.方法 在我军现有错觉模拟训练方案基础上,参照北大西洋公约组织推荐的地面错觉模拟训练方案,依据现有的设备,对80名健康飞行员进行地面错觉模拟训练.在VTS-0型电动转椅上进行躯体旋动错觉、科里奥利错觉模拟,在VTS-Ⅲ型前庭功能检查系统上进行相对运动性错觉、自动性错觉模拟,观察错觉的诱发情况,并进行相应错觉反应参数(错觉持续时间、潜伏期)的记录.结果 躯体旋动错觉、科里奥利错觉、相对运动性错觉和自动性错觉的诱发率分别为100.0%、90.7%、72.5%和49.2%.前庭性错觉的诱发率要大于视性错觉(χ2=5.01,P〈0.05).飞行员躯体旋动错觉、科里奥利翻转错觉、科里奥利滚转错觉的持续时间分别为(8.4±4.5)s、(4.9±2.3) s、(5.4±3.0) s;相对运动性错觉、自动性错觉的潜伏期分别为(34.8±19.0) s、(42.8±15.2) s.5种错觉反应数据的参考值分别为:躯体旋动错觉持续时间≤17.4 s,科里奥利滚转错觉持续时间≤11.4 s,科里奥利翻转错觉持续时间为0.3~9.5 s,相对运动性错觉潜伏期≤72.8 s,自动性错觉潜伏期为12.4~73.2 s.结论 立足现有训练装备,我军飞行员躯体旋动错觉、科里奥利错觉、相对运动性错觉及自动性错觉的地面模拟训练方案是有效的、可行的.5种错觉反应数据的参考值可望为飞行员地面错觉模拟效果评价提供依据. Objective To validate the feasibility of applying ground-based spatial disorientation training scenarios to aeromedical training of Chinese military pilots and to provide reference values for assessing its effects. Methods Eighty healthy pilots performed ground-based spatial disorientation training on the basic of previously established aeromedical training profiles of Chinese Air Force and the scenarios applied by North Atlantic Treaty Organization (NATO) were referenced. Somatogyral illusion and Coriolis illusion were induced by VTS-0 type electric rotating chair, while circular vection and autokinetic illusion were induced by VTS-Ⅲ type vestibular function examination system. During the illusion demonstrations, the response parameters of illusion, including the latent period and the duration of induced illusions were recorded. Results The induced rate of somatogyral illusion, Coriolis illusion, circular vection and autokinetic illusion was 100.0%, 90.7%, 72.50% and 49.2% respectively. The induce rate of vestibular illusions was higher than that of visual illusions (χ2=5.01, P〈0.05). The duration of somatogyral illusion, Coriolis illusion (rolling sensation) and Coriolis illusion (tumbling sensation) was (8.4±4.5) s, (4.9±2.3) s and (5.4±3.0) s respectively, while the latent period of circular vection and autokinetic illusion was (34.8±19.0) s and (42.8±15.2) s respectively. The response reference value corresponding to the duration of somatogyral illusion, Coriolis illusion (rolling sensation) and Coriolis illusion (tumbling sensation) was respectively not more than 17.4 s, 11.4 s and between 0.3 and 9.5 s, while the response reference value for the latent period of circular vection and autokinetic illusion was respectively not more than 72.8 s and within the range from 12.4 to 73.2 s. Conclusions Somatogyral illusion, Coriolis illusion, circular vection and autokinetic illusion training scenarios can be demonstrated by the existing ground-based training devices of Chinese military pilots and the training is feasible and effective for aeromedical training of Chinese military pilots. We hope that response reference values can be used in assessing the effect of ground-based spatial disorientation training.
出处 《中华航空航天医学杂志》 CSCD 2011年第2期81-85,共5页 Chinese Journal of Aerospace Medicine
基金 全军医学科学技术研究"十一五"计划第二批专项课题(08Z015)
关键词 错觉 前庭 反应时间 科里奥利加速力 参考值 Illusions Vestibule Reaction time Coriolis force Reference value
  • 相关文献

参考文献21

  • 1Rayman RB, McNaughton GB. Sudden incapacitation.. USAF experience, 1970-80. Aviat Space Environ Med, 1983, 54(2) :161-164.
  • 2Bellenkes A, Bason Yacavone DW. Spatial disorientation in naval aviation mishaps: a review of class A incidents from 1980 through 1989. Aviat Space Environ Med, 1992,63 (2) : 128-131.
  • 3Lyons TJ, Ercoline WR, Freeman JE, et at. Classification problems of U.S. Air Force spatial disorientation accidents, 1989-91. Aviat Space Environ Med, 1994,65(2) : 147-152.
  • 4Lyons TJ, Ercoline W, O' Toole K, et al. Aircraft and related factors in crashes involving spatial disorientation: 15 years of U. S. Air Force data. Aviat Space Environ Med, 2006,77(7) :720-723.
  • 5Cheung B, Money K, Wright H, et al. Spatial disorienta- tion-implicated accidents in Canadian forces, 1982-92. Aviat Space Environ Med, 1995,66(6) :579-585.
  • 6罗永昌.空军卫生工作60年回顾与展望[J].航空军医,2009,:185-192.
  • 7Benson AJ. Spatial disorientation--a perspeetive//RTO/ NATO. RTO-MP-086 Spatial disorientation in military vehi- cles: causes, consequences and cures. Ottawa; St. Joseph Print Group Inc,2003:23-30.
  • 8Bles W. TR-HFM-118 Spatial disorientation training-- demonstration and avoidance. Soesterberg, Netherlands: North Atlantic Treaty Organization, 2008:42-44.
  • 9Previc FH, Ercoline WR. Spatial disorientation in aviation// Zarchan P. Progress in aeronautics and astronautics: Vol. 203. Reston,VA: AIAAInc., 2004:509-555.
  • 10Previc FH, Ercoline WR. Trends in spatial disorientation re- search. Aviat Space Environ Med,2001,72(11) : 1048-1050.

二级参考文献19

  • 1荣增平,陆斌,刘正,霍权,高升祥,于立身,魏凌.Coriolis加速度耐力检查中的错觉[J].中华航空医学杂志,1996,7(4):243-244. 被引量:2
  • 2涂通今.中国医学百科全书·军事医学[M].上海:上海科学技术出版社,1995.689-690.
  • 3詹皓,关宏.精神药物在战时调节飞行人员睡眠与抗疲劳中的应用[J].中华航空航天医学杂志,1997,8(1):48-51. 被引量:25
  • 4Clarke AH. Perspectives for the comprehensive examination of semicircular canal and otolith function. Biol Sci Space, 2001,15(4) :393-400.
  • 5Honrubia V, House M. Mechanism of posterior semicircular canal stimulation in patients with benign paroxysmal positional vertigo. Acta Otolaryngol,2001,121(2) :234-240.
  • 6Halmagyi GM, McGarvie LA, Aw ST,et al. The click-evoked vestibulo-ocular reflex in superior semicircular canal dehiscence.Neurology,2003, 60(7): 1172-1175.
  • 7Iida M, Hitouji K, Takahashi M. Vertical semicircular canal function: a study in patients with benign paroxysmal positional vertigo. Acta Otolaryngol,2001,545 (Suppl): 35-37.
  • 8Fetter M, Aw S, Haslwanter T, et al. Three-dimensional eye movement analysis during caloric stimulation used to test vertical semicircular canal function. Am J Otol, 1998,19(2): 180-187.
  • 9Young YH, Chiang CW, Wang CP. Three-dimensional analysis of post-caloric nystagmus caused by postural change. Acta Otolaryngol, 2001,545 (Suppl): 69-72.
  • 10yon Brevern M, Faldon ME, Brookes GB, et al. Evaluating 3D semicircular canal function by perception of rotation. AmJ Otol,1997,18(4) :484-93.

共引文献25

同被引文献112

引证文献17

二级引证文献56

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部