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伞兵轨迹测量与过载预测方法研究

Paratrooper Track Measurement Method and Estimation of Overload
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摘要 论文在分析伞兵降落过程中自由坠落阶段和充气阶段运动的基础上,提出了一种伞兵轨迹测量与过载预测的方法。飞行试验结果表明该方法对于伞兵轨迹的测量与过载的预测满足工程测量的精度要求。这种方法不受空投高度、天气等条件的限制,操作简单,成本低。可用于空降试飞或其他领域内的轨迹测量。 Based on the analysis during free fall parachutist's landing stage and inflatable foundation phase of the campaign,aparatrooper track measurement method and estimation of overload are proposed.Flight test results show that the method for paratrooper track measurement and the prediction of overload meet the accuracy requirements of engineering survey.This method is not restricted by drop height,weather and other conditions,whose operation is simple and cost is low.It can be used for flight test for drop by parachute or other areas of track measurement.
作者 吉宁 惠广裕
出处 《计算机与数字工程》 2016年第5期805-808,共4页 Computer & Digital Engineering
关键词 伞兵降落 轨迹 开伞动载 测量 预测 paratroopers landed track overload of parachute measurement estimation
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  • 1江桂清.降落伞风洞试验中的几个主要问题[J].航空学报,1993,14(6). 被引量:4
  • 2龚文轩.降落伞附加质量与开伞动载[J].航空学报,1995,16(1):84-86. 被引量:11
  • 3Desabrais K J. Velocity field measurements in the near wake of a parachute canopy [ D ]. Massachusetts : Worcester Polytechnic Institute, 2002.
  • 4Lee C K, Lanza J, Buckley J, et al. Experimental investiga- tion of clustered parachutes inflation[ R]. AIAA-97-1478, 1997.
  • 5Tribot J P, Chalot F. Lardge gliding parachute experimen- tal and theoretical approaches[ R]. AIAA-97-1482,1997.
  • 6Lee C K. Experimental investigation of full-scale and mod- el parachute opening[ C ]//AIAA 8th Aerodyn & Balloon Technology Conference. Hyannis, MA, April 2-4, 1984: 215 -223.
  • 7Johnson X, Yakimeoko O, Kaminer I, et al. On the devel- opment and pre-flight testing of the affordable guided air- drop system for G-12 cargo parachute [ R ]. AIAA-2001- 2060,2001.
  • 8匿名著者,降落伞技术导论,1977年
  • 9Desabrais K J.Velocity field measurements in the near wake of a parachute canopy[D].Worcester,MA:Worcester Polytechnic Institute,2002:1-6.
  • 10Watkins J W.A total energy method to predictparachute canopy inflation forces[C]//17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar.Monterey,California,2003:AIAA-2003-2166.

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