期刊文献+

无风条件下军用装备定点投放的数学建模及仿真 被引量:3

On Mathematical Modeling and Simulation of Fixed-point Drop of Military Equipment under Windless Condition
下载PDF
导出
摘要 以牛顿第二定律为基础,分析了降落伞和装备组成的伞物系统在空气中的受力情况,建立了无风、空气密度均匀条件下装备投放的微分方程模型。研究了装备在降落过程中的速度、迎角、降落时间、落地位置与飞机飞行高度、速度以及降落伞的关系,借助M ATLAB软件求常系数微分方程模型的数值解,对装备的降落过程进行模拟仿真。利用仿真结果对实际装备的投放操作进行指导,可以达到更好的投放效果。 On the basis of Newton's Second Law of Motion, air force of the umbrella system made up of parachute and equipment is analyzed and constant coefficient differential equation model of equipment drop under the condition of no wind and equal air density is established. The relationship between the speed, angle of attack, landing time, landing position of the equipment at the process of drop and the flying height and speed of the plane and the parachute is researched. Meanwhile, the process of the parachute dropping is simulated through constant coefficient differential equation model in virtue of software MATLAB. If guided by the result of the simulation, better effect of actual dropping operation of the equipment could be achieved.
出处 《火力与指挥控制》 CSCD 北大核心 2012年第10期43-45,共3页 Fire Control & Command Control
基金 海军工程大学科研基金资助项目(HGDJJ08001)
关键词 空气阻力系数 收尾速度 迎角 离散化 仿真 air resistance coefficient, terminal velocity, angle of attack, discrete solution, simulation
  • 相关文献

参考文献8

二级参考文献13

  • 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
  • 3刘浩然,王冠.DSP环境下C代码的手工汇编优化[J].现代电子技术,2006,29(12):92-95. 被引量:5
  • 4Texax Insrtuments. TMS320C55x DSP Library Progrmnme' s Reference( spm,422i ) [ Z]. Texax Insrtuments ,2006.
  • 5Krolik J. Time delay estimation via generalized correlation with adaptve spatial prefiltering [ J ]. ICASSP' 86, 1986,20 (35) :1 -4.
  • 6Reed F A. Time delay estimation using the LMS adaptive tilers-static behavior [ J ]. IEEE Trans, 1981,29 (3) :561-571.
  • 7Desabrais K J.Velocity field measurements in the near wake of a parachute canopy[D].Worcester,MA:Worcester Polytechnic Institute,2002:1-6.
  • 8Watkins 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.
  • 9Arai N,Suzuki K.Inflation process and free oscillation of flexible parachute-like body[C]//18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar.Munich,Germany,2005:AIAA-2005-1610.
  • 10Doherr K.Extended parachute opening shock estimation method[C]//17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar.Monterey,California,2003:AIAA 2003-2173.

共引文献58

同被引文献23

引证文献3

二级引证文献6

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