文件名称:Rungerkutta4
- 所属分类:
- 数学计算/工程计算
- 资源属性:
- [Windows] [Visual C] [源码]
- 上传时间:
- 2012-11-26
- 文件大小:
- 202kb
- 下载次数:
- 0次
- 提 供 者:
- d**
- 相关连接:
- 无
- 下载说明:
- 别用迅雷下载,失败请重下,重下不扣分!
介绍说明--下载内容均来自于网络,请自行研究使用
该程序利用4阶龙格库塔方法解二阶常微分方程,该微分方程描述火箭发射时质心运动轨迹。-The program uses the 4th order Runge-Kutta method of second order ordinary differential equations, differential equations describe the mass center when the rocket trajectory.
(系统自动生成,下载前可以参看下载内容)
下载文件列表
Rungerkutta4\123.dsp
............\123.dsw
............\123.ncb
............\123.opt
............\123.plg
............\Debug\123.exe
............\.....\123.ilk
............\.....\123.pch
............\.....\123.pdb
............\.....\Text3.obj
............\.....\Text3.obj.enc
............\.....\vc60.idb
............\.....\vc60.pdb
............\Text3.c
............\Debug
Rungerkutta4
............\123.dsw
............\123.ncb
............\123.opt
............\123.plg
............\Debug\123.exe
............\.....\123.ilk
............\.....\123.pch
............\.....\123.pdb
............\.....\Text3.obj
............\.....\Text3.obj.enc
............\.....\vc60.idb
............\.....\vc60.pdb
............\Text3.c
............\Debug
Rungerkutta4