文件名称:GMisssileTraje
- 所属分类：
- Windows编程
- 资源属性：
- [Windows] [Visual C] [源码]
- 上传时间：
- 2012-11-26
- 文件大小：
- 66kb
- 下载次数：
- 2次
- 提 供 者：
- ywh***
- 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
通用弹道仿真计算程序源码V1.0本程序源码包为vxLand提供的经典版的通用导弹、炮弹、火箭弹等的弹道仿真计算程序源码，适用于无控*，用户能需要根据加入三点法、比例导引等导引方法，修改、扩充成相应的的有控、制导导模拟仿真弹道程序源码。程序源码包中MissileTrajectorySimulationRk.h的rk()是经典的4阶龙格库塔方法求常微分方程的数值算法的函数子程序源码，大家可参考使用。M
-The general trajectory simulation program source code V1.0 program source code to package provided for vxLand, classic Universal version of the missile, artillery, rockets and other ballistic simulation program source code and applies no control ammunition, users need to join the three-point method, such as proportional navigation guidance method, modify, expand into a corresponding to the control, guided guided simulation trajectory program source. Program source package in MissileTrajectorySimulationRk.h rk () is the classical 4th order Runge-Kutta method for solving ordinary differential equations numerical algorithms function subroutine source, we can use and reference. M
-The general trajectory simulation program source code V1.0 program source code to package provided for vxLand, classic Universal version of the missile, artillery, rockets and other ballistic simulation program source code and applies no control ammunition, users need to join the three-point method, such as proportional navigation guidance method, modify, expand into a corresponding to the control, guided guided simulation trajectory program source. Program source package in MissileTrajectorySimulationRk.h rk () is the classical 4th order Runge-Kutta method for solving ordinary differential equations numerical algorithms function subroutine source, we can use and reference. M
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下载文件列表
GMisssileTraje\MissileTrajectorySimulation\MissileTrajectorySimulation.Cpp
..............\...........................\MissileTrajectorySimulation.dsp
..............\...........................\MissileTrajectorySimulation.dsw
..............\...........................\MissileTrajectorySimulation.exe
..............\...........................\MissileTrajectorySimulation.h
..............\...........................\MissileTrajectorySimulation.ncb
..............\...........................\MissileTrajectorySimulation.opt
..............\...........................\MissileTrajectorySimulation.plg
..............\...........................\MissileTrajectorySimulationRk.Cpp
..............\...........................\MissileTrajectorySimulationRk.h
..............\...........................\MissileTrajectorySimulation_Input.dat
..............\...........................\MissileTrajectorySimulation_Input.dat.bak
..............\...........................\MissileTrajectorySimulation_Output.dat
..............\...........................\通用弹道仿真计算程序(经典版).txt
..............\MissileTrajectorySimulation
GMisssileTraje
..............\...........................\MissileTrajectorySimulation.dsp
..............\...........................\MissileTrajectorySimulation.dsw
..............\...........................\MissileTrajectorySimulation.exe
..............\...........................\MissileTrajectorySimulation.h
..............\...........................\MissileTrajectorySimulation.ncb
..............\...........................\MissileTrajectorySimulation.opt
..............\...........................\MissileTrajectorySimulation.plg
..............\...........................\MissileTrajectorySimulationRk.Cpp
..............\...........................\MissileTrajectorySimulationRk.h
..............\...........................\MissileTrajectorySimulation_Input.dat
..............\...........................\MissileTrajectorySimulation_Input.dat.bak
..............\...........................\MissileTrajectorySimulation_Output.dat
..............\...........................\通用弹道仿真计算程序(经典版).txt
..............\MissileTrajectorySimulation
GMisssileTraje