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Rungerkutta4
- 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.
Missile--algorithms
- 导弹弹道分析算法,模拟实现两级火箭的弹道导弹飞行过程-Missile trajectory analysis algorithms, simulation of ballistic missiles to achieve two-stage rocket flight
huojiandandaojisuan
- 计算火箭飞行的弹道。采用欧拉法,龙哥库塔近似计算火箭飞行弹道。-Calculation of the rocket flight trajectory. Using Euler method, Long Ge Kuta approximate rocket flight trajectory.
missile
- 用于计算固体火箭弹道的仿真实例程序,绘制弹道仿真图像-Simulation example is used to calculate the trajectory of the solid rocket program, draw a trajectory simulation image
main
- 空间三维最优化三级运载火箭弹道求解算法。基于Matlab和GPOPS 5.2工具箱。实测收敛快,但对初值较敏感,轨道大于800km时需仔细调整参数。附带GPOPS 5.2工具箱和程序说明,可与STK接口。-Three dimensional space rocket trajectory optimization algorithm. Based on Matlab and GPOPS 5.2 toolbox. Found fast convergence, but more sensitive
Missile trajectory design
- 设计图形用户界面,直观的实现更改攻角、各级火箭喷射时间等参数后得到对应参数下的导弹弹道图像以及导弹的飞行时间和飞行距离。适合航天专业的初学者进行仿真测试。(The design of the graphical user interface, the intuitive implementation of the change attack Angle, the various levels of rocket injection time and other parameters to the
弹道导弹被动段
- 内附有弹道导弹弹道要求及过程,有完整的matlab程序,可以借鉴学习。自己大三时的远程火箭弹道学大作业。(t includes ballistic missile trajectory requirements and process, complete matlab program, which can be used for reference and learning. My junior year of long-range rocket ballistics homework.)