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wind_jianmo_fangzhen
- 从风场的统计特性出发，建立了适用于弹道计算的简化风场模型。以这些模型为基础进行了弹道计 算.模拟了不同风场模型引起的弹箭射击误差，揭示了风与弹道误差的对应关系.为风修正弹箭设计提供了参考依据。 -Congfeng statistical properties of the starting field, the establishment of ballistics applicable to the simplified calculation of the wind field mo
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
Rocket-simulation
- 三级火箭弹道仿真，基于matlab环境对多级火箭的弹道进行六自由度的仿真，进而预测出每一级脱落后的落区-Three rocket trajectory simulation, matlab environment based on multistage rocket trajectory simulation conducted six degrees of freedom, and thus predict a fall off after each drop zone
dandao2
- 大气中的火箭弹道模拟，考虑空气阻力因素，用4阶龙格库塔解运动方程-Atmospheric rocket trajectory simulation, considering air resistance factor, with fourth-order Runge-Kutta solution of the equations of motion
ROCKET-TRAJECTORY-
- 提供龙格库塔积分程序，火箭入轨的判据。有一定的深度。具备相当的参考价值-provide Runge-Kutta calculus, fire arrow-format input . Have certain specific depth equivalent basis references
Equation-of-motion
- 铅锤平面内的弹道程序，但没有输入以及输出文件，通用程序可供参考-C of rocket s trajectory
waidandao
- 使用龙格库塔法对火箭弹水平轰炸弹道进行仿真-Using the Runge-Kutta method for level bombing rocket trajectory simulation
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
NX SRM Design 帮助文档
- 计算内弹道，固体火箭发动机装药内弹道计算(Calculating interior trajectory, solid rocket motor charge interior trajectory calculation)
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.)