搜索资源列表
noncontrol-ballistic-simulation
- Matlab编写的纵向平面内无控弹道仿真程序，（内含气动数据），采用线性插值与4阶龙格库塔法解算常微分方程组-The longitudinal plane Matlab prepared uncontrolled trajectory simulation program (includes aerodynamic data), using linear interpolation with four first-order Runge-Kutta method ODE solver
proportional-guidance
- 用Matlab编写的铅垂平面内的比例导引方案弹道程序，目标为水平面内的平动物体-Proportional navigation scheme with ballistic programs written in Matlab vertical plane, the target for the level of animal body in a horizontal plane
ballis
- A method for the determination of the trajectory of a ballistic missile over a rotating, spherical Earth given only the launch position and impact point has been developed. The iterative solution presented uses a state transition matrix to correc
DATCOM
- 弹道计算工具，包括文档说明，和相关源代码，好东西-Ballistic calculation tools, including documentation, and related source code, good things
youhuaguocheng
- 我写的这个是对弹道飞行轨迹的优化过程，大家一起学习交流.- 请键入文字或网站地址，或者上传文档。 取消 Wǒ xiě de zhège shì duì dàndào fēixíng guǐjī de yōuhuà guòchéng, dàjiā yì qǐ xuéxí jiāoliú.I wrote this is a ballistic trajectory optimization process, with everyone learning exchanges
shizhongxiugai_v1
- 89c51的数字钟程序，在keil里边一。当弹道弹道弹道弹道导弹-89C51 the digital clock procedures, in a keil inside. When the ballistic trajectory of ballistic missile
CCRP
- 采用连续计算命中点方法投放炸弹的弹道解算-Using a continuous method of calculating the hit point bombs ballistic solver
vbdatm
- VisualBasic6.0编写的底排弹内弹道程序注释丰富；底排弹内弹道数值流场仿真计算，程序编译通过可直接运行，并附带结果和图像供参考。像是一个民爆企业的内部火药计算程序，具体的换算关系不是太懂，是别人发过来让分享的VB源码，可用VB6顺利编译。 Module1模块：用于定义全局变量，函数fun()和xztel()，fun函数：用于实现四阶龙格库塔法解微分方程右端子式，xztel函数：用于计算火药特征尺寸-Ballistic rich program notes written in
Calculate
- 采用瞬时平衡假设，计算导弹的理想弹道，命中精度0.35米-Instantaneous equilibrium assumption, calculate the ideal ballistic missile hit accuracy 0.35 m
trajectory
- 用4阶龙格库塔法求解给定攻角情况下的空地导弹弹道。-to solve a given Angle of attack of the ballistic missile with a four order runge kutta method.
Missile-algorithm
- 基于MATLAB导弹仿真源代码(missile simulation) 给出了比例导引法的差分方程, 采用Matlab语言, 对比例导引法的导弹理想弹道进行了三维数据仿真, 绘制出三维理想弹道。随导弹与目标参数变化情况, 对理想弹道的特性进行了分析-Missile simulation based on MATLAB source code (missile simulation) Differential equation gives the proportiona
donghua
- 应用龙哥库塔法求解弹道并且模拟弹道的轨迹，及其对比图-Long 哥库塔 track application and simulation method for solving ballistic trajectory, and its comparison chart
standardtrajectory
- 导弹标准弹道计算，可以给出飞行过程中的高度、速度、攻角等信息-Ballistic Missile standards can be given during the flight altitude, speed, angle of attack and other information
sanwei
- 增量比例导引算法，可用于弹道目标的拦截等处理-Interception increment proportional navigation algorithm can be used for ballistic targets handling
zengliangbiliyindao
- 一组有意义的弹道导弹增量比例引导弹道仿真弹道分析程序，分别用一维、二维插值等方法对弹道导弹的弹道进行了仿真，分析了其弹道特性-A set of meaningful ballistic missile incremental proportion guide ballistic trajectory simulation analysis program, with one-dimensional and two-dimensional interpolation method for the
KKVbiaozhundandao
- KKV标准弹道仿真程序，仿真了KKV在中段拦截TBM的弹道。供大家参考。-KKV standard ballistic simulation program, the simulation of KKV in the middle of the TBM interception trajectory.For your reference.
jisuandandaochengxu
- 某炮弹质量为20KG，直径120mm，出炮口是的初速为800m/s，初始发射角等于45°，试计算弹道。解答过程与程序详解-A shell quality is 20 kg, 120 mm in diameter, out of the muzzle velocity of 800 m/s, initial emission Angle is 45 °, try ballistic calculation. The solution process and procedure, rounding
jindianneidandaoc
- 基于龙格库塔的经典内弹道的计算，很不错的文件。-Within the classical Runge-Kutta-based ballistic calculations
EKFTracking
- tarcking a ballistic target
Analysis-of-a-single-stage-compressed-gas-launche
- Single stage compressed gas guns are used in Shock Physics laboratory to perform characterization experiments and ballistic events. The main advantage of this kind of launcher is that impact conditions are well defined (impact obliquity, impact