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trajectory1.C语言计算导弹弹道
- C语言计算导弹弹道,C语言计算导弹弹道 ,C language calculated ballistic missiles, C language calculated ballistic missile
zyzd.rar
- 最优制导律反战术弹道导弹TBM弹道仿真，matlab编写。,Optimal Guidance Law TBM anti-tactical ballistic missile trajectory simulation, matlab prepared.
duidaodanjinxingdandaofenxi
- 这段代码是对导弹进行弹道分析，用MATLAB运行。-The code is a ballistic missile analysis, using MATLAB to run.
弹道分析
- 用matlab来编写的较复杂的程序，用来对导弹进行弹道分析-prepared using Matlab to the more complex procedures for the analysis of ballistic missile
1
- matlab程序 防御系统弹道导弹目标识别方面的matlab程序-matlab program of ballistic missile defense system target identification procedures matlab
dandaofenxi
- 复杂情况下的弹道分析仿真。对于导弹专业的理论仿真很实用。-Complex case of ballistic analysis simulation. For the theoretical simulation of the missile professional practical.
atbm
- 反战术导弹导弹比例导引律三维弹道仿真程序.-The proportion of anti-tactical ballistic missile missile guidance law of three-dimensional trajectory simulation program.
Matlab_Simulink_daodan_3dof
- 提出了基于MATLAB/Simulink的导弹三通道弹道动力学模型仿真方法。分析了运动受力情况,给出导弹空间六自由度运动动力 学模型,对在某初始条件下的三通道弹道进行了仿真和分析,结果很好地反映了弹道特点,证明该仿真方法有效可行。-Based on MATLAB/Simulink ballistic missile dynamic model of three-channel simulation method. Analysis of the movement by force, is g
Matlab_3dof_animation
- 采用比例导引法,把三维追击轨道分解到两个二维平面上分别导引,并充分考虑到目标的 机动性对弹道的影响,用MATLAB软件编写程序模拟出导弹实际追击的三维变轨弹道,绘制出分运动和合运动中各参数的 变化曲线。最后比较了不同的追击速度和不同的导引系数k对弹道特性的影响,考虑到导弹实际飞行时受需用法向过载的 制约,导出了导引系数k应满足的普遍公式,提出了对实战具有一定参考价值的建议。 -Using proportional navigation law, in pursuit of the
ballastic_missile_free_flying_simulation
- 利用OpenGL三维图形实时交互技术,在VC++中编程,实现了不同输入条件下的导弹自由段飞行弹道与飞行姿态仿真,包括导弹建模、以及由云彩绘制和流动效果组成的云彩的建模。-Use OpenGL real-time interactive three-dimensional graphics technology, VC++ In programming, to achieve a different input under the conditions of the free flights of
quaternion_in_missile_flight_simulation
- 论述了四元数法在垂直发射战术导弹和火箭子导弹的仿真中的应用.对反坦克导弹和舰空导弹飞行弹道仿真中的具体应用进行了方程推导、计算分析。 -Discusses the quaternion method in the vertical launching tactical missile and rocket missile sub-simulation. The anti-tank missiles and ship-to-air ballistic missile flight simula
daodandandaoyouhua
- 针对助推- 滑翔导弹的弹道优化问题,给出了一种求解其最大射程弹道的分段优化方法,建立了其 纵平面运动模型和弹道优化模型。在考虑攻角绝对值、攻角变化率、法向过载、分离点攻角衔接及落地条件等约束 下,应用序列二次规划法求解了其最大射程弹道。分析表明,助推- 滑翔导弹比传统弹道导弹射程显著提高,其最 优弹道的起伏有助于增大射程和提高突防能力-For booster- Optimize glider ballistic missile problem, give a maximum rang
daodan
- 比例导引理想弹道仿真Matlab代码，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。-Ideal proportional navigation trajectory simulation Matlab code, the law gives the proportional navigation differential equations using Matla
Proportional navigation method
- 用比例导引法进行拦截弹针对机动目标的弹道仿真，仿真是基于三维模型。-Proportional navigation method used to intercept ballistic missile targets for motor simulation, simulation is based on three-dimensional model.
Basedon Matlab Simulink simulation
- Based on Matlab / Simulink simulation of ballistic missile three-channel-Based on Matlab/Simulink simulation of ballistic missile three-channel
missile
- 基于Matlab/Simulin对导弹的弹道进行了仿真计算-Based on Matlab/Simulin ballistic missile was simulated
ballistic-missile-simulation
- 导弹的弹道分析程序，实现导弹弹道仿真，分析数据-Ballistic missile analysis procedures to achieve the missile trajectory simulation, analysis of data
Ballistic-missile-ballistics
- 弹道导弹弹道学，PDG格式。偶尔在一国防科技网看到的。相当不错。-Ballistic missile ballistics, PDG format. Occasionally, a National Defense Science and Technology Network to see. Quite good.
nse
- 战术攻防对抗弹道仿真Simulation of Tactical Ballistic Missile Defense-Simulation of Tactical Ballistic Missile Defense
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