Description: 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 Platform: |
Size: 22528 |
Author:向礼 |
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Description: 无控纵向导弹弹道计算。用四阶龙库、阿当姆斯积分法，运行时间短，效果好。-no control ballistic missile vertical calculation. With the four-Long, Adam Shams integral method, a short running time, the effect is good. Platform: |
Size: 2048 |
Author:杨 |
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Description: 采用Matlab编写的弹道分析算法，该算法可以模拟弹道飞行轨迹-Matlab preparation of the trajectory analysis algorithm, which can be simulated ballistic trajectory Platform: |
Size: 21504 |
Author:杨向华 |
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Description: 导弹载入弹道的优化设计，主要是机动段的优化-ballistic missile printed in the optimization of the design, mainly the optimization of the mobile Platform: |
Size: 228352 |
Author:何瑾 |
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Description: 一篇用弹道系数识别弹道导弹目标的博士论文！这是非常难得的文章！-With a ballistic coefficient of a ballistic missile target recognition doctoral thesis! This is a very rare article! Platform: |
Size: 1514496 |
Author:LIU weijian |
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Description: 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 given a missile in space dynamic model of six degrees of freedom movement, the initial conditions in a three-channel under the ballistic simulation and analysis, the results well reflect the ballistic characteristics of the simulation method proved effective feasible. Platform: |
Size: 140288 |
Author:李恒 |
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Description: 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 ballistic missile flight attitude and simulation, including missile modeling, as well as the effect of clouds and mobile mapping the composition of clouds Modeling. Platform: |
Size: 263168 |
Author:李恒 |
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Description: 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 simulation application specific equation, calculated and analyzed. Platform: |
Size: 207872 |
Author:木木 |
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Description: 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 range of its ballistic solution of the sub-optimization method, set up the vertical plane motion model and optimization model of trajectory. In considering the absolute angle of attack, the rate of change of angle of attack, normal load, the separation point of convergence and the arrival angle of attack constraint conditions, the application of sequential quadratic programming method to solve a maximum range of its ballistic. Analysis showed that propelled- gliding range ballistic missile than the traditional significantly improve, the optimal trajectory of the ups and downs will help increase the range and ability to enhance penetration Platform: |
Size: 381952 |
Author:王敏 |
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