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: 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: 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: 根据导弹仿真数据，绘制可直观显示弹道特性的理想弹道曲线。给出了比例导引法的差分方程，建立了
比例导引法的三维弹道仿真模型。在对比例导引法进行三维弹道仿真的基础上，分别对增量比例导引、基于二次
型的最优制导律和考虑动态特性的二次型最优制导律进行了三维弹道仿真，绘制出了可直观显示弹道特性的理想
弹道，计算了导弹与目标的遭遇时间，并对结果进行了比较分析。最后得出考虑弹体动态特性的二次型最优制导
律具有最优性。-According to the missile simulation data, mapping can be visual display characteristics of an ideal ballistic ballistic curve. Proportional navigation law gives the differential equation, proportional navigation law established a three-dimensional trajectory simulation model. Proportional navigation in the three-dimensional trajectory simulation method, based on the respective proportion of the incremental guidance, based on quadratic optimal guidance law and consider the dynamic characteristics of quadratic optimal guidance law for a three-dimensional trajectory simulation, rendering a visual display may be the ideal ballistic trajectory characteristics, calculated the missile with the target Platform: |
Size: 189440 |
Author:特步 |
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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: 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 three-dimensional orbit decomposition to two two-dimensional plane, respectively, guidance, and taking fully into account the objectives of the impact of mobility on the trajectory, using MATLAB software programming practical pursuit of missile simulated three-dimensional orbit trajectory , to map out points Movement Hop movement curve of each parameter. Finally, the pursuit of different speed and different-guided ballistic coefficient k on the characteristics of, taking into account the actual missile flight by the need to overload the use of constraints derived Seeker coefficient k should satisfy the general formula, put forward on the actual reference value has a certain proposal. Platform: |
Size: 295936 |
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: 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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Description: 弹道导弹SINS/CNS组合导航的程序，在发射点惯性坐标系下-Ballistic Missile SINS/CNS Integrated Navigation of the program, the launch point inertial coordinate system Platform: |
Size: 5120 |
Author:Adolph |
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Description: nanoMOS is a 2-D simulator for thin body (less than 5 nm), fully depleted, double-gated n-MOSFETs. A choice of three transport models is currently available (drift-diffusion, classical ballistic, and quantum ballistic). The transport models treat quantum effects in the confinement direction exactly and the names indicate the technique used to account for carrier transport along the channel. Each of these transport models is solved self-consistently with Poisson’s equation. Several internal quantities such as subband profiles, subband areal electron densities, potential profiles and I-V information can be obtained from the source code.
Platform: |
Size: 5998592 |
Author:mohammad |
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