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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
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Size: 189440 |
Author: 特步 |
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Description: 运载火箭性能计算一体化优化设计系统在运载火箭方案论证设计阶段中有着重要的应用价值。本
文在面向对象方法学的指导下，建立了运载火箭性能计算一体化优化设计软件系统的对象模型、动态模型以及功
能模型，划分了系统的组成模块，利用$42,/& <3,=4 >?) 和@0045A!))) 开发实现了该软件系统。对象技术的应用使得
系统具有良好的通用性。该软件系统可以完成不同型号运载火箭和不同优化设计性能要求的仿真优化计算，软件
具有较好的稳定性、可重用性和可维护性。-Launch Vehicle Integrated Optimal Design of performance calculation program demonstration system in the rocket design stage has important application value. In this paper, object-oriented methodology under the guidance of established optimal design of launch vehicle performance computing software system integration, object model, dynamic model and functional model, dividing the system composed of modules, the use of $ 42,/& " 3, = 4 " ?), and @ 0045A!))) to achieve the development of the software system. The application of object technology makes the system has good versatility. The software system can complete the different types of carrier rockets and different optimal design performance requirements of the simulation and optimization calculations, the software has good stability, reusability and maintainability.
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Size: 4201472 |
Author: 江伟 |
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Description: 精品自编程序：导弹-火箭制导控制仿真计算VC++源代码.rar-Missile- Rocket Guidance and Control Simulation v0.8-VC++ source code. Rar
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Size: 1643520 |
Author: 天马 |
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Description: 包括火箭主动段的标准轨道发射器以及主动段的显示制导制导律仿真-Guidance Guidance Law including the display emulation standard orbit rocket launchers active segment and active segment
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Size: 1220608 |
Author: yxylin |
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