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Description: rocket 演示了控制图片移动的方法，控制火箭的移动 -rocket demonstration of the control methods Photo Mobile, the mobile rocket control
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Size: 9526 |
Author: 黄均强 |
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Description: 用C语言编写一个腾飞的火箭程序-C language of a rocket takeoff procedures
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Size: 1024 |
Author: 边奎星 |
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Description: rocket 演示了控制图片移动的方法，控制火箭的移动 -rocket demonstration of the control methods Photo Mobile, the mobile rocket control
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Size: 9216 |
Author: 黄均强 |
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Description: 一个mpeg测试文件！！！！！
值得一看！！！！！！！！
非常小-a test paper! ! ! ! ! An eye-catcher! ! ! ! ! ! ! ! Very small! !
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Size: 95232 |
Author: goodluck |
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Description: 导弹控制系统的鲁棒控制设计实例，包括3中不同的方法，有详细的注解和最后simulink 仿真。-Missile control system design example of robust control, including 3 in different ways, have detailed comment and final simulink simulation.
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Size: 37888 |
Author: jesse |
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Description: matlab关于鲁棒控制的例子，设计一个Rocket，有源代码，和设计过程详解。是入门的好资料-matlab on the examples of robust control, the design of a Rocket, active code, and explain the design process. Is a good data entry
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Size: 849920 |
Author: 王维 |
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Description: 模拟火箭发射的c语言源程序，火箭发射动画-Simulated rocket c language source code, rocket launchers Animation
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Size: 1024 |
Author: apple |
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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: 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.
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Size: 207872 |
Author: 木木 |
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Description: Rocket Simulation Module in JAVA
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Size: 2048 |
Author: Khan |
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Description: AVR Project for rocket development with C source and circuit
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Size: 1591296 |
Author: Dori_leroi |
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Description: 一个可爱的火箭上天
超赞
一个C实例-rocket c on the sky
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Size: 1024 |
Author: 冷甜心 |
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Description: 导弹弹道计算程序 ，用到的参数文件，包括速度，质量，转动惯量，火箭推力。-Ballistic Missile program, the parameters used in documents, including the speed, quality, moment of inertia, rocket thrust.
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Size: 7168 |
Author: 水木林 |
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Description: 倒立摆系统是研究控制理论的实验平台，它的行为与火箭飞行以及两足机器人行走有很大相似性，因而对其研究具有重大的理论和实践意义，一直是控制界关注的焦点。以直线单级倒立摆作为研究对象，采用最优控制策略实现对其平衡控制，进行仿真实验设计。-Inverted pendulum control theory is to study the experimental platform, its behavior and the rocket s flight and walking biped robot is very similar, and thus their study is of great theoretical and practical significance, has been the focus of attention control. Inverted Pendulum on a straight line as the object of study, the optimal control strategy to achieve their balance control, a simulation design
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Size: 1024 |
Author: 林 |
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Description: 一个设计火箭和火箭仿真模拟的Java软件源码-a rocket degin and simulation java software source
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Size: 3824640 |
Author: 李博 |
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Description: 一个六自由度火箭的鲁棒控制程序，该程序鲁棒H infinity control, robust loop shaping control 和mu analysis control三种不同的控制算法，并与火箭的非线性模型仿真结果进行了对比。-A six DOF robust control rocket program that robust H infinity control, robust loop shaping control and mu analysis control of three different control algorithms, and nonlinear model rocket simulation results were compared.
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Size: 37888 |
Author: 小方 |
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Description: 火箭模型，可观转换视角，也可选择观看模式-Rocket model, substantial transformation perspective, can also choose to view mode
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Size: 15360 |
Author: Xinyue wang |
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Description: 大概模拟火箭升空的后面飞行时发出的火焰的样子。-Probably off the back of the simulated rocket flight given the way the flame.
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Size: 31744 |
Author: 江川 |
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Description: 一个火箭轨道控制程序，利用模态综合法降阶后，对火箭发射过程的振动模态进行观测和控制-A rocket orbit control procedures, the use of reduced-order modal synthesis method, the process of rocket vibration mode for observation and control
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Size: 8192 |
Author: liupan |
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Description: wordpress提高访问速度火箭加速，飞一般速度(WordPress increases access speed, rocket acceleration, flying speed)
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Size: 1147904 |
Author: minerli |
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