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3下载:
导弹六自由度仿真模型,并且仿真了导弹攻击一个匀速直线运动的目标的过程-missile six degree-of-freedom simulation model and simulation of a missile attack on a uniform linear motion of the target
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采用c语言实现的几个计算机图形学教程中的问题。分别包括阻尼运动,导弹打飞机,抛物线模拟等-language used in several computer graphics Guide issues. Respectively damping campaign, a missile attack against aircraft, such as parabolic simulation
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导弹发射演示,模拟导弹的飞行轨迹,3D效果-Missile launch demonstration, the missile' s flight path simulation, 3D effects
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STT导弹六自由度仿真,全弹道仿真,侧滑转弯-STT missile 6-DOF simulation
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导弹弹道仿真计算程序,采用四阶龙格库塔法,为研究导弹弹道仿真提供有效计算方法-Missile trajectory simulation program, using fourth-order Runge-Kutta method for the study of the missile trajectory simulation provides an effective method
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一个基于VC++t OpenGL制作的导弹射击行为模拟,导弹建模技术和粒子系统-One based on VC++ t OpenGL simulation produced by firing a missile, missile modeling techniques and particle systems
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导弹轨道仿真源代码,模型可见钱杏芳《导弹飞行学》第二章的建模,采用四阶龙哥库塔仿真-Missile trajectory simulation source code, the model can be seen Qian Xing-fang, " Missile Flight Science," Chapter II of the modeling, simulation of a four-order Longge Kuta
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一个导弹拦截仿真程序,大家可以看一下!谢谢!-A missile to intercept the simulation program, we can look at! Thank you!
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导弹轨道的模拟程序,舰船的导弹打中目标的过程-Missile orbit simulation program, the missile hit the target ship s course
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对导弹弹道的仿真程序,简单实用。谢谢! 谢谢!-The missile trajectory simulation program, simple and practical. Thanks! Thanks! Thanks!
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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.
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基于LabVIEW的空地导弹弹道仿真系统设计-LabVIEW-based simulation of the open space system design ballistic missile
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带喷射效果的游戏导弹弹道模拟。
按住鼠标不松还能蓄力。
Flash8以上版本都可以通过编译。-Effect of the game with a jet missile trajectory simulation. Hold down the mouse can not loose Charge. Flash8 the above versions can be compiled.
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一个简单的用OpenGL和MFC单文档实现模拟导弹撞击的场景-OpenGL Missile Hit Object Simulation
The program shows a procedure of a missle hitting on the wall!
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:为了提高最小二乘支持向量回归机的性能,将Morlet小波核函数引入其中,形成了最小二乘小波支
持向量回归机模型。利用待优化的参数重构模型的目标函数和约束条件,并在此基础上通过遗传算法进行参数
选择,从而提高了该模型的泛化能力。将最小二乘小波支持向量回归机应用于导弹陀螺仪的漂移趋势预测,仿真
实验结果表明了该方法的有效性和可行性,因此可以为陀螺仪的故障预报、可靠性辅助决策提供依据。-To improve the ability of least square support vect
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模拟飞机飞行状态的小游戏。可以从4个视角看效果。(说明:我之前的导弹功能描述有误,导致和 重复,抱歉)-Aircraft flight simulation game. View from the four results. (Note: I am a missile before the functional descr iption is inaccurate, leading to and repeat, sorry)
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对基于弹载IMU/C:PS组合导航系统的动基座对准问题进行了研究与仿真 首先,分析了弹载IMU与GI S的系统误差,建立获得了其系统误差模型 然后,利用卡尔曼滤波技术,设计了弹载IMU/UPS组合导航系统的动基座对准算法 -Based on onboard IMU/C: PS Integrated Navigation System Alignment conducted a study and simulation first analyzed onboard IMU and GI S of
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对基于弹载IMU/C:PS组合导航系统的动基座对准问题进行了研究与仿真 首先,分析了弹载IMU与GI S的系统误差,建立获得了其系统误差模型 然后,利用卡尔曼滤波技术,设计了弹载IMU/UPS组合导航系统的动基座对准算法 -Based on onboard IMU/C: PS Integrated Navigation System Alignment conducted a study and simulation first analyzed onboard IMU and GI S of
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对基于弹载IMU/C:PS组合导航系统的动基座对准问题进行了研究与仿真 首先,分析了弹载IMU与GI S的系统误差,建立获得了其系统误差模型 然后,利用卡尔曼滤波技术,设计了弹载IMU/UPS组合导航系统的动基座对准算法 -Based on onboard IMU/C: PS Integrated Navigation System Alignment conducted a study and simulation first analyzed onboard IMU and GI S of
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采用平行接近法对导弹飞行制导过程进行弹道模拟-Parallel close to the method of ballistic missile flight guidance process simulation
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