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一个基于opengl非常逼真的导弹模拟程序,值得参考
Update : 2008-10-13 Size : 364.34kb Publisher : cxl

一个基于opengl非常逼真的导弹模拟程序,值得参考
Update : 2025-02-19 Size : 364kb Publisher : cxl

6 DOF Missle Simulation
Update : 2025-02-19 Size : 2.14mb Publisher : alley_007

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!
Update : 2025-02-19 Size : 3.14mb Publisher : 王卫

this will help u in the simulation of missle functions
Update : 2025-02-19 Size : 186kb Publisher : abhi

介绍导弹制导方面的书籍,一本经典的直到方面的外文书籍,希望能对相关专业人士有所帮助-Introduction about missile guidance and control sysytem,you can study missle zhidao system from it ,Most air defense systems in use or under development today, employ homing guidance to effect intercept of the target. By virtue of the use of onboard data gathering, the homing guidance system provides continually improving quality of target information right up to the intercept point. More than any single device, the guided missile has shaped the aerospace forces of the world today. Combat aircraft, for example, are fitted with airborne weapons that can be launched against enemy aircraft, ground forces, or strategic targets deep inside enemy territory. Also, the guided missile can be employed as a diversionary weapon to confuse ground and air forces. Ground-based missile systems have various range capabilities from a few miles to several thousand miles. These ground-based missiles are ballistic or nonballistic types, depending on their mission requirements. The design of a gu
Update : 2025-02-19 Size : 2.9mb Publisher : liuhazi

导弹模块主调接口程序,该模块将动力学结构学环境等参数汇总后交给主程序-Missile melody interface program module, the module structure, learning environment will be dynamic parameters such as aggregate turned over to the main program
Update : 2025-02-19 Size : 2kb Publisher : hailan

基于 OPENGL 开发的导弹碰撞测试程序,对入门OPENGL编程有帮助-OPENGL missile developed based on crash test procedures, entry-OPENGL programming help
Update : 2025-02-19 Size : 218kb Publisher : fbin

java tank war jsp, including missle, tank body
Update : 2025-02-19 Size : 10kb Publisher : xiaoye

导弹仿真程序,拉格朗日插值,四阶龙格库塔-missle
Update : 2025-02-19 Size : 1kb Publisher : 古越涛

DL : 0
一个用于计算最长递增子列的代码,值得玩味。-A code used to calculate the longest increasing subsequence, worth pondering.
Update : 2025-02-19 Size : 5kb Publisher : 王程序

导弹控制系统鲁棒设计程序源代码,可以用来参考编程,比较实用-missile control system design
Update : 2025-02-19 Size : 39kb Publisher : zz

机载导弹捷联惯性导航系统,空中动基座传递对准技术研究,研究弹载子系统与机载主惯性导航系统在飞行过程中的动态传递对准技术-Airborne missile strapdown inertial navigation systems, air Moving Base Transfer the main alignment technology, research onboard subsystems and airborne inertial navigation system during the flight dynamic Transfer Alignment
Update : 2025-02-19 Size : 1.52mb Publisher :

DL : 0
grid on the surface of the missle,use the fortran code .with the most imortant orchard and structure 2D grid
Update : 2025-02-19 Size : 3kb Publisher : 王得强

missle acceleration dynamics codes.
Update : 2025-02-19 Size : 1kb Publisher : pouya

DL : 3
课程设计时完成的。 包涵导弹六自由度建模,目标运动建模,制导系统建模,控制建模,命中条件建模和最后将他们和为一体的整个系统建模。 还有学院教授编写的制导手册,里面有讲解和实例。 还有导弹气动参数的文本。 由matlab编写,模型由simulink建立。-Upon completion of the course design. Bear with six degrees of freedom missile modeling, object motion modeling, guidance system modeling, control modeling, modeling, and finally hit their conditions and for the integration of the entire system modeling. Matlab prepared by the model established by the simulink.
Update : 2025-02-19 Size : 4.22mb Publisher : 马一鸣

文件为基于MATLAB的惯性导航仿真,文件内有导弹飞行模拟参数,根据参数绘出导弹的飞行轨迹-It s a work about inertial simulation based on Matlab, the file includes the flying parameters, we can draw the orbits of the missle
Update : 2025-02-19 Size : 541kb Publisher : 王宁

DL : 1
程序为matlab simulink 编写 实现了多智能体一致性(The programs are written by matlab simulink to realize multi-agent consistency)
Update : 2025-02-19 Size : 20kb Publisher : 图图111

设计图形用户界面,直观的实现更改攻角、各级火箭喷射时间等参数后得到对应参数下的导弹弹道图像以及导弹的飞行时间和飞行距离。适合航天专业的初学者进行仿真测试。(The design of the graphical user interface, the intuitive implementation of the change attack Angle, the various levels of rocket injection time and other parameters to the corresponding parameters of the missile trajectory image and the missile's flight time and flight distance.Suitable for aerospace professional beginners to conduct the simulation test.)
Update : 2025-02-19 Size : 47kb Publisher : 水浮莲
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