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MissileTest
- 用户可以使用键盘对飞机进行控制，如导弹的俯仰，偏航，加速等操作，观看的导弹变化飞行目标，爆炸，弹片飞散等尽可能阵势的描述-Users can use the keyboard to control the aircraft, such as the missile' s pitch, yaw and speed up operations, etc. to watch the flight of the changes in the target missile, explosion, s
Garden_v101
- 飞行游戏，z\x\c控制发射导弹，Source_v101文件夹包含源代码-Flying Games, z \ x \ c control the missile, Source_v101 folder contains the source code
rtems
- RTEMS的全称是"实时导弹控制执行体"。现在RTEMS的全称是 "多处理器实时操作系统",是一个纯粹的32位系统（由于充分利用了32位的特性，所以无法像uCOSII那样用于低端的8位系统）。-RTEMS stands for " real-time control of the implementation of the missile body." Now RTEMS stands for " multi-processor real-time operating
Integgn
- 基于测发一体化技术的导弹发射控制系统设计Integration technology based on measurements made missile launch control system design-Integration technology based on measurements made missile launch control system design
Crme
- 飞航自动驾驶仪系统控制方案研究Cruise Missile Autopilot System Control Scheme-Cruise Missile Autopilot System Control Scheme
4002519Matlab_Simulink_daodan_3dof
- Missile degine and control from an input image
Image-stabilization
- 关于低空高射武器观瞄系统的图像稳定技术的处理及算法。-Low altitude high shooting weapon is an integr al par t of the modern aerial defense system. Cooperating w ith missile and high shoot ing aerial defense system, it can buildup effect ive low altitude def
zhanluedaodan
- 主要接受战略导弹的测试发射控制方法的发展和相关模拟器在测试发射控制总的运用-Mainly by the strategic missile test launch control simulator in the development and testing related to the use of the total emission control
VSCS
- 自己发表的小论文《导弹变结构控制系统设计》附带程序-His essay published in " missile variable structure control system design" with the program
ballistics problem
- 本程序包为vxLand提供的经典版的通用导弹、炮弹、火箭弹等的弹道仿真计算程序，适用于无控弹药，用户可以需要根据加入三点法、比例导引等导引方法，修改、扩充成相应的有控、制导模拟仿真弹道程序。 -This package provides the classic version of vxLand common missile, artillery shells, rockets and other ballistic simulation program for non-control a
Missile1
- Robust Multivariable Control System Synthesis of Longitudinal Axis Autopilot for Missile
IEE-autopilot1
- In this paper, a missile longitudinal autopilot is designed using a new nonlinear control synthesis technique
xy7z.ZIP
- 导弹三维制导控制一体化设计Three dimensional guidance and control for Missile-Three dimensional guidance and control for Missile
d4ef13.ZIP
- 基于扩张状态观测器的导弹纵向控制系统设计Based on the extended state observer design of missile longitudinal control system-Based on the extended state observer design of missile longitudinal control system
btt6dof1good
- 用simulink建立的导弹6自由度模型，同时还有BTT控制，已调试通过，完美运行-Simulink to establish the missile 6-DOF model, as well as BTT Control has been debugging through the perfect run
6dof
- 导弹全弹仿真模型 制导律为比例 控制采用pid-Bomb simulation model of the missile guidance law for proportional control using pid
GMisssileTraje
- 通用弹道仿真计算程序源码V1.0本程序源码包为vxLand提供的经典版的通用导弹、炮弹、火箭弹等的弹道仿真计算程序源码，适用于无控弹药，用户能需要根据加入三点法、比例导引等导引方法，修改、扩充成相应的的有控、制导导模拟仿真弹道程序源码。程序源码包中MissileTrajectorySimulationRk.h的rk()是经典的4阶龙格库塔方法求常微分方程的数值算法的函数子程序源码，大家可参考使用。M -The general trajectory simulation program so
Kkallmanfileea
- 卡尔曼滤波C程序源码 卡尔曼滤波器是一个“optimal recursive data processing algorithm（最优化自回归数据处理算法）”。对于解决非常大部分的问题，他是最优，效率率最高甚甚至是最有用的。他的广泛应用已经超过30年，包含机器人导航，控制，传感器数据融合甚至在军事方面的雷达系统和导弹追踪等等。近年来更被应用于计算机图像处理，例如头脸识别，图像分割，图像边缘检测等等。 -C program source code of Kalman filter Kalman
XHZResult
- 在vb软件上模拟导弹飞行过程与轨迹控制-vbsoftware simulated missile flight trajectory control
kongzhidandaoqingjiao
- 导弹结构参数给定，控制导弹弹道倾角的编程方案-The missile structure parameters given control solution for programming of the missile trajectory inclination