搜索资源列表
Kepler_orbit_rotate
- 计算得出导弹的被动段飞行轨迹（未考虑大气）和再入点、落点信息（在发射惯性坐标系内的位置量）-Calculated the passive missile flight path segment (not to consider the atmosphere) and re-entry point, placement of information (in the firing position within the inertial coordinate system volume)
UKF
- GPS定位采用UKF滤波方式。包括调用的数据dat文件（选用卫星数据和机动目标运行轨迹数据）和调用的sigma点生成子程序。运行可观察定位误差（位置、速度和加速度）-GPS positioning using UKF filtering method. The data include call dat file (optional operation of satellite data and maneuvering target trajectory data) and the sigma
bili
- 导弹飞行过程中采用比例导引法，本程序对飞行轨迹就行模拟计算。-Missile flight in the proportional guidance law, the procedures of the flight path on-line simulation.
flying
- 飞行器仿真实验，对飞行器的轨迹进行仿真，求解速度及位置-Vehicle simulation, the simulation of the aircraft' s trajectory, velocity and position to solve
trajectory
- 捷联惯导中的模拟轨迹程序，适用于惯导学习者-SINS trajectory
three-particle-algorithms
- BPF算法（回溯粒子滤波），还包括判断粒子是否有效的子函数，以及其中用到的判断两条直线是否相交的函数（用来判断轨迹是否与墙壁相交）。- three particle filter algorithms(SIR,ASIR and BPF) for indoor pedestrian navigation.Also include a function for particle validation detection and a function to check if two lines i
fullmodel
- 产生以群结构运动的多个目标的模拟运动轨迹 参数可调-group tracking data
bilidaoyin
- 比例导引法 导弹三维仿真，可以用来计算导弹的飞行轨迹-The Proportional Navigation Act missile three-dimensional simulation
CNS
- 天文导航，弹道导弹SINS/CNS组合导航，轨迹发生器，卡尔曼滤波-Celestial navigation, ballistic missile SINS/CNS integrated navigation, trajectory generator, Kalman filtering
car-manage-system
- 车辆监控系统软件，可以实现车辆的监控，轨迹回放等多项功能!-The system is very usefull to creat the manage system of cars！
hybrid_pseudo_L
- 高超声速飞行器上升轨迹优化计算。采用勒让德伪谱法直接优化方法。-trajectory optimization of hypersonic craft program with legendre method
SINS_simulation
- 基于MATLAB的捷联惯导轨迹发生器，以及SINS解算程序-SINS based on MATLAB trajectory generator and solver SINS
NMEA2KML
- 内部包含nmea2kml.exe 主要用于GPSNMEA数据向KML轨迹文件的转换，PUDN有一个相关的文件，但并不包含可执行文件。-Contains an internal nmea2kml.exe Mainly used for transforming GPSNMEA data to KML trace file, PUDN has a relevant document, but does not contain executable file.
guijifashengqi
- 捷联式惯性导航的轨迹发生器，使用matlab语言编写-Strapdown inertial navigation path generator
daodanfeixinglixue
- 通过导弹的空气动力系数计算导弹的之心运动方程组，并利用MATLAB进行绘图，包括轨迹，速度时间曲线等-Aerodynamic coefficients calculated by missile missile equations of motion of the heart, and using MATLAB graphics, including trajectory, velocity-time curve
missileg
- 轨迹发生器，包含助推段，加速段，巡航段，下降段及落地，大机动，高空高速。完全正确。-Trajectory generator, including the boost phase, the acceleration, cruise segment, down section and landing, large motor, high-altitude high speed. Entirely correct.
Desktop
- 机器人轨迹仿真编程和动态变化。同时，也具有良好的仿真效果-Robot trajectories and dynamics simulation programming. It also has a good simulation effect
1247900827CS_Kaman
- 目标跟踪程序实现_对雷达采集的数据进行分析，然后得出目标的飞行轨迹，程序采用了卡尔曼滤波加当前统计模型-Target tracking procedures to achieve _ radar data collected for analysis, and then draw the target flight path, the program uses a Kalman filter plus current statistical model
trace-generator
- 惯导轨迹发生器,生成各种常规运动下的惯性传感器数据-inertial navigation trace generator
MY_MPCController3
- 基于模型预测控制的，运动学的轨迹跟踪控制器设计-Based on model predictive control, the kinematic trajectory tracking controller design