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tulun
- 理论力学经典问题数值模拟课件,平底凸轮的动画演示。显示了不同动点的选择,相对运动轨迹的形式。-Numerical simulation of the classic problems of theoretical mechanics courseware, flat cam animation. Shows the different choices of fixed points, the relative trajectory of the form.
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.
vibrating-rotator-experiment
- 用于高校学生 转子振动台轴跳动轨迹分析仿真实验。采用正交的具有相位差的两列正弦波来模拟传感器测到的X方向和Y方向的轴跳动。包括信号的时频分析,滤波处理,叠加还原和边界检验。参数可自定-For college students beat the rotor shaft vibration table trajectory analysis simulation. With orthogonal phase difference of two sine waves to simulate the s
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
GPS-satellite-track
- 以GPS卫星为例,主要介绍利用SDP8模型,预报GPS卫星在几天内的星历,从而利用BorlandC++Builder 编程实现GPS卫星星座、星下点轨迹仿真及全球DOP值图形分析,测站星空图变化,测站DOP值分析,从而更好的分析GPS卫星星座、轨道变化、卫星的性能, 为改进卫星的星座及轨道提供技术依据。-This paper introduces that is using SDP8 propagation model to predict GPS of position and velocit
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
MAPXtest
- MAPX地图放大,缩小,平移,手动测试距离,汽车在道路上行驶方向,轨迹显示等MAPX相关代码-MAPX related code MAPX map zoom in, zoom out, pan, the manual test distance, the car in the direction of travel on the road, track display
nonlinear
- 非线性动力学、分岔 Matlab 程序实现,弹簧质量系统在简谐激励作用下的受迫振动,弹簧的恢复力F与变形x的关系为F=kx3,动力学方程为...30cosmxcxkxFwt++= 其中,给定参数,1m=,0.3c=,1.0k=,1w=,初始条件为(0)3.0x=,.(0)4.0x=设系统的动态参数为F0,绘出系统状态变量随参数变化分岔图,绘图参数对应的系统各周期及混沌状态的时间历程图、相轨迹图、Poincare映射图-Nonlinear dynamics, bifurcation Matlab
navigation-yan
- 严老师编写的惯性/GPS组合导航相关程序,包括轨迹生成、滤波、解算等-Inertial/GPS navigation strict teacher written procedures, including trajectory generation, filtering solver
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!
Missile-Fly
- 导弹飞行轨迹的数值模拟程序(已知初始位置及状态),考虑了科氏力和地球自转的影响,比较实用。-Numerical simulation of the missile trajectory program (known initial position and status), taking into account the Coriolis force and the Earth s rotation, more practical.
Asynchronous_motor_subdivision
- 传统异步电机直接转矩控制多采用六边形磁链控制或六区间的圆形磁链控制,容易造 成转矩和磁链脉动过大,限制了其实用范围。针对此缺陷,本文采用矢量细分的方法,将传统的六电压矢量和六扇区细分为十二电压矢量和十二个扇区,制定了相应的矢量开关表,并通过 MATLAB 对其进行了仿真实验。仿真结果表明,基于矢量细分的异步电机直接转矩控制能够有效改善磁链轨迹,减小转矩脉动,提高系统控制性能。 -Conventional induction motor direct torque control multip
Satellite_orbit_design
- 现需要在高度为600~700KM范围内,回归周期为30天的太阳同步轨道上布置一颗L波段的合成孔径雷达卫星。 1. 请设计合适的轨道参数,并仿真对应轨道下一个运行周期内星下点轨迹图(纬度和经度两个图); 2. 计算多普勒中心频率,多普勒调频率与纬度的关系图(设姿态角为0°,天线视角20°~60°,推荐35°); 3. 按高斯投影方式,将星下点轨迹图投影到地图坐标上。-Now requires a height of 600 ~ 700KM range, return period
still
- 地球不转时的星下点轨迹,回归周期1天,可自行设定-Earth does not rotate when the nadir track one day return period
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