搜索资源列表
WSP
- 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
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)
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.
pingxing
- 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
ballistic_missile_inertial_navigation
- 弹道导弹从东经120北纬20高度30公里打目标东经150北纬30高度0的目标，关机点及飞行时间计算。还介绍了惯性导航的内容。 对于弹道式导弹：目标作为地球上的某一点，它是随地球一起在惯性空间运动的，因此需要迭代求解需要速度和自由飞行时间。按照给出的程序进行多次迭代解算即可得出考虑地球自转时的关机点参数解算和飞行时间计算。-20 ballistic missile from a high degree of north latitude and 120 east longitude hit tar
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
bilidaoyin.m
- 设计的比例导引法引导导弹飞行的程序，比较适合航空制导-Design proportional navigation guidance missile program, more suitable for aerospace guidance
kalman
- 导弹飞行轨迹的kalman滤波程序，包括标准kalman滤波和信息滤波程序- U5BFC u983 u983 u8C0 u8F09 u8C0 u7E09 u7E2
MissileSim
- 导弹飞行控制 3自由度动力学仿真 质点运动学仿真(Missile flight control)