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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.
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
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.
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
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