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Modeling-of-trajectory
- Matlab进行再入式飞行器轨道建模与仿真,建立各种模型,最后获得飞行器的动力学模型,并调用龙格库塔函数求解该微分方程初值问题。-Matlab for reentry spacecraft orbit modeling and simulation, the establishment of various models, and finally obtain the dynamic model of the aircraft, and call the Runge-Kutta function