Modeling-of-trajectory
代码说明：
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 of the initial value problem solving differential equations.)
文件列表：
再入式飞行器轨道建模与仿真
..........................\atmosphere.m,3553,2013-11-11
..........................\get_drag.m,1427,2013-11-11
..........................\gravity.m,723,2013-11-11
..........................\kinetic_equation.m,1750,2013-11-11
..........................\main_function.asv,2528,2013-11-11
..........................\main_function.m,2547,2013-11-11
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