文件名称:Modeling-of-trajectory
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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.
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下载文件列表
再入式飞行器轨道建模与仿真\atmosphere.m
..........................\get_drag.m
..........................\gravity.m
..........................\kinetic_equation.m
..........................\main_function.asv
..........................\main_function.m
再入式飞行器轨道建模与仿真