- Category:
- matlab
- Tags:
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[Matlab]
[源码]
- File Size:
- 7kb
- Update:
- 2014-05-29
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- Uploaded by:
- zcx
Description: 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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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
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