Description: Two body problem solving program
There are two files:
1.orbit_ Solver. M initialization program, numerical calculation and drawing output.
Set the initial position coordinate R0 and speed V0 of the satellite, set the start and end time t0 and TF of the simulation, and then it can run directly.
2.dif_ orbit_ Dynamic. M orbit dynamics function, including the unperturbed dynamics and the dynamics equation under J2 perturbation, which dynamics should be set in this program.
To Search:
File list (Check if you may need any files):
| Filename | Size | Date |
|---|
| TwoBody\ReadMe.txt | 297 | 2020-05-25
|
| TwoBody\dif_orbit_dynamic.m | 561 | 2020-05-25
|
| TwoBody\orbit_solver.m | 1620 | 2020-05-25
|
| TwoBody | 0 | 2020-05-25 |
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