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   源码介绍

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Ground track and 3D orbit simulation of LEO satellite.

Ground track and 3D orbit simulation of LEO satellite.
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### Use:
1. Run setup.m.
2. Open initSimulationParams.m.
    1. Input initial Keplerian elements.
    2. Input simulation time in days and step time in seconds.
3. Run mainKeplerGroundTrack.m or mainNewtonGroundTrack.m.

.
├── Ground track and 3D orbit simulation of LEO satellite..zip
└── Satellite-Orbit-master
    ├── README.md
    ├── initSimulationParams.m
    ├── mainKeplerGroundTrack.m
    ├── orbit
    │   ├── getWw.m
    │   ├── keplerianDynamics.m
    │   └── physicalParams.m
    ├── plots
    │   ├── earth.jpg
    │   ├── plotEarth.m
    │   └── plotSatelliteOrbit.m
    ├── setup.m
    ├── utils
    │   ├── RK4.m
    │   ├── dcm313Euler.m
    │   ├── dcm321Euler.m
    │   ├── transformCartesian2Spherical.m
    │   ├── transformECEF2ECI.m
    │   ├── transformECI2ECEF.m
    │   └── transformKeplerians2ECI.m
    └── validations
        ├── fig.1.png
        ├── fig.2.png
        ├── fig.3.png
        ├── fig.4.png
        └── init_conditions.png

5 directories, 23 files