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**Flat Earth Theory / Numerical method for satellite orbits**

« **on:**May 06, 2019, 05:39:08 AM »

Below is a link to a dissertation which describes a numerical integration technique used for propagating the orbits of satellites.

Below that is a description of a numerical package along with embedded links for initial conditions for describing orbits and trajectories. The model is displayed for view.

This piece serves as illustration that Newtonian dynamics are not only solvable for explaining and modeling orbits, but also used to position artificial satellites around objects in our solar system.

Let me know if you have any questions as these numerical techniques would prove useful for FET pursuits.

https://www.colorado.edu/ccar/sites/default/files/attached-files/numerical_algorithms_for_preci.pdf

http://www.maia.ub.edu/dsg/wsem/documents/validated01.pdf

Below that is a description of a numerical package along with embedded links for initial conditions for describing orbits and trajectories. The model is displayed for view.

This piece serves as illustration that Newtonian dynamics are not only solvable for explaining and modeling orbits, but also used to position artificial satellites around objects in our solar system.

Let me know if you have any questions as these numerical techniques would prove useful for FET pursuits.

https://www.colorado.edu/ccar/sites/default/files/attached-files/numerical_algorithms_for_preci.pdf

http://www.maia.ub.edu/dsg/wsem/documents/validated01.pdf