Keplerian Orbit

A program for computation an orbit of a satellite by third Kepler law.
1K descargas
Actualizado 2 Nov 2019

Ver licencia

This contribution contains an algorithm to calculate the orbit of a satellite according to the third law of Kepler and Newton's law of gravitation.
The program loads input data from a file of type two-line elements (TLE).
An input TLE file: https://www.dropbox.com/s/lezxmsxnn6vai5n/TLE_skCUBE.txt?dl=0

TLE file type, information about satellite skCUBE is described in the following article:
Szabó, P., Gombíková, K., Ferencová, M. and Košuda, M.:"Keplerian Orbit and Satellite skCUBE",
2019 New Trends in Aviation Development (NTAD), pp. 174-179, IEEE,
https://ieeexplore.ieee.org/document/8875530

This program is a part of a diploma thesis. Author and title of thesis:
Katarína Gombíková: MATLAB for flight engineers (2020).

Citar como

Peter Szabó and Katarína Gombíková (2019). Keplerian Orbit (https://www.mathworks.com/matlabcentral/fileexchange/72098), MATLAB Central File Exchange. Retrieved July 11, 2019.

Compatibilidad con la versión de MATLAB
Se creó con R2019b
Compatible con cualquier versión desde R2018b
Compatibilidad con las plataformas
Windows macOS Linux

Community Treasure Hunt

Find the treasures in MATLAB Central and discover how the community can help you!

Start Hunting!
Versión Publicado Notas de la versión
1.0.7

minor output fixes

1.0.6

minor text fixes

1.0.5

Adding a reference to the program.

1.0.4

1.0.4
- O = Omega (program note, MATLAB variables)

1.0.3

1.0.3
- software description update

1.0.2

1.0.2
- description update

1.0.1

1.0.1
- Adding a link to an input file
- Diploma thesis information

1.0.0