Keplerian Orbit

Version 1.0.7 (145 KB) von Peter Szabó
A program for computation an orbit of a satellite by third Kepler law.
4.3
(3)
1K Downloads
Aktualisiert 2 Nov 2019

Lizenz anzeigen

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).

Zitieren als

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

Kompatibilität der MATLAB-Version
Erstellt mit R2019b
Kompatibel mit R2018b und späteren Versionen
Plattform-Kompatibilität
Windows macOS Linux

Community Treasure Hunt

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

Start Hunting!

Version Veröffentlicht Versionshinweise
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