Abstract
A program, METUGEO, is developed to predict the orbital parameters of a geostationary satellite. The program is verified by comparing its predictions to a similar program used at the TÜRKSAT ground control station. The program is employed to test and compare long term inclination (north) maneuver strategies for TÜRKSAT series satellites. Two strategies are investigated. The first one being the actual strategy used at the TÜRKSAT ground control station, and the second one is the long-term strategy proposed by Soop. One year long experiment, using the two strategies mentioned, is conducted. It is found that the strategy proposed by Soop results in less fuel consumption, than the actual control strategy used at the TÜRKSAT ground control stations. Consequently, it is shown that the operational life of the spacecraft may be extended by proper maneuvering strategies.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
Garner. J.T.: Satellite Control. A Comprehensive Approach, John Wiley and Sons, England, 1996.
Erdal. T.: Investigation of Minimum Fuel Maneuvers for TÜRKSAT Satellites with Possible Use of Its Simulator, M.S. Thesis in Aeronautical Engineering, Middle East Technical University Libraries, Ankara, Turkey, November 1998.
Soop. E.M.: Handbook of Geostationary Orbits, Kluwer Academic Publishers, Dordrecht, 1994.
Sakaci C: Two Simulation Models: Low Altitude Flows and the TÜRKSAT Satellite Orbit, M.S. Thesis in Aeronautical Engineering, Middle East Technical University Libraries, Ankara, Turkey, January, 1996.
TÜRKSAT Engineering Training Documents, Vol. 3 , Aerospatiale Espace & Defence, 1993.
Uslu Ö.: Orbit Dynamics, Attitude Dynamics and Control: Investigation into Possible Applications to TÜRKSAT, M.S. Thesis in Aeronautical Engineering, Middle East Technical University Libraries, Ankara. January, 1997.
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2000 Springer Science+Business Media Dordrecht
About this chapter
Cite this chapter
Erdal, T., Tekinalp, O., Tulunay, Y. (2000). Minimum Fuel Station Keeping Maneuver Strategy for TÜRKSAT Geostationary Satellites. In: Miau, JJ., Holdaway, R. (eds) Reducing the Cost of Spacecraft Ground Systems and Operations. Space Technology Proceedings, vol 3. Springer, Dordrecht. https://doi.org/10.1007/978-94-015-9395-3_5
Download citation
DOI: https://doi.org/10.1007/978-94-015-9395-3_5
Publisher Name: Springer, Dordrecht
Print ISBN: 978-90-481-5400-5
Online ISBN: 978-94-015-9395-3
eBook Packages: Springer Book Archive