Abstract
The principles, strategies, and algorithms of the station keeping of geostationary satellite are discussed. For north/south station keeping, the design of inclination confined ring and the calculation of inclination control target for single satellite and collocated satellites are discussed. The relation between control moment and local satellite time is also discussed and a specific case simulation of the control process is given. For east/west station keeping, the complicated situation of coupling control of the drift rate and eccentricity is analyzed, including the distribution strategy and the pulse execution algorithm of single pulse, bi-pulses, and tri-pulses.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Kamel A, Ekman D, Tibbitts R (1973) East-west station keeping requirements of nearly synchronous satellites due to Earth’s Tri-axiality and Luni-Lunar Effects. Celest Mech 8:129–148
Kamel A, Wagner C (1982) On the orbital eccentricity control of synchronous satellites. J Astronaut Sci 3(1):61–73
Chao CC, Baker JM (1983) On the propagation and control of geosynchronous satellites. J Astronaut Sci 4(1):99–115
Liu L (1992.8) Orbital dynamics for earth satellite. High Education Press, Beijing [In Chinese]
Li JS (1995.8) The precision orbit determination for earth satellite. PLA Press, Beijing [In Chinese]
Soop EM (1994.10) Handbook of geostationary orbits. Kluwer Academic Publishers, Dordrecht
Soop EM (1987) Coordinated station keeping at longitude 19 degrees west. OAD paper No.342, 1987
Montenbruck O (1989) Practical ephemeris calculations. Springer, Berlin
Li HN (2010.10) Geostationary satellite orbital analysis and collocation strategies. National Defense Industry Press, Beijing [In Chinese]
Author information
Authors and Affiliations
Rights and permissions
Copyright information
© 2014 National Defense Industry Press, Beijing and Springer-Verlag Berlin Heidelberg
About this chapter
Cite this chapter
Li, H. (2014). Maintaining Geostationary Orbit. In: Geostationary Satellites Collocation. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-40799-4_7
Download citation
DOI: https://doi.org/10.1007/978-3-642-40799-4_7
Published:
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-40798-7
Online ISBN: 978-3-642-40799-4
eBook Packages: EngineeringEngineering (R0)