Abstract
The characteristics of the perturbation period of geostationary satellite are analyzed. The spectral decomposing algorithm is established to identify periodical motions from high-precise oscillation ephemeris, and an identification algorithm of periodical motions based on singular value decomposition is presented.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Kozai Y (1959) The effect of the Earth’s oblateness on the orbit of a near satellite. J Astron 64:378–397
Kozai Y (1962) Second order solution of artificial satellite theory without drag. J Astron 67:446–461
Blitzer L (1962) Circular orbit in an axially symmetric gravitational field. J ARS 32:1102
Cook GE (1966) Perturbation of near-circular orbits by the Earth’s gravitational potential. Planet Space Sci 14:433
Cook GE (1963) Perturbations of satellite orbits by tesseral harmonics in the Earth’s gravitational potential. Planet Space Sci 11:797
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
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). Harmonic Analysis Geostationary Orbit. In: Geostationary Satellites Collocation. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-40799-4_5
Download citation
DOI: https://doi.org/10.1007/978-3-642-40799-4_5
Published:
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-40798-7
Online ISBN: 978-3-642-40799-4
eBook Packages: EngineeringEngineering (R0)