Abstract
The relation between the relative motion of geostationary orbit and the station keeping elements is proposed; the orbit correction equations for the radial, tangential, and normal impulse thrust as well as the continuous thrust are reviewed; and the common properties of in-plane orbit correction and out-plane orbit correction are analyzed.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
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). Correction Geostationary Orbit. In: Geostationary Satellites Collocation. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-40799-4_6
Download citation
DOI: https://doi.org/10.1007/978-3-642-40799-4_6
Published:
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-40798-7
Online ISBN: 978-3-642-40799-4
eBook Packages: EngineeringEngineering (R0)