Abstract
Satellites are attracted not only by the central force of the earth, but also by the non-central force, the attraction forces of the sun and the moon, and the drag force of the atmosphere. They are also affected by solar radiation pressure, earth and ocean tides, general relativity effects (cf. Chap. 5), and coordinate perturbations. Equations of satellite motion must be represented by perturbed equations. In this chapter, after discussions of the perturbed equations of motion and the attraction forces, for convenience of the earth tide and ocean loading tide computations, the ephemerides of the sun and the moon are described. Orbit correction is discussed based on an analysis solution of the \( \overline{C}_{20} \) perturbation. Emphasis is given to the precise orbit determination, which includes the principle of orbit determination , algebraic solution of the variation equation, numerical integration, and interpolation algorithms, as well as the related partial derivatives .
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Xu, G., Xu, Y. (2016). Perturbed Orbit and Its Determination. In: GPS. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-662-50367-6_11
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DOI: https://doi.org/10.1007/978-3-662-50367-6_11
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