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2016 | Supplement | Chapter

Post-Newtonian Orbital Equations for Fermi Frames in the Vicinity the Earth

Authors : J. M. Gambi, M. L. García del Pino, M. M. Tung

Published in: Progress in Industrial Mathematics at ECMI 2014

Publisher: Springer International Publishing

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Abstract

Synge’s equations for time-like geodesics in terms of Fermi coordinates are used to derive post-Newtonian equations for the relative motion of satellites in coplanar circular near orbits about the earth. The reference frame, co-moving with the base satellite, is assumed to be a Fermi frame, that is, inertial guided. The resulting system is autonomous, linear, and reduces to the equation of the geodesic deviation for nearby satellites. Hence, it can be used by some Acquisition, Pointing, and Tracking systems to increase the accuracy presently reached in locating passive radio-transmitters.

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Footnotes
1
For any two events in E, \(P_{1}(x^{k_{1}})\), \(P_{2}(x^{k_{2}})\), for which there is a unique geodesic \(\varGamma _{P_{1}P_{2}}\) joining them with equations x k = ξ k (u) where u is an affine parameter ranging from 0 to 1, the world-function Ω(P 1, P 2) is defined by the line integral
$$\displaystyle{ \varOmega (P_{1},P_{2}) =\varOmega (x^{k_{1}},x^{k_{2}}) = \frac{1} {2}\int _{0}^{1}g_{ ij}U^{i}U^{j}du }$$
taken along \(\varGamma _{P_{1}P_{2}}\) where \(x^{k_{1}} \equiv \xi ^{k}(0)\), \(x^{k_{2}} \equiv \xi ^{k}(1)\) and U k = k du.
 
Literature
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Metadata
Title
Post-Newtonian Orbital Equations for Fermi Frames in the Vicinity the Earth
Authors
J. M. Gambi
M. L. García del Pino
M. M. Tung
Copyright Year
2016
DOI
https://doi.org/10.1007/978-3-319-23413-7_129

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