How to use the Sun–Earth Lagrange points for fundamental physics and navigation

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作者
A. Tartaglia
E. C. Lorenzini
D. Lucchesi
G. Pucacco
M. L. Ruggiero
P. Valko
机构
[1] Politecnico di Torino and INdAM,DISAT
[2] University of Padova,Department of Industrial Engineering
[3] Istituto di Astrofisica e Planetologia Spaziali - Istituto Nazionale di Astrofisica (IAPS/INAF),Department of Physics
[4] Istituto Nazionale di Fisica Nucleare (INFN),DISAT
[5] Sezione di Tor Vergata,Department of Physics
[6] University of Rome Tor Vergata,undefined
[7] Politecnico di Torino and INFN,undefined
[8] Slovak University of Technology,undefined
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关键词
Gravitation; Reference systems; Sun rotation; Galactic halo;
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摘要
We illustrate the proposal, nicknamed LAGRANGE, to use spacecraft, located at the Sun–Earth Lagrange points, as a physical reference frame. Performing time of flight measurements of electromagnetic signals traveling on closed paths between the points, we show that it would be possible: (a) to refine gravitational time delay knowledge due both to the Sun and the Earth; (b) to detect the gravito-magnetic frame dragging of the Sun, so deducing information about the interior of the star; (c) to check the possible existence of a galactic gravitomagnetic field, which would imply a revision of the properties of a dark matter halo; (d) to set up a relativistic positioning and navigation system at the scale of the inner solar system. The paper presents estimated values for the relevant quantities and discusses the feasibility of the project analyzing the behavior of the space devices close to the Lagrange points.
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