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  • 1
    Online Resource
    Online Resource
    Hauppauge :Nova Science Publishers, Incorporated,
    Keywords: Gravitational fields -- Measurement. ; Electromagnetism -- Measurement. ; Electronic books.
    Type of Medium: Online Resource
    Pages: 1 online resource (302 pages)
    Edition: 1st ed.
    ISBN: 9781621006145
    DDC: 526/.7
    Language: English
    Note: Intro -- THE MEASUREMENTOF GRAVITOMAGNETISM:A CHALLENGING ENTERPRISE -- Contents -- List of Figures -- List of Tables -- Preface -- The Usual Decomposition -- The Decomposition Using Trace-Less Parts -- Decomposition Into Two Parts -- Decomposition Into Divergence-Free Parts -- Part IOVERVIEW -- Introduction -- 1.1. The Experimental Basis of General Relativity -- 1.2. Testing Gravitomagnetism -- 1.2.1. The Gravitomagnetic Field in Astrophysical Scenarios -- 1.2.2. The Gravitomagnetic Field of the Earth -- 1.2.3. The Gravitomagnetic Fields of the Sun and of Mars -- 1.3. LAGEOS and GP-B -- 1.3.1. The LAGEOS Tests -- 1.3.2. The GP-B Test -- 1.4. Is It Really Necessary to Perform Experiments to DirectlyMeasure Gravitomagnetism ? -- 1.5. Purpose of the Book -- 1.6. Acknowledgements -- Mach's Principle -- 2.1. Introduction -- 2.2. Absolute Versus Relative -- 2.3. Mach's Principle and General Relativity -- 2.4. Gravitomagnetism -- 2.5. Tact of the Natural Investigator -- 2.6. Quantum Theory and Inertia -- 2.7. Discussion -- Part IITHEORY -- Gravitoelectromagnetism:A Brief Review -- 3.1. Introduction -- 3.2. Linear Perturbation Approach to GEM -- 3.3. Gravitational Larmor Theorem -- 3.4. Spacetime Curvature Approach to GEM -- 3.5. Spin-Rotation-Gravity Coupling -- Analogies and Differences betweenGravito-Electromagnetism andElectromagnetism -- 4.1. Introduction -- 4.2. Direct Deduction of the Gravito-Electromagnetic Faraday-Henry Law -- 4.3. Is There a Gravito-Magnetic Meissner Effect? -- 4.4. Inconsistencies of the Gravito-Electromagnetic Analogy -- 4.5. Discussion and Conclusions -- Quasi-Inertial Coordinates -- 5.1. Introduction -- 5.2. Fermi-Walker Transport of a Tetrad -- 5.3. Gyroscope Held Fixed -- 5.4. Geodetic Precession of Freely-Falling Gyroscope -- 5.5. Construction of Quasi-Inertial Coordinates -- 5.5.1. The Basis Tetrad. , 5.5.2. Coordinate Transformations -- 5.5.3. Metric in Quasi-Inertial Frame -- 5.6. Spin Precession in the Quasi-Inertial Frame -- 5.7. Aberration -- 5.8. Two Sources-Sun and Earth -- 5.9. Local Inertial Frame of Earth -- 5.10. Summary -- The Lense-Thirring Effect on theOrbit of a Test Particle -- 6.1. The Orbit of a Test Particle in Space -- 6.2. The Derivation of the Lense-Thirring Effect on the Orbit ofa Test Particle: the Lagrangian Approach -- 6.3. The Derivation of the Lense-Thirring Effect on the Orbit ofa Test Particle: the Gaussian Approach -- 6.4. An Extension of the Gravitational Larmor Theorem -- 6.5. The Gravitomagnetic Stern-Gerlach Force -- Post-Newtonian OrbitalPerturbations -- 7.1. Introduction -- 7.2. The Equations of Motion -- 7.3. The Perturbing Potential -- 7.4. Orbital Perturbations -- 7.4.1. Precession of the Pericenter -- 7.4.2. Precession of the Orbital Plane -- 7.4.3. The Change in the Mean Motion -- 7.5. Time Difference Induced by Precession -- 7.5.1. Time Difference due to Pericenter Precession -- 7.5.2. Time Difference due to Orbital Precession -- 7.6. The Sidereal Period and the Gravitomagnetic Clock Effect -- 7.7. An Alternative Derivation of the Gravitomagnetic SiderealEffect for Circular and Equatorial Orbits -- Part IIIEXPERIMENT -- Recent Developments in TestingGravitomagnetism with SatelliteLaser Ranging -- 8.1. Introduction -- 8.1.1. The Gravitoelectric Effects -- 8.1.2. The Gravitomagnetic Effects -- 8.2. The Major Systematic Errors -- 8.2.1. The Non-Gravitational Errors -- 8.2.2. The Gravitational Errors -- 8.3. Some New Observables for Measuring the Lense-ThirringEffect -- 8.3.1. The Supplementary Orbital Planes Option -- 8.3.2. Other Approaches -- 8.4. The Impact of the 1st Generation of Earth Gravity Modelsfrom CHAMP and GRACE -- 8.4.1. The Full-Range Even Zonal Harmonics Observables. , 8.4.2. The Partial-Range Even Zonal Harmonics Observables -- 8.4.3. Combinations With the Other Existing Geodetic Satellites -- 8.5. The Use of Data from the Altimeter Satellite Jason-1 -- 8.5.1. A Possible Combination of Nodes and the Gravitational Errors -- 8.5.2. The Impact of the Observational Errors of Ajisai and Jason-1 -- 8.5.3. The Impact of the Non-Gravitational Perturbations of Ajisai -- 8.5.4. The Impact of the Non-Gravitational Perturbations on Jason-1 -- 8.6. The 2nd Generation of the GRACE-only Earth GravityModels and the First CHAMP/GRACE Combined Model -- 8.6.1. EIGEN-GRACE02S -- 8.6.2. GGM02S -- 8.6.3. EIGEN-CG01C -- 8.7. A Quantitative Assessment of the Impact of the SecularVariations of the Even Zonal Harmonics on the PerformedTest with the Nodes of the LAGEOS Satellites -- 8.7.1. Numerical Simulations -- 8.7.2. The J˙eff -- 8.7.3. Summary -- 8.8. Discussion and Conclusions -- 8.8.1. The Use of Ajisai and Jason-1 -- 8.8.2. The LAGEOS-LAGEOS II Node-Node-Perigee Combination -- 8.8.3. A New Dedicated Satellite? -- Acknowledgments -- The LAGEOS Satellites:Non-Gravitational Perturbationsand the Lense-Thirring Effect -- 9.1. Introduction -- 9.2. The Osculating Orbital Elements and the Gaussian PerturbativeEquations -- 9.3. The Non-Gravitational Perturbations:A Brief Review -- 9.3.1. Visible Radiation Effects: Direct Solar Radiation Pressure -- 9.3.2. Visible Radiation Effects: Earth Albedo -- 9.3.3. The LAGEOS Satellites Spin-Axis Modeling -- 9.3.4. Thermal Thrust Effects -- 9.3.5. The Asymmetric Reflectivity Effect -- 9.4. Numerical Simulation -- 9.5. The Lense-Thirring Effect Error Budget and the NGP -- 9.6. Conclusions -- On the Impossibility of Using theNode of Nearly Polar Satellites forMeasuring the Lense-Thirring Effect -- 10.1. The Use of GP-B Data -- 10.1.1. The Static and Time-Varying Part of the Earth Gravitational Field. , 10.2. On the (Im)possibility of Using a Polar Lares -- 10.3. Conclusions -- Error Budget for theGravitomagnetic Clock Effect -- 11.1. Introduction -- 11.2. The Impact of the Orbital Injection Errors -- 11.2.1. The Imperfect Cancellation of the Keplerian Periods -- 11.2.2. The Imperfect Cancellation of the Post-Newtonian Periods -- 11.2.3. The Impact of the Classical Gravitational Perturbations -- 11.2.4. The Impact of the Errors in the Inclinations -- 11.2.5. The N−Body Gravitational Perturbations -- 11.2.6. The Impact of the Non-Gravitational Perturbations -- 11.3. Conclusions -- Is it Possible to Measure theLense-Thirring Effect in theGravitational Fields of the Sun andof Mars? -- 12.1. The Solar Gravitomagnetic Field -- 12.1.1. Compatibility of the Estimated Extra-Precessions of Planetary Periheliawith the Lense-Thirring Effect -- 12.1.2. Analysis of Other Independent Data -- 12.2. Testing Gravitomagnetism with Mars Global Surveyor inthe Field of Mars -- 12.3. Discussion and Conclusions -- On the Detectability of the Earth'sGravitomagnetic Field in LaboratoryExperiments -- 13.1. Introduction -- 13.2. Proposed Earth Based Laboratory Experiments -- 13.2.1. A Foucault Pendulum at South Pole -- 13.2.2. A Magnetic-Gravitomagnetic Experiment -- 13.2.3. A Michelson-Moreley-Type Experiment -- 13.2.4. The Use of Ring Laser Gyroscopes -- 13.2.5. A Terrestrial Version of the Gravitomagnetic Clock Effect -- 13.3. Discussion and Conclusions -- Atom Interferometry andGravitomagnetism -- 14.1. Introduction -- 14.2. The Sagnac Effect -- 14.2.1. The Sagnac Effect for Light -- 14.2.2. The Operational Definition of Rotation -- 14.2.3. The Sagnac Effect for Matter Waves -- 14.3. Basics About Atomic Interferometry -- 14.3.1. The Non-Relativistic Hamiltonian for Atoms -- 14.3.2. The Hamiltonian for the Energy Levels -- 14.3.3. The Center-of-Mass Hamiltonian. , 14.3.4. The Dipole Interaction -- 14.3.5. Two-Level-System -- 14.3.6. The Beam Splitting -- 14.3.7. The Observed Interference Pattern -- 14.4. The Phase Shift for Gravito-Inertial Effects -- 14.4.1. Coupling to Acceleration -- 14.4.2. The Sagnac-Effect -- 14.4.3. The Space Project HYPER -- 14.4.4. Comparison with Other Methods -- Appendix AThe Inclination Functions -- Appendix BThe Classical Orbital Precessions -- B.1. The Node Coefficients -- B.2. The Pericenter Coefficients -- Appendix CWEB Resources -- References -- INDEX.
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  • 2
    Publication Date: 2012-06-21
    Print ISSN: 1687-7969
    Electronic ISSN: 1687-7977
    Topics: Physics
    Published by Hindawi
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  • 3
    Publication Date: 2012-06-21
    Description: We investigate the effect of possible a priori “imprinting” effects of general relativity itself on satellite/spacecraft-based tests of it. We deal with some performed or proposed time-delay ranging experiments in the sun's gravitational field. It turns out that the “imprint” of general relativity on the Astronomical Unit and the solar gravitational constant GM⊙, not solved for in the so far performed spacecraft-based time-delay tests, induces an a priori bias of the order of 10-6 in typical solar system ranging experiments aimed to measure the space curvature PPN parameter γ. It is too small by one order of magnitude to be of concern for the performed Cassini experiment, but it would affect future planned or proposed tests aiming to reach a 10-7–10-9 accuracy in determining γ.
    Print ISSN: 1687-7969
    Electronic ISSN: 1687-7977
    Topics: Physics
    Published by Hindawi
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  • 4
    Publication Date: 2012-06-21
    Description: We use the corrections to the Newton-Einstein secular precessions of the longitudes of perihelia ϖ˙ of some planets (Mercury, Earth, Mars, Jupiter, Saturn) of the Solar System, phenomenologically estimated as solve-for parameters by the Russian astronomer E. V. Pitjeva in a global fit of almost one century of data with the EPM2004 ephemerides, in order to put on the test the expression for the perihelion precession induced by a uniform cosmological constant Λ in the framework of the Schwarzschild-de Sitter (or Kottler) space-time. We compare such an extra rate to the estimated corrections to the planetary perihelion precessions by taking their ratio for different pairs of planets instead of using one perihelion at a time for each planet separately, as done so far in literature. The answer is negative, even by further rescaling by a factor 10 (and even 100 for Saturn) the errors in the estimated extra precessions of the perihelia released by Pitjeva. Our conclusions hold also for any other metric perturbation having the same dependence on the spatial coordinates, as those induced by other general relativistic cosmological scenarios and by many modified models of gravity. Currently ongoing and planned interplanetary spacecraft-based missions should improve our knowledge of the planets' orbits allowing for more stringent constraints.
    Print ISSN: 1687-7969
    Electronic ISSN: 1687-7977
    Topics: Physics
    Published by Hindawi
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  • 5
    Publication Date: 2013-01-22
    Print ISSN: 1687-7969
    Electronic ISSN: 1687-7977
    Topics: Physics
    Published by Hindawi
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  • 6
    Publication Date: 2014-09-30
    Description: We analytically calculate some orbital effects induced by the Lorentz-invariance/ momentum-conservation   parameterized   post-Newtonian (PPN)  parameter α3 in   a gravitationally bound binary system made of a primary orbited by a test particle.  We neither restrict ourselves to any particular orbital configuration nor to specific orientations of the primary’s spin axis ψˆ.  We use our results to put preliminary  upper bounds on α3 in the weak-field regime by using the latest data from Solar System’s planetary dynamics. By linearly combining the supplementary perihelion  precessions ∆w˙ of the Earth, Mars and Saturn, determined by astronomers with the Ephemerides of Planets and the Moon (EPM) 2011 ephemerides for the general relativistic  values of the PPN parameters β = γ = 1, we infer |α3| ;5 6 × 10−10.   Our result is about three orders of magnitude better than the previous weak-field  constraints existing  in the literature and of the same  order of magnitude of the constraint expected from the future BepiColombo mission to Mercury. It is, by construction, independent of the other preferred-frame PPN parameters α1, α2, both preliminarily constrained down to a ≈ 10−6 level. Future analyses should be performed by explicitly including α3 and a selection  of other PPN parameters in the models fitted by the astronomers to the observations and estimating them in dedicated covariance analyses.
    Electronic ISSN: 2075-4434
    Topics: Physics
    Published by MDPI
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