View source for Expected Gyrotational Orbit Accelerations of an Elliptical Fly-By

{{Infobox paper
| title = Expected Gyrotational Orbit Accelerations of an Elliptical Fly-By
| url = [http://www.naturalphilosophy.org/pdf/abstracts/abstracts_6355.pdf Link to paper]
| author = [[Thierry De Mees]]
| keywords = [[Fly-by]], [[satellite]], [[planet]], [[gravitation]], [[gyrotation]], [[prograde]], [[retrograde]], [[orbit]]
| published = 2011
| journal = [[General Science Journal]]
| num_pages = 8
}}

'''Read the full paper''' [http://www.naturalphilosophy.org/pdf/abstracts/abstracts_6355.pdf here]

==Abstract==

Following to the two former papers ''"The Gyro-Gravitational Spin Vector Torque Dynamics of Main Belt Asteroids in relationship with their Tilt and their Orbital Inclination"'' and ''"Cyclic Tilt Spin Vector Variations of Main Belt Asteroids due to the Solar Gyro-Gravitation"'', wherein we theoretically studied the tilt motions and variations of spinning asteroids, we continue the analysis with the study of the orbit anomalies of satellites. The equations for the fly-by of satellites near the Earth, or near planets in general are deduced.

[[Category:Scientific Paper|expected gyrotational orbit accelerations elliptical fly-by]]

[[Category:Gravity|expected gyrotational orbit accelerations elliptical fly-by]]