Journal of Aeronautics & Aerospace Engineering

Journal of Aeronautics & Aerospace Engineering
Open Access

ISSN: 2168-9792

+44-77-2385-9429

The Universal Stellar Law and its application to the explanation of stability and forms of planetary orbits


International Conference and Exhibition on Satellite

August 17-19, 2015 Houston, USA

Alexander M Krot

National Academy of Sciences, Belarus

Posters-Accepted Abstracts: J Aeronaut Aerospace Eng

Abstract :

This work considers the universal stellar law (USL) for explanation of stabilities and forms of planetary orbits in extra solar systems based on the statistical theory of gravitating spheroidal bodies. It shows that knowledge of some orbital characteristics for multi-planet extra solar systems refines own parameters of stars based on the combined 3rd Keplerâ��s law with universal stellar law (3KL-USL). The proposed 3KL-USL explains the stability of planetary orbits in the extra solar systems entirely and predicts statistical oscillations of the orbital angular velocity of rotation of planets around stars. This work applies the statistical theory of gravitating spheroidal bodies to explore forms of planetary orbits with regard to the Alfv�©nâ��s oscillating forces in the Solar system as well as other exoplanetary systems. It explains an origin of Alfv�©nâ��s radial and axial oscillations modifying forms of planetary orbits within the framework of the statistical theory of gravitating spheroidal bodies. This work finds that temporal deviation of the gravitational compression function of a spherically symmetricalspheroidal body (under the condition of its mechanical quasi equilibrium) induces the additional periodic force. In turn, as shown here, if the additional periodic force becomes counter balance to the gravitational force then the principle of anchoring mechanism is realized in extra solar systems, i.e. the stability of planetary orbits occurs. The work also notes that spatial deviation of gravitational potential of the rotating spheroidal body from spherically symmetrical one implies the difference of values of the radial and the axial orbital oscillations (even in the case of its mechanical equilibrium).

Biography :

Email:

alexkrot@vak.org.by

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