Abstract

This paper focuses on resonance of the motion of a geocentric synchronous satellite under the effect of gravitational forces of the Sun-Earth system subject to Poynting Robertson (PR) drag. With the assumption that the two bodies (the Earth, the Sun) lie in an ecliptic plane and the third body (satellite) lie in the orbital plane, five resonance points results from commensurability between the average angular velocity of the Earth and the mean motion of satellite. The amplitude and time period of the oscillation have been determined here in different cases at the resonance points.

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.