Astronomy and Astrophysics – Astrophysics – Earth and Planetary Astrophysics
Scientific paper
2010-09-21
Astrophysics and Space Science Volume 332, Number 1, 99-106(2011)
Astronomy and Astrophysics
Astrophysics
Earth and Planetary Astrophysics
Accepted for publication in Astrophysics & Space Science
Scientific paper
10.1007/s10509-010-0493-9
This paper describes design of the trajectory and analysis of the stability of collinear point $L_2$ in the Sun-Earth system. The modified restricted three body problem with additional gravitational potential from the belt is used as the model for the Sun-Earth system. The effect of radiation pressure of the Sun and oblate shape of the Earth are considered. The point $L_2$ is asymptotically stable upto a specific value of time $t$ correspond to each set of values of parameters and initial conditions. The results obtained from this study would be applicable to locate a satellite, a telescope or a space station around the point $L_2$.
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