Aliasi, G., Mengali, G. and Quarta, A. (2011) Artificial Equilibrium Points for a Generalized Sail in the Circular Restricted Three-Body Problem. Celestial Mechanics and Dynamical Astronomy, 110, 343-368.
https://doi.org/10.1007/s10569-011-9366-y

has been cited by the following article:

• TITLE: Artificial Equilibrium Points in the Low-Thrust Restricted Three-Body Problem When Both the Primaries Are Oblate Spheroids

  AUTHORS: Amit Mittal, Krishan Pal

  KEYWORDS: Restricted Three-Body Problem, Artificial Equilibrium Points, Low-Thrust, Stability, Oblate Spheroid, Zero Velocity Curves

  JOURNAL NAME: International Journal of Astronomy and Astrophysics, Vol.8 No.4, December 29, 2018

  ABSTRACT: This paper studies the existence and stability of the artificial equilibrium points (AEPs) in the low-thrust restricted three-body problem when both the primaries are oblate spheroids. The artificial equilibrium points (AEPs) are generated by canceling the gravitational and centrifugal forces with continuous low-thrust at a non-equilibrium point. Some graphical investigations are shown for the effects of the relative parameters which characterized the locations of the AEPs. Also, the numerical values of AEPs have been calculated. The positions of these AEPs will depend not only also on magnitude and directions of low-thrust acceleration. The linear stability of the AEPs has been investigated. We have determined the stability regions in the xy, xz and yz-planes and studied the effect of oblateness parameters A1(0A1and A2(0A2