On the rotational trapped motion of a satellite near collinear equilibrium points L1,L2 in the planar ER3BP with variable eccentricity: Semi-analytical results and Melnikov chaos analysis

2026/07/01 by Sergey Ershkov, T.S. Amer, A.H. Elneklawy +1
Engineering · #Spacecraft Dynamics and Control #Space Satellite Systems and Control #Aerospace Engineering and Control Systems

paper · doi:10.1016/j.icarus.2026.117277

Citations

• Stability of the triangular points in the elliptic restricted problem of three bodies
• Characteristic exponents of the five equilibrium solutions in the elliptically restricted problem
• The chaotic rotation of Hyperion
• Spin-orbit coupling in the solar system