“…The secondary-body motion is described by hybrid orbital elements (r, v x , i, h, θ, Ω) (Bakhtiari et al 2017c) Also, the third-body is in an inclined orbit with semimajor axis a 3 , eccentricity e 3 , argument of perigee ω 3 , argument of latitude θ 3 , and RAAN Ω 3 (Xu et al 2012). Also, the potential function of the system is stated as (Bakhtiari et al 2017a)…”