Notes. In the first column, (·) denotes the osculating orbital elements comprising the secular, long-period, and short-period terms as expressed in Eq. (20). The osculating orbital elements of (e_x, e_y) are substituted to (·)n²r_r, and those of (e_x, e_y, I, Ω, ϕ) are substituted to and for the analysis. In the second to fourth columns, c^(s), c^(lp) , and c^(sp) indicate the orders of the control acceleration magnitudes to compensate for the absolute physical perturbations for the secular, long-period, and short-period terms, respectively. They are defined as , and c^(sp) = δ(·)^(sp)n²a, respectively.