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Table 3

Control approach for mitigating each perturbation in this study.

Perturbations Fc fp fo ff
CW nonlinearity
Earth J2 gravity
Earth J3 gravity (e(lp)) * * *
Lunisolar gravity
Lunisolar gravity (e(s)) * * *
Lunisolar gravity (e(lp)) * * *
Atmospheric drag
Solar radiation pressure

Notes. A check mark indicates that all marked perturbations are compensated for by the control, and a check mark with an asterisk indicates that either the absolute or relative perturbations are compensated for. The perturbation specified as “Lunisolar gravity” excludes its secular and long-period effects on the eccentricity vector drift. The e(s) and e(lp) indicate the secular and long-period perturbations on the eccentricity vector, respectively.

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