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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