Table 4
Largest contributing factors to the control magnitudes.
| Perturbations | Contributing Absolute | factors Relative |
|---|---|---|
| CW nonlinearity | N/A |  |
| Earth J2 gravity | a−4 | a−5rr |
| Earth J3 gravity (e(lp)) | a−5 | a−4rr |
| Lunisolar gravity | a | rr |
| Lunisolar gravity (e(s)) | a2 | a−1/2rrt |
| Lunisolar gravity (e(lp)) | a2 | a−1/2rr |
| Atmospheric drag | ρa−1 | ρa−1 |
| Solar radiation pressure | Const. | Const. |
Notes. For Earth J3 gravity (e(lp)) and lunisolar gravity (e(s) and e(lp)), the eccentricity originally had a contributing factor of (en2 rr) ∝ (ea−3 rr) to the relative fictitious accelerations, as shown in Sect. 4.1. Subsequently, the contributing factors were calculated by substituting the secular and long-period parts of the eccentricity for Earth J3 and lunisolar gravity into (ea−3 rr).
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