Open Access
Table 5
Typical numerical conditions for control-acceleration analysis.
| Item | Symbol | Conditions |
|---|---|---|
| Initial time | – | 2024 January 1, |
| 00:00:00 UT | ||
| Initial orbital elements | – |  |
| Area-to-mass ratio | (S/m) | 4.5 × 10−3 m2 kg−1 |
| Atmospheric drag | Cd | 2.5 |
| (δ Bd / Bd) | 0.1 | |
| Solar radiation pressure | Ps | 4.56 × 10−6 Pa |
| Cs | 2 | |
| (δ Bs / Bs) | 0.1 | |
| Control period (e(s)) | – | 1 year |
Notes. The initial orbital elements of 
, and 
were selected based on each mission application, as given in Sects. 5.1–5.3.
Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.
Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.
Initial download of the metrics may take a while.