Table 4 Terminal time and corresponding impulsive increment solution Sets.
From: An analytical approach to generating orbital maneuver sets for spacecraft on-orbit services
Scenario | Time of Flight (days) | Quantity/pcs | Minimum ΔV(m/s) |
|---|---|---|---|
Scenario 1 | 0.5 | 258,719 | 3.0346 |
1.0 | 0 | Â | |
1.5 | 512,975 | 0.2433 | |
2.0 | 0 | Â | |
2.5 | 40,547 | 2.9367 | |
Scenario 2 | 0.5 | 1,022,751 | 0.9571 |
1.0 | 679,821 | 3.7921 | |
1.5 | 110,674 | 1.7724 | |
2.0 | 638,047 | 3.6937 | |
2.5 | 292,708 | 1.0740 | |
Scenario 3 | 0.5 | 860,827 | 3.7948 |
1.0 | 709,814 | 4.6838 | |
1.5 | 363,424 | 2.0381 | |
2.0 | 616,534 | 4.6103 | |
2.5 | 893,284 | 0.9117 | |
Scenario 4 | 6.5/24 | 382 | 3.3241 |
8/24 | 1770 | 3.6840 | |
9.5/24 | 2248 | −2.0381 | |
11/24 | 1156 | 5.9303 | |
12.5/24 | 858 | −4.9149 |
