Research Article
Spacecraft Formation Orbit Estimation Using WLPS-Based Localization
Table 1
Third and fourth spacecrafts' orbital elements.
| | Inclination (deg) | Arg. perigee (deg) | RAAN (deg) | Initial anomaly (deg) |
| | S/C 1 | 5 |
0
| 5 | 3 | | S/C 2 |
−5
|
0
|
0
|
2
| | S/C 3 |
−3
|
0
|
7
|
−4
| | S/C 4 |
3
|
0
|
−4
|
10
| | S/C 5 |
−2.5
|
0
|
−3
|
2
| | S/C 6 |
−10
|
0
|
0
| |
|
|
