Research Article
Dual Quaternion Based Close Proximity Operation for In-Orbit Assembly via Model Predictive Control
Table 1
Orbit parameters of chaser satellite.
| Parameters | Major semi-axis | Eccentricity | Inclination | RAAN | Argument of perigee | True anomaly |
| Values | | 0.02 | 45 (deg) | 0 | 0 | 30 (deg) |
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