Research Article
Research on Minimum Time Interception Problem with a Tangent Impulse under Relative Motion Models
Table 1
Initial orbit parameters of the satellite and target.
| Orbital parameter | Target orbit | Satellite orbit |
| Semimajor axis (km) | 16545.13 | 16535.13 | Eccentricity | 0.4 | 0.399 | Orbit inclination (°) | 90 | 90 | RAAN (°) | 0 | 0 | Argument of perigee (°) | 20 | 19.99 | Initial true anomaly (°) | 30 | 29.99 |
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