Research Article
Continuous-Thrust Station-Keeping of Cis-Lunar Orbits Using Optimal Sliding Mode Control with Practical Constraints
Table 3
The constraints and other parameters.
| | Parameters | | Value |
| | Initial insertion error | Position | 100 km | | Velocity | 1 cm/s |
| | Navigation error | Position | 1 km | | Velocity | 1 cm/s |
| | Propulsion error | | 2% |
| | Navigation interval | | 2 days |
| | Engine limitation | Minimum | | | Maximum | |
| | Orbital duration | | 2 years |
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