Research Article
Shorter Path Design and Control for an Underactuated Satellite
Table 1
Numerical simulation parameters.
| Parameters | Symbol | Value | Units |
| Moment of inertia for the spacecraft | | diag | kg·m2 | Skew angle | | 53.13 | deg | Control gains | | diag | — | | diag | — | Maximum number of maneuver | | 8 | — | Failed axis | | — | — |
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