Research Article
Shorter Path Design and Control for an Underactuated Satellite
Table 2
Initial and obtained sets of a target attitude for case 1.
| State | Euler angle | | (deg) | (deg) |
| Initial attitude | — | 3-2-1 set | — | | — |
| Target attitude | Normal | 3-2-1 set | 1 | | 30.0 | Failure 3-axis | 1-2-1-… set | 3 | | 210.0 | 4 | | 160.6 | 5 | | 160.9 | 6 | | 161.0 | 7 | | 161.6 | 8 | | 161.6 | 2-1-2-… set | 3 | | 210.0 | 4 | | 160.6 | 5 | | 160.9 | 6 | | 161.8 | 7 | | 161.2 | 8 | | 162.3 |
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