Research Article
Study of Stability of Rotational Motion of Spacecraft with Canonical Variables
Table 6
Analysis of possible singularities of the Anloyer variables for satellites MP, PP1 and PP2.
| Unstable equilibrium point of Table 2, 3, and 4, respectively. |
| Satellite | | | | | Situation |
| MP | 0,56693 | 1,53881 | | | Accepted | PP-1 | 1,04377 | 1,23145 | | 380948,0 | Accepted | PP-2 | 2,73176 | 0,46676 | | | Accepted |
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