Research Article
Study of Stability of Rotational Motion of Spacecraft with Canonical Variables
Table 5
Analysis of possible singularities of the Anloyer variables for satellites MP, PP1 of and PP2.
| Lyapunov stable equilibrium point of Table 2, 3 and 4, respectively. | Satellite | | | | | Situation |
| MP | 2,20566 | 0,862451 | 0,00373909 | 1680,4 | Accepted | PP-1 | 1,03788 | 1,55784 | 1,59939 | 3,92848 | Accepted | PP-2 | 1,26592 | 1,48439 | 0,196422 | 31,9882 | Accepted |
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