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	𝐼2(rad)	𝐽2(rad)	𝜔(rad/s)	𝑇(s)	Situation
MP	0,56693	1,53881	−4,071∗10^−9	−1,543∗10^9	Accepted
PP-1	1,04377	1,23145	1,64936∗10^−5	380948,0	Accepted
PP-2	2,73176	0,46676	7,52836∗10^−9	8,346∗10^8	Accepted