Abstract The attitude motion of an artificial satellite carrying a strong magnet is studied. The approximate first integrals of the problem, i.e., adiabatic invariants, are indicated. The basic properties of the satellite motions close to the regular precessions with slowly varying parameters are established via the analysis of the adiabatic invariants.
One Class of Motions for a Satellite Carrying a Strong Magnet
Cosmic Research ; 40 , 2 ; 133-141
2002-03-01
9 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
One Class of Motions for a Satellite Carrying a Strong Magnet
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