| Grant number: | 09/00735-5 |
| Support Opportunities: | Scholarships in Brazil - Doctorate |
| Start date: | August 01, 2009 |
| End date: | February 28, 2013 |
| Field of knowledge: | Engineering - Aerospace Engineering - Flight Dynamics |
| Principal Investigator: | Rodolpho Vilhena de Moraes |
| Grantee: | Jarbas Cordeiro Sampaio |
| Host Institution: | Faculdade de Engenharia (FEG). Universidade Estadual Paulista (UNESP). Campus de Guaratinguetá. Guaratinguetá , SP, Brazil |
Abstract The dynamical system associated to the orbital motion of artificial satellites with mean motion commensurable with the Earth's rotational motion is analyzed. This analysis can be applied to orbits of small and high eccentricities and inclinations. A suitable sequence of canonical transformations reduces the system to a kernel that can be integrated. The stability analysis of the motion in the neighborhood of the exact resonance is done. | |
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