@Article{GonçalvesRoccMoraPrad:2016:EfInTe,
               author = "Gon{\c{c}}alves, Liana Dias and Rocco, Evandro Marconi and 
                         Moraes, Rodolpho Vilhena de and Prado, Antonio Fernando Bertachini 
                         de Almeida",
          affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto 
                         Nacional de Pesquisas Espaciais (INPE)} and {Universidade Federal 
                         de S{\~a}o Paulo (UNIFESP)} and {Instituto Nacional de Pesquisas 
                         Espaciais (INPE)}",
                title = "Effects of the individual terms of the lunar potential in the 
                         motion of satellites around the Moon",
              journal = "International Journal of Theoretical and Applied Mechanics",
                 year = "2016",
               volume = "1",
                pages = "20--29",
             keywords = "Astrodynamics, Lunar potential, Orbital Motion, Orbital Maneuvers, 
                         Satellite, Control System.",
             abstract = "The present work study analyzes the influence of non homogeneity 
                         of the lunar gravitational field in the orbit of an artificial 
                         satellite. The model is based in spherical harmonics, according to 
                         the development presented by Konopliv. This model allows us to 
                         consider spherical harmonics until degree and order 100. 
                         Simulations are performed for the analysis of the following facts: 
                         the contribution of each term of the potential; the variation of 
                         the perturbation due to the inclination of the orbit; the 
                         actuation of the control system; the influence in transfer and 
                         correction maneuvers made to minimize the perturbative effects in 
                         the artificial satellite orbit. The transfer and correction 
                         maneuvers of lunar satellites are simulated using continuous 
                         thrust and trajectory control in closed loop.",
                 issn = "0861-6663",
                label = "lattes: 0404556644554239 1 
                         Gon{\c{c}}alvesRoccMoraPrad:2016:EfInTe",
             language = "en",
           targetfile = "goncalves_effects.pdf",
        urlaccessdate = "11 maio 2024"
}