@Article{DomingosPradGome:2014:EfEcPe,
               author = "Domingos, R. C. and Prado, Antonio Fernando Bertachini de Almeida 
                         and Gomes, V. M.",
          affiliation = "{Universidade Estadual Paulista (UNESP)} and {Instituto Nacional 
                         de Pesquisas Espaciais (INPE)} and {Universidade Estadual Paulista 
                         (UNESP)}",
                title = "Effects of the eccentricity of a perturbing third body on the 
                         orbital correction maneuvers of a spacecraft",
              journal = "Mathematical Problems in Engineering",
                 year = "2014",
               volume = "2014",
             keywords = "Spacecraft, Annual cost, Averaged models, Dwarf planets, Eccentric 
                         orbits, Orbital maneuvers, Planetary system, Station keeping, 
                         Three-body problem, Orbits.",
             abstract = "The fuel consumption required by the orbital maneuvers when 
                         correcting perturbations on the orbit of a spacecraft due to a 
                         perturbing body was estimated. The main goals are the measurement 
                         of the influence of the eccentricity of the perturbing body on the 
                         fuel consumption required by the station keeping maneuvers and the 
                         validation of the averaged methods when applied to the problem of 
                         predicting orbital maneuvers. To study the evolution of the 
                         orbits, the restricted elliptic three-body problem and the single- 
                         and double-averaged models are used. Maneuvers are made by using 
                         impulsive and low thrust maneuvers. The results indicated that the 
                         averaged models are good to make predictions for the orbital 
                         maneuvers when the spacecraft is in a high inclined orbit. The 
                         eccentricity of the perturbing body plays an important role in 
                         increasing the effects of the perturbation and the fuel 
                         consumption required for the station keeping maneuvers. It is 
                         shown that the use of more frequent maneuvers decreases the annual 
                         cost of the station keeping to correct the orbit of a spacecraft. 
                         An example of an eccentric planetary system of importance to apply 
                         the present study is the dwarf planet Haumea and its moons, one of 
                         them in an eccentric orbit.",
                  doi = "10.1155/2014/359845",
                  url = "http://dx.doi.org/10.1155/2014/359845",
                 issn = "1024-123X",
                label = "scopus 2014-11 DomingosPradGome:2014:EfEcPe",
             language = "en",
           targetfile = "Domingos_effects.pdf",
        urlaccessdate = "27 abr. 2024"
}