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@InProceedings{SolorzanoPradKuga:2001:ThPeUs,
               author = "Solorzano, C. R. H. and Prado, Antonio Fernando Bertachini de 
                         Almeida and Kuga, H{\'e}lio Kuga",
                title = "Third-body perturbation using a single averaged model",
            booktitle = "Proceedings...",
                 year = "2001",
         organization = "International Symposium on Space Flight Dynamics, 16.",
             keywords = "ENGENHARIA E TECNOLOGIA ESPACIAL, Third-Body Perturbation, 
                         Averaged Models, Astrodynamics.",
             abstract = "papers studied the effect of the third body perturbation in a 
                         spacecraft, usually working with the Hamiltonian of the system or 
                         with the disturbing function expressed in an analytic manner. The 
                         present paper has the goal of developing a semi-analytical study 
                         of the perturbation caused in a spacecraft by a third body with a 
                         single averaged model to eliminate the terms due to the short time 
                         periodic motion of the spacecraft. Several plots will show the 
                         time histories of the Keplerian elements of the orbits involved. 
                         One of the most important applications is to calculate the effect 
                         of Lunar and Solar perturbations on high-altitude Earth.",
  conference-location = "Pasadena, USA",
      conference-year = "3-7 Dec. 2001",
                label = "10982",
        urlaccessdate = "16 maio 2024"
}


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