@InProceedings{OliveiraPrad:2015:UsElTe,
               author = "Oliveira, Thais Carneiro and Prado, Antonio Fernando Bertachini de 
                         Almeida",
          affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto 
                         Nacional de Pesquisas Espaciais (INPE)}",
                title = "Using eletrodynamic tethers to perform station-keeping maneuvers 
                         in leo satellites",
            booktitle = "Proceedings...",
                 year = "2015",
         organization = "International Symposium on Space Flight Dynamics, 25.",
             keywords = "Electromagnetic Tether, Station-Keeping Maneuver, Orbital 
                         Maneuver, Tether Systems, Disturbing Forces.",
             abstract = "This paper analyses the concept of using an electrodynamic tether 
                         to provide propulsion to a space system with an electric power 
                         supply and no fuel consumption. The present work is focused on 
                         orbit maintenance and on re-boost maneuvers for tethered satellite 
                         systems. The analyses of the results will be performed with the 
                         help of a practical tool called Perturbation Integrals and an 
                         orbit integrator that can include many external perturbations, 
                         like atmospheric drag, solar radiation pressure and luni-solar 
                         perturbation.",
  conference-location = "Munich, Germany",
      conference-year = "19-23 Oct.",
        urlaccessdate = "27 abr. 2024"
}