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@InProceedings{MeirelesPradMeloPere:2020:StDiAt,
               author = "Meireles, Lucas Gouv{\^e}a and Prado, Antonio Fernando Bertachini 
                         de Almeida and Melo, Cristiano Fiorilo de and Pereira, Maria 
                         Cec{\'{\i}}lia",
          affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto 
                         Nacional de Pesquisas Espaciais (INPE)} and {Universidade Federal 
                         de Minas Gerais (UFMG)} and {Universidade Federal de Minas Gerais 
                         (UFMG)}",
                title = "A study on different attitude strategies for the LightSail-2 
                         mission",
            booktitle = "Anais... do 11º Workshop em Engenharia e Tecnologia Espaciais",
                 year = "2020",
               editor = "Rodrigues, Aline Castilho and Barbosa, Anderson Luis and Teixeira, 
                         Andr{\'e} Ferreira and Batista, Carlos Leandro Gomes and 
                         Oliveira, Caroline Mateus de and Cuellar, Dairo Antonio",
         organization = "Workshop em Engenharia e Tecnologia Espaciais, 11. (WETE)",
            publisher = "Instituto Nacional de Pesquisas Espaciais (INPE)",
              address = "S{\~a}o Jos{\'e} dos Campos",
             keywords = "LightSail-2, Solar Sailing, Orbital Mechanics, Optimal Attitude 
                         Strategy.",
             abstract = "Planetary Societys LightSail-2 mission successfully validated the 
                         orbital maneuvering capability of a Solar Radiation Pressure 
                         propelled spacecraft. This paper presents a study on alternative 
                         attitude strategies for the orientation of its solar sail with the 
                         goal of increasing the spacecrafts orbital maneuverability and its 
                         capacity of gaining altitude. Simulations with the use of 
                         Planetary Societys published strategy were made and compared with 
                         one that keeps the orientation of the solar sail at a direction 
                         that maximizes the spacecrafts specific orbital energy gain. A 
                         third strategy was proposed, with an additional goal of reducing 
                         the number of attitude maneuvers. Results show that it is possible 
                         to enhance the altitude gain of the spacecraft and improve the 
                         propelling influence of a solar sail while still reducing the 
                         number of maneuvers necessary to change the spacecrafts 
                         attitude.",
  conference-location = "S{\~a}o Jos{\'e} dos Campos",
      conference-year = "18 -20 ago. 2020",
                 issn = "2177-3114",
             language = "pt",
         organisation = "Instituto Nacional de Pesquisas Espaciais (INPE)",
                  ibi = "8JMKD3MGPDW34R/433LNQ8",
                  url = "http://urlib.net/ibi/8JMKD3MGPDW34R/433LNQ8",
           targetfile = "24 - [ARTIGO][INPE] Lucas Meireles.pdf",
                 type = "CMC",
        urlaccessdate = "28 mar. 2024"
}


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