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@InProceedings{NaccaratoCarMouTikSan:2016:CuAp,
               author = "Naccarato, Kleber Pinheiro and Carretero, Miguel Adrian and Moura, 
                         C. O. de and Tikami, Auro and Santos, Walter Abrah{\~a}o dos",
          affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto 
                         Nacional de Pesquisas Espaciais (INPE)} and {} and {Instituto 
                         Nacional de Pesquisas Espaciais (INPE)} and {Instituto Nacional de 
                         Pesquisas Espaciais (INPE)}",
                title = "Total lightning flash detection from space: a CubeSat approach",
                 year = "2016",
         organization = "International Lightning Detection Conference, 24. (ILDC); 
                         International Lightning Meteorolgy Conference, 6.",
             keywords = "lightning, cubesat, detection, technology, space, VHF, optical, 
                         thunderstorms.",
             abstract = "The RaioSat project intends to detect intra-cloud and 
                         cloud-to-ground lightning flashes simultaneously, the socalled 
                         total lightning data, using an optical sensor and a VHF antenna 
                         onboard a CubeSat platform. Two different sensor networks that 
                         detect and locate lightning flashes in Brazil, called RINDAT and 
                         BrasilDAT, will be used as reference data. The RaioSat mission is 
                         expected to be in a LEO orbit at 650km and it will use a 
                         3U-CubeSat aluminum frame (10x10x30cm) to accommodate the main 
                         platform and its payload. The main platform shall have telemetry, 
                         commanding and housekeeping capabilities via an on-board computer, 
                         3-axis attitude control and a GPS. The payload shall have a VHF 
                         passive antenna (range of 50 to 200MHz) and a spectral imaging 
                         camera (SIC) with resolution of 2,048 x 1,536 pixels leading to a 
                         surface imaging of 80 m/pixel. Also SIC shall have a spectral 
                         range from 700 to 900nm using a band-pass optical filter. 
                         Additionally, the paper briefly describes all the main stages of 
                         the space mission over the system life-cycle.",
  conference-location = "San Diego, CA",
      conference-year = "18-21 Apr.",
             language = "en",
           targetfile = "naccarato_total.pdf",
        urlaccessdate = "03 dez. 2020"
}


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