Desarrollo de un método para determinar la ubicación de un nanosatelite utilizando ADS-B

• Sergey Frolov Research Institute of Radioelectronic Systems, Southwest State University,305040, Kursk, Russian Federation
• Olga Chadrina Facultad Ciencias de la Ingeniería e Industrias, Universidad UTE, Quito, Ecuador
• Evgeny Titenko Research Institute of Radioelectronic Systems, Southwest State University,305040, Kursk, Russian Federation
• Aleksey Shitov Research Institute of Radioelectronic Systems, Southwest State University,305040, Kursk, Russian Federation
• Khanis Andrey Department of Information Security, Southwest State University
• Teterin Dmitry JSC Aviaavtomatika named after V.V. Tarasov, 305040, Kursk, Russian federation
• Gorbunov Andrey Research Institute of Radioelectronic Systems, Southwest State University,305040, Kursk, Russian Federation

Palabras clave: Aeronaves, ADS-B, Tierra, Nanosatélite, Cubesat.

Resumen

El método para calcular las coordenadas aproximadas de ubicación del Cubesat, utilizando los datos históricos de vuelo, tiene un error bastante alto; ya que no considera las características geofísicas de la trayectoria de vuelo. Como regla general, las desviaciones en los cálculos están asociadas con la alta velocidad del vuelo a lo largo de toda la órbita, la limitada área de cobertura del Cubesat sobre la superficie de la tierra (2000-3000 km²) y la dependencia simultanea de la ubicación de los puntos de referencia sobre la superficie de la tierra y la del Cubesat en el espacio. El objetivo del estudio fue desarrollar un método que permita determinar la posición del Cubesat, mediante la recepción de la posición de aeronaves y buques que utilizan ADS-B. Los cálculos demuestran El método y algoritmo propuestos pueden calcular no solamente la posición del Cubesat, sino también determinar su trayectoria. Esta circunstancia permitirá a futuro dejar de utilizar los datos orbitales enviados desde las estaciones radar para determinar la posición de un Cubesat.

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