Electromechanical flight stabilization system for CubeSat nanosatellites
The objective of the research was to design and simulate a stabilization system for attitude control of CubeSat nanosatellites in LEO orbit. The electronic system was inside the mechanical system, designed in Proteus. The mechanical system was designed in SolidWorks, then a CubeSat 3U CAD was downl...
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| Language: | English |
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Universidad Nacional de Colombia
2024-12-01
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| Series: | Dyna |
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| Online Access: | https://revistas.unal.edu.co/index.php/dyna/article/view/115957 |
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| author | Fausto R. Freire Karla E. Mora |
| author_facet | Fausto R. Freire Karla E. Mora |
| author_sort | Fausto R. Freire |
| collection | DOAJ |
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The objective of the research was to design and simulate a stabilization system for attitude control of CubeSat nanosatellites in LEO orbit. The electronic system was inside the mechanical system, designed in Proteus. The mechanical system was designed in SolidWorks, then a CubeSat 3U CAD was downloaded for simulation and finally, all CAD designs were assembled. These data were used for the analysis of the spatial environmental perturbations of aerodynamic drag, gradient, gravity and magnetic field. Attitude representation was done by analyzing the Euler, Poisson and Quaternions equations. Then, a fuzzy logic control was created with two cases for automatic control. The analysis and virtual reality simulation revealed the correct attitude control on the CubeSat 3U nanosatellite, considering the perturbations of the space environment and a new 25° orientation of each axis.
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| format | Article |
| id | doaj-art-7050834d88b74f9082030e8b1074a385 |
| institution | Kabale University |
| issn | 0012-7353 2346-2183 |
| language | English |
| publishDate | 2024-12-01 |
| publisher | Universidad Nacional de Colombia |
| record_format | Article |
| series | Dyna |
| spelling | doaj-art-7050834d88b74f9082030e8b1074a3852025-01-17T17:09:44ZengUniversidad Nacional de ColombiaDyna0012-73532346-21832024-12-019123410.15446/dyna.v91n234.115957Electromechanical flight stabilization system for CubeSat nanosatellitesFausto R. Freire0https://orcid.org/0000-0003-4307-5048Karla E. Mora1https://orcid.org/0009-0003-5778-7350Facultad de Ciencias de la Ingeniería e Industrias, Universidad UTE, Quito, EcuadorFacultad de Ciencias de la Ingeniería e Industrias, Universidad UTE, Quito, Ecuador The objective of the research was to design and simulate a stabilization system for attitude control of CubeSat nanosatellites in LEO orbit. The electronic system was inside the mechanical system, designed in Proteus. The mechanical system was designed in SolidWorks, then a CubeSat 3U CAD was downloaded for simulation and finally, all CAD designs were assembled. These data were used for the analysis of the spatial environmental perturbations of aerodynamic drag, gradient, gravity and magnetic field. Attitude representation was done by analyzing the Euler, Poisson and Quaternions equations. Then, a fuzzy logic control was created with two cases for automatic control. The analysis and virtual reality simulation revealed the correct attitude control on the CubeSat 3U nanosatellite, considering the perturbations of the space environment and a new 25° orientation of each axis. https://revistas.unal.edu.co/index.php/dyna/article/view/115957fuzzy controlsimulationvirtual realityelectromechanical stabilization systemLEO orbit |
| spellingShingle | Fausto R. Freire Karla E. Mora Electromechanical flight stabilization system for CubeSat nanosatellites Dyna fuzzy control simulation virtual reality electromechanical stabilization system LEO orbit |
| title | Electromechanical flight stabilization system for CubeSat nanosatellites |
| title_full | Electromechanical flight stabilization system for CubeSat nanosatellites |
| title_fullStr | Electromechanical flight stabilization system for CubeSat nanosatellites |
| title_full_unstemmed | Electromechanical flight stabilization system for CubeSat nanosatellites |
| title_short | Electromechanical flight stabilization system for CubeSat nanosatellites |
| title_sort | electromechanical flight stabilization system for cubesat nanosatellites |
| topic | fuzzy control simulation virtual reality electromechanical stabilization system LEO orbit |
| url | https://revistas.unal.edu.co/index.php/dyna/article/view/115957 |
| work_keys_str_mv | AT faustorfreire electromechanicalflightstabilizationsystemforcubesatnanosatellites AT karlaemora electromechanicalflightstabilizationsystemforcubesatnanosatellites |