Análisis dinámico estructural de satélite educativo CanSat

Antonio Gómez Roa; Mauricio Leonel Paz González; Andrés Calvillo Téllez; Juan Antonio Paz González; Oscar Adrián Morales Contreras; José Cruz Núñez Pérez

doi:10.13053/CyS-22-2-2942

Análisis dinámico estructural de satélite educativo CanSat

Translated title of the contribution: Structural dynamic analysis of cansat educational satellite

Antonio Gómez Roa, Mauricio Leonel Paz González, Andrés Calvillo Téllez, Juan Antonio Paz González, Oscar Adrián Morales Contreras, José Cruz Núñez Pérez

Centro de Investigación y Desarrollo de Tecnología Digital (CITEDI)

Research output: Contribution to journal › Article › peer-review

1 Scopus citations

Abstract

The present article shows a dynamic analysis of the behavior experienced on the educative pico-satellite CanSat. The structure model was analyzed through the theory of the Finite Element, for the study of the structure we used the ANSYS platform, which allowed us to predict the answer of the structure during its launching, as well as the CanSat drop. We determined the first 15 modal forms and their natural corresponding frequencies. The analysis was performed considering the acceleration force of 30 g, on a vertical direction. We analyzed the concentration states of stress, defect and the values of natural frequencies. On this work, we discuss the results obtained in the structure configuration when this is transported by a hexacopter drone with a motor operation frequency of 480 Hz.

Translated title of the contribution	Structural dynamic analysis of cansat educational satellite
Original language	Spanish
Pages (from-to)	451-461
Number of pages	11
Journal	Computacion y Sistemas
Volume	22
Issue number	2
DOIs	https://doi.org/10.13053/CyS-22-2-2942
State	Published - 2018

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title = "An{\'a}lisis din{\'a}mico estructural de sat{\'e}lite educativo CanSat",

abstract = "The present article shows a dynamic analysis of the behavior experienced on the educative pico-satellite CanSat. The structure model was analyzed through the theory of the Finite Element, for the study of the structure we used the ANSYS platform, which allowed us to predict the answer of the structure during its launching, as well as the CanSat drop. We determined the first 15 modal forms and their natural corresponding frequencies. The analysis was performed considering the acceleration force of 30 g, on a vertical direction. We analyzed the concentration states of stress, defect and the values of natural frequencies. On this work, we discuss the results obtained in the structure configuration when this is transported by a hexacopter drone with a motor operation frequency of 480 Hz.",

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AU - Roa, Antonio Gómez

AU - González, Mauricio Leonel Paz

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AU - González, Juan Antonio Paz

AU - Contreras, Oscar Adrián Morales

AU - Pérez, José Cruz Núñez

PY - 2018

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AB - The present article shows a dynamic analysis of the behavior experienced on the educative pico-satellite CanSat. The structure model was analyzed through the theory of the Finite Element, for the study of the structure we used the ANSYS platform, which allowed us to predict the answer of the structure during its launching, as well as the CanSat drop. We determined the first 15 modal forms and their natural corresponding frequencies. The analysis was performed considering the acceleration force of 30 g, on a vertical direction. We analyzed the concentration states of stress, defect and the values of natural frequencies. On this work, we discuss the results obtained in the structure configuration when this is transported by a hexacopter drone with a motor operation frequency of 480 Hz.

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KW - Modal form

KW - Natural frequency

KW - Numerical modeling

KW - Structure

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Análisis dinámico estructural de satélite educativo CanSat

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