Low-cost Test System for 1U CubeSat Attitude Control with Reaction Wheels

Pablo R. Yanyachi, Hammerly Mamani-Valencia, Brayan Espinoza-Garcia

Resultado de la investigación: Capítulo del libro/informe/acta de congresoContribución a la conferenciarevisión exhaustiva

Resumen

CubeSat development is becoming one of the most important research topics due to the growing interest of American countries in developing their aerospace technology. The main aim of this work is to simulate a 1U CubeSat Dynamics and develop a test system to allow students to probe their attitude control algorithms. The test system has four parts: a ball-type Dyson sphere air bearing, a Prototype of a CubeSat that includes reaction wheels as actuators, an Onboard computer based on an ARM Cortex M4 TM4C123G, and a PC Software interface. In its preliminary stages, the system allows testing attitude control algorithms for small Euler Angles and monitors reaction wheel parameters such as rates and currents. For the 1U CubeSat simulation, a linear mathematical model, a PID attitude controller, and a PID torque controller are proposed guidelines for attitude control algorithm designs.

Idioma originalInglés
Título de la publicación alojada2022 IEEE Biennial Congress of Argentina, ARGENCON 2022
EditorialInstitute of Electrical and Electronics Engineers Inc.
ISBN (versión digital)9781665480147
DOI
EstadoPublicada - 2022
Evento2022 IEEE Biennial Congress of Argentina, ARGENCON 2022 - San Juan, Argentina
Duración: 7 set. 20229 set. 2022

Serie de la publicación

Nombre2022 IEEE Biennial Congress of Argentina, ARGENCON 2022

Conferencia

Conferencia2022 IEEE Biennial Congress of Argentina, ARGENCON 2022
País/TerritorioArgentina
CiudadSan Juan
Período7/09/229/09/22

Nota bibliográfica

Publisher Copyright:
© 2022 IEEE.

Huella

Profundice en los temas de investigación de 'Low-cost Test System for 1U CubeSat Attitude Control with Reaction Wheels'. En conjunto forman una huella única.

Citar esto