Design and simulation of an attitude determination system based on the Extended Kalman Filter for Cube-Sat Colombia I

Cesar A. Castellanos; Lilia Edith Aparicio Pico

doi:10.17533/udea.redin.18658

Autores/as

Cesar A. Castellanos Universidad Distrital FJC
Lilia Edith Aparicio Pico Universidad Distrital FJC

DOI:

https://doi.org/10.17533/udea.redin.18658

Palabras clave:

filtro extendido de Kalman, algoritmo determinístico y no determinístico, picosatélite Colombia I, sistema de determinación de actitud

Resumen

El propósito de este documento es describir el diseño y simulación de un Sistema de Determinación de Actitud (ADS) para el picosatélite Cubesat Colombia I, basado en el Filtro Extendido de Kalman (EKF) [1, 2] . En este desarrollo la propagación del estado del sistema ha sido implementada a través de un procedimiento Runge-Kutta a cambio del método tradicional por matriz de transición de estado, mejorando las predicciones del filtro EKF, sin hacer mediciones directas de velocidad angular . Se obtuvo una reducción del tiempo de predicción incorporando un algoritmo determinístico (El algoritmo TRIAD) dentro del EKF. Los resultados mostrados en este artículo se validaron mediante simulación.

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Biografía del autor/a

Cesar A. Castellanos, Universidad Distrital FJC

Grupo de investigación GITEM, Facultad de Ingeniería.

Lilia Edith Aparicio Pico, Universidad Distrital FJC

Facultad de Ingeniería.

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