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

The purpose of this document is to describe the design and simulation of an attitude determination system (ADS) for the CubeSat Colombia I picosatellite, based on an extended Kalman filter EKF [1,2]. In this development the propagation of the State of the system has been implemented through a Runge-...

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Vydáno v:	Revista Facultad de Ingeniería číslo 70; s. 146 - 154
Hlavní autoři:	Castellanos, Cesar A., Aparicio Pico, Lilia Edith
Médium:	Journal Article
Jazyk:	angličtina
Vydáno:	Universidad de Antioquia 27.02.2014
Témata:	attitude determination system extended Kalman filter non deterministic and deterministic algorithm picosatellite Colombia I
ISSN:	0120-6230, 2422-2844
On-line přístup:	Získat plný text
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Popis
Shrnutí:	The purpose of this document is to describe the design and simulation of an attitude determination system (ADS) for the CubeSat Colombia I picosatellite, based on an extended Kalman filter EKF [1,2]. In this development the propagation of the State of the system has been implemented through a Runge-Kutta procedure instead of traditional State Transition matrix method, improving predictions from the EKF filter without making direct measurements of angular velocity, it was obtained a reduced prediction time by incorporating a deterministic algorithm (the TRIAD algorithm) within the EKF. The results validated through simulation are those shown in this article.
ISSN:	0120-6230 2422-2844
DOI:	10.17533/udea.redin.18658